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Revert "Merge pull request #20 from cthunter01/propagator" 
This reverts commit 6280d9fb0184275843a8f4406c7293e41e65a639, reversing
changes made to 3c9c8b8c6a2b2e7430ff09efdc2cc0c1996b16ca.
2025-04-16 18:23:28 -06:00

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<engine-database>
<engine-list>
<engine mfg="Aerotech" code="C3.4T" Type="single-use" dia="18." len="72." initWt="23.9"
propWt="5.2" delays="4,6,1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="3.133" peakThrust="9.08" throatDia="0." exitDia="0." Itot="8.959"
burn-time="2.86" massFrac="21.76" Isp="175.69" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Aerotech C3.4-PT RASP.ENG file made from NAR published data
File produced, 2013
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="5.2" cg="36."/>
<eng-data t="0.023" f="3.188" m="5.17872" cg="36."/>
<eng-data t="0.028" f="5.669" m="5.16587" cg="36."/>
<eng-data t="0.093" f="9.08" m="4.88765" cg="36."/>
<eng-data t="0.235" f="8.208" m="4.17521" cg="36."/>
<eng-data t="0.427" f="6.881" m="3.33445" cg="36."/>
<eng-data t="0.513" f="6.188" m="3.00827" cg="36."/>
<eng-data t="0.6" f="5.438" m="2.71473" cg="36."/>
<eng-data t="0.666" f="4.803" m="2.51858" cg="36."/>
<eng-data t="0.762" f="3.649" m="2.2831" cg="36."/>
<eng-data t="0.838" f="2.668" m="2.14377" cg="36."/>
<eng-data t="0.97" f="2.149" m="1.95925" cg="36."/>
<eng-data t="1.228" f="1.918" m="1.65473" cg="36."/>
<eng-data t="1.522" f="1.918" m="1.32744" cg="36."/>
<eng-data t="1.8" f="1.86" m="1.02263" cg="36."/>
<eng-data t="2.013" f="1.745" m="0.799792" cg="36."/>
<eng-data t="2.068" f="2.034" m="0.739473" cg="36."/>
<eng-data t="2.134" f="1.803" m="0.665979" cg="36."/>
<eng-data t="2.326" f="1.803" m="0.465052" cg="36."/>
<eng-data t="2.509" f="1.745" m="0.276623" cg="36."/>
<eng-data t="2.645" f="1.687" m="0.141166" cg="36."/>
<eng-data t="2.721" f="1.457" m="0.0718222" cg="36."/>
<eng-data t="2.807" f="0.879" m="0.01352" cg="36."/>
<eng-data t="2.86" f="0." m="0." cg="36."/>
</data>
</engine>
<engine mfg="Aerotech" code="D9W" Type="reloadable" dia="24." len="70." initWt="47.1"
propWt="10.1" delays="4,7" auto-calc-mass="1" auto-calc-cg="1" avgThrust="9.979"
peakThrust="20." throatDia="0." exitDia="0." Itot="18.76" burn-time="1.88"
massFrac="21.44" Isp="189.41" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<comments>Aerotech D9 RASP.ENG file made from NAR published data
File produced July 4, 2000
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="10.1" cg="35."/>
<eng-data t="0.023" f="2.204" m="10.0864" cg="35."/>
<eng-data t="0.077" f="1.653" m="10.0303" cg="35."/>
<eng-data t="0.177" f="4.96" m="9.85228" cg="35."/>
<eng-data t="0.269" f="8.817" m="9.51109" cg="35."/>
<eng-data t="0.308" f="9.92" m="9.31438" cg="35."/>
<eng-data t="0.315" f="9.368" m="9.27804" cg="35."/>
<eng-data t="0.358" f="10.604" m="9.04686" cg="35."/>
<eng-data t="0.415" f="11.94" m="8.70096" cg="35."/>
<eng-data t="0.515" f="13.917" m="8.00492" cg="35."/>
<eng-data t="0.623" f="16.675" m="7.11555" cg="35."/>
<eng-data t="0.731" f="19.155" m="6.0739" cg="35."/>
<eng-data t="0.792" f="20." m="5.43096" cg="35."/>
<eng-data t="0.865" f="19.155" m="4.66154" cg="35."/>
<eng-data t="0.889" f="19.562" m="4.41141" cg="35."/>
<eng-data t="0.923" f="18.6" m="4.06214" cg="35."/>
<eng-data t="1.038" f="16.12" m="2.98733" cg="35."/>
<eng-data t="1.115" f="14.195" m="2.35899" cg="35."/>
<eng-data t="1.185" f="12.538" m="1.85526" cg="35."/>
<eng-data t="1.277" f="10.336" m="1.28878" cg="35."/>
<eng-data t="1.373" f="7.44" m="0.829414" cg="35."/>
<eng-data t="1.485" f="4.822" m="0.459729" cg="35."/>
<eng-data t="1.612" f="2.755" m="0.200697" cg="35."/>
<eng-data t="1.762" f="1.24" m="0.0393873" cg="35."/>
<eng-data t="1.88" f="0." m="0." cg="35."/>
</data>
</engine>
<engine mfg="Aerotech" code="D13W" Type="reloadable" dia="18." len="70." initWt="33."
propWt="9.8" delays="4,7,10" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="11.284" peakThrust="22.25" throatDia="0." exitDia="0." Itot="19.183"
burn-time="1.7" massFrac="29.7" Isp="199.6" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="9.8" cg="35."/>
<eng-data t="0.01" f="22.25" m="9.74317" cg="35."/>
<eng-data t="0.2" f="22.25" m="7.58344" cg="35."/>
<eng-data t="0.4" f="20." m="5.42499" cg="35."/>
<eng-data t="0.8" f="12.5" m="2.1043" cg="35."/>
<eng-data t="1." f="8." m="1.057" cg="35."/>
<eng-data t="1.4" f="1.34" m="0.102686" cg="35."/>
<eng-data t="1.7" f="0." m="0." cg="35."/>
</data>
</engine>
<engine mfg="Aerotech" code="D15T" Type="reloadable" dia="24." len="70." initWt="44."
propWt="8.9" delays="4,7" auto-calc-mass="1" auto-calc-cg="1" avgThrust="14.012"
peakThrust="28.5" throatDia="0." exitDia="0." Itot="19.617" burn-time="1.4"
massFrac="20.23" Isp="224.77" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<data>
<eng-data t="0." f="0." m="8.9" cg="35."/>
<eng-data t="0.01" f="26." m="8.84102" cg="35."/>
<eng-data t="0.1" f="28.5" m="7.72838" cg="35."/>
<eng-data t="0.4" f="23." m="4.22373" cg="35."/>
<eng-data t="0.8" f="11.2" m="1.12058" cg="35."/>
<eng-data t="1." f="4.5" m="0.408309" cg="35."/>
<eng-data t="1.4" f="0." m="0." cg="35."/>
</data>
</engine>
<engine mfg="Aerotech" code="D24T" Type="reloadable" dia="18." len="70." initWt="30.8"
propWt="8.7" delays="4,7" auto-calc-mass="1" auto-calc-cg="1" avgThrust="14.768"
peakThrust="25.52" throatDia="0." exitDia="0." Itot="18.017" burn-time="1.22"
massFrac="28.25" Isp="211.17" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<comments>AEROTECH D24 RASP.ENG file made from NAR data
File produced August 22, 2002
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="8.7" cg="35."/>
<eng-data t="0.01" f="10.992" m="8.67346" cg="35."/>
<eng-data t="0.015" f="14.575" m="8.6426" cg="35."/>
<eng-data t="0.023" f="18.641" m="8.57844" cg="35."/>
<eng-data t="0.041" f="25.52" m="8.38652" cg="35."/>
<eng-data t="0.048" f="23.419" m="8.30381" cg="35."/>
<eng-data t="0.06" f="22.576" m="8.17055" cg="35."/>
<eng-data t="0.108" f="21.141" m="7.66391" cg="35."/>
<eng-data t="0.127" f="21.853" m="7.46668" cg="35."/>
<eng-data t="0.189" f="21.141" m="6.8231" cg="35."/>
<eng-data t="0.245" f="20.769" m="6.25645" cg="35."/>
<eng-data t="0.255" f="21.01" m="6.15558" cg="35."/>
<eng-data t="0.365" f="20.408" m="5.05558" cg="35."/>
<eng-data t="0.421" f="19.805" m="4.51188" cg="35."/>
<eng-data t="0.473" f="19.324" m="4.02062" cg="35."/>
<eng-data t="0.572" f="17.999" m="3.12851" cg="35."/>
<eng-data t="0.676" f="16.673" m="2.25791" cg="35."/>
<eng-data t="0.734" f="15.71" m="1.80443" cg="35."/>
<eng-data t="0.78" f="14.395" m="1.47008" cg="35."/>
<eng-data t="0.803" f="14.515" m="1.30954" cg="35."/>
<eng-data t="0.828" f="13.07" m="1.14304" cg="35."/>
<eng-data t="0.884" f="11.996" m="0.804133" cg="35."/>
<eng-data t="0.94" f="9.838" m="0.508924" cg="35."/>
<eng-data t="0.973" f="8.163" m="0.365502" cg="35."/>
<eng-data t="1.02" f="5.649" m="0.208768" cg="35."/>
<eng-data t="1.07" f="3.373" m="0.0998549" cg="35."/>
<eng-data t="1.116" f="1.936" m="0.0408921" cg="35."/>
<eng-data t="1.151" f="0.977" m="0.0162761" cg="35."/>
<eng-data t="1.22" f="0." m="0." cg="35."/>
</data>
</engine>
<engine mfg="Aerotech" code="D2.3T" Type="single-use" dia="18." len="72." initWt="29.3"
propWt="10.7" delays="1000" auto-calc-mass="1" auto-calc-cg="1" avgThrust="2.114"
peakThrust="10.14" throatDia="0." exitDia="0." Itot="17.209" burn-time="8.14"
massFrac="36.52" Isp="164." tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1."
FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Aerotech D2.3-PT RASP.ENG file made from NAR published data
File produced, 2013
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="10.7" cg="36."/>
<eng-data t="0.02" f="5.071" m="10.6685" cg="36."/>
<eng-data t="0.039" f="9.478" m="10.5825" cg="36."/>
<eng-data t="0.093" f="10.14" m="10.2532" cg="36."/>
<eng-data t="0.184" f="9.478" m="9.69818" cg="36."/>
<eng-data t="0.275" f="8.429" m="9.19157" cg="36."/>
<eng-data t="0.438" f="6.82" m="8.41884" cg="36."/>
<eng-data t="0.657" f="4.372" m="7.65684" cg="36."/>
<eng-data t="0.747" f="3.392" m="7.4396" cg="36."/>
<eng-data t="0.838" f="2.413" m="7.27537" cg="36."/>
<eng-data t="1.056" f="2.064" m="6.97195" cg="36."/>
<eng-data t="1.365" f="1.923" m="6.58894" cg="36."/>
<eng-data t="1.892" f="1.783" m="5.98176" cg="36."/>
<eng-data t="2.528" f="1.713" m="5.29052" cg="36."/>
<eng-data t="2.946" f="1.713" m="4.8453" cg="36."/>
<eng-data t="3.219" f="1.643" m="4.56047" cg="36."/>
<eng-data t="4.091" f="1.573" m="3.68863" cg="36."/>
<eng-data t="4.727" f="1.573" m="3.06659" cg="36."/>
<eng-data t="5.218" f="1.573" m="2.58637" cg="36."/>
<eng-data t="5.636" f="1.573" m="2.17754" cg="36."/>
<eng-data t="6.217" f="1.573" m="1.6093" cg="36."/>
<eng-data t="6.726" f="1.433" m="1.13362" cg="36."/>
<eng-data t="7.199" f="1.503" m="0.701884" cg="36."/>
<eng-data t="7.635" f="1.363" m="0.313406" cg="36."/>
<eng-data t="7.907" f="1.224" m="0.094646" cg="36."/>
<eng-data t="8.016" f="0.734" m="0.0282957" cg="36."/>
<eng-data t="8.14" f="0." m="0." cg="36."/>
</data>
</engine>
<engine mfg="Aerotech" code="D7-RC" Type="reloadable" dia="24." len="70." initWt="42.2"
propWt="10.5" delays="1000" auto-calc-mass="1" auto-calc-cg="1" avgThrust="6.456"
peakThrust="10.99" throatDia="0." exitDia="0." Itot="18.527" burn-time="2.87"
massFrac="24.88" Isp="179.93" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<comments>Aerotech D7 RASP.ENG file made from NAR published data
File produced July 4, 2000
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="10.5" cg="35."/>
<eng-data t="0.036" f="3.336" m="10.466" cg="35."/>
<eng-data t="0.084" f="9.326" m="10.2937" cg="35."/>
<eng-data t="0.101" f="10.281" m="10.1993" cg="35."/>
<eng-data t="0.143" f="10.827" m="9.94808" cg="35."/>
<eng-data t="0.213" f="10.99" m="9.51533" cg="35."/>
<eng-data t="0.271" f="10.887" m="9.15578" cg="35."/>
<eng-data t="0.359" f="10.685" m="8.61786" cg="35."/>
<eng-data t="0.471" f="10.13" m="7.95726" cg="35."/>
<eng-data t="0.506" f="10.342" m="7.75423" cg="35."/>
<eng-data t="0.535" f="9.929" m="7.58765" cg="35."/>
<eng-data t="0.81" f="8.697" m="6.13621" cg="35."/>
<eng-data t="1.226" f="6.713" m="4.31969" cg="35."/>
<eng-data t="1.589" f="5.138" m="3.10068" cg="35."/>
<eng-data t="1.8" f="4.861" m="2.50285" cg="35."/>
<eng-data t="2.151" f="4.581" m="1.56374" cg="35."/>
<eng-data t="2.649" f="4.57" m="0.272392" cg="35."/>
<eng-data t="2.696" f="3.887" m="0.15976" cg="35."/>
<eng-data t="2.748" f="2.388" m="0.0672987" cg="35."/>
<eng-data t="2.807" f="0.889" m="0.0125122" cg="35."/>
<eng-data t="2.842" f="0.207" m="0.00164238" cg="35."/>
<eng-data t="2.87" f="0." m="0." cg="35."/>
</data>
</engine>
<engine mfg="Aerotech" code="E11J" Type="reloadable" dia="24." len="70." initWt="62.4"
propWt="25." delays="3" auto-calc-mass="1" auto-calc-cg="1" avgThrust="11.613"
peakThrust="19.259" throatDia="0." exitDia="0." Itot="32.865" burn-time="2.83"
massFrac="40.06" Isp="134.05" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<comments>Based On NAR Test Data
12/23/93</comments>
<data>
<eng-data t="0." f="0." m="25." cg="35."/>
<eng-data t="0.0725446" f="14.3704" m="24.6035" cg="35."/>
<eng-data t="0.16183" f="17.6296" m="23.5168" cg="35."/>
<eng-data t="0.206473" f="18.3704" m="22.9055" cg="35."/>
<eng-data t="0.418527" f="19.2593" m="19.8705" cg="35."/>
<eng-data t="0.731027" f="18.3704" m="15.3979" cg="35."/>
<eng-data t="1.31696" f="14.2222" m="8.1343" cg="35."/>
<eng-data t="1.91964" f="9.03704" m="2.80263" cg="35."/>
<eng-data t="2.51116" f="2.22222" m="0.269489" cg="35."/>
<eng-data t="2.83" f="0." m="0." cg="35."/>
</data>
</engine>
<engine mfg="Aerotech" code="E15W" Type="single-use" dia="24." len="70." initWt="50.1"
propWt="20.1" delays="4,7,1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="15.06" peakThrust="28.84" throatDia="0." exitDia="0." Itot="39.759"
burn-time="2.64" massFrac="40.12" Isp="201.71" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Aerotech E15 RASP.ENG file made from NAR published data
File produced July 4, 2000
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="20.1" cg="35."/>
<eng-data t="0.02" f="23.33" m="19.9821" cg="35."/>
<eng-data t="0.036" f="27.318" m="19.7772" cg="35."/>
<eng-data t="0.058" f="28.84" m="19.4649" cg="35."/>
<eng-data t="0.079" f="27.171" m="19.1676" cg="35."/>
<eng-data t="0.139" f="25.638" m="18.3667" cg="35."/>
<eng-data t="0.183" f="24.263" m="17.8117" cg="35."/>
<eng-data t="0.237" f="24.106" m="17.1515" cg="35."/>
<eng-data t="0.297" f="22.426" m="16.4457" cg="35."/>
<eng-data t="0.373" f="21.964" m="15.593" cg="35."/>
<eng-data t="0.4" f="20.894" m="15.3005" cg="35."/>
<eng-data t="0.443" f="21.355" m="14.8413" cg="35."/>
<eng-data t="0.487" f="20.442" m="14.3764" cg="35."/>
<eng-data t="0.617" f="19.833" m="13.0529" cg="35."/>
<eng-data t="0.742" f="18.457" m="11.8431" cg="35."/>
<eng-data t="0.812" f="20." m="11.1626" cg="35."/>
<eng-data t="0.85" f="18.006" m="10.7976" cg="35."/>
<eng-data t="0.899" f="18.467" m="10.3458" cg="35."/>
<eng-data t="1.035" f="17.711" m="9.10213" cg="35."/>
<eng-data t="1.1" f="16.945" m="8.53273" cg="35."/>
<eng-data t="1.16" f="16.945" m="8.01874" cg="35."/>
<eng-data t="1.377" f="15.736" m="6.22613" cg="35."/>
<eng-data t="1.426" f="14.656" m="5.8497" cg="35."/>
<eng-data t="1.436" f="16.198" m="5.77171" cg="35."/>
<eng-data t="1.463" f="14.813" m="5.56006" cg="35."/>
<eng-data t="1.55" f="14.361" m="4.91849" cg="35."/>
<eng-data t="1.572" f="15.432" m="4.75281" cg="35."/>
<eng-data t="1.61" f="13.752" m="4.47248" cg="35."/>
<eng-data t="1.827" f="12.839" m="3.01392" cg="35."/>
<eng-data t="2.126" f="10.098" m="1.28036" cg="35."/>
<eng-data t="2.337" f="6.116" m="0.41559" cg="35."/>
<eng-data t="2.538" f="1.369" m="0.0352967" cg="35."/>
<eng-data t="2.64" f="0." m="0." cg="35."/>
</data>
</engine>
<engine mfg="Aerotech" code="E16W" Type="reloadable" dia="29." len="121." initWt="107."
propWt="19." delays="4,7" auto-calc-mass="1" auto-calc-cg="1" avgThrust="14.099"
peakThrust="27.92" throatDia="0." exitDia="0." Itot="38.35" burn-time="2.72"
massFrac="17.76" Isp="205.82" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<data>
<eng-data t="0." f="0." m="19." cg="60.5"/>
<eng-data t="0.04" f="27.92" m="18.7233" cg="60.5"/>
<eng-data t="0.16" f="23.5" m="17.1948" cg="60.5"/>
<eng-data t="0.26" f="21.4" m="16.0826" cg="60.5"/>
<eng-data t="2." f="10.9" m="2.16039" cg="60.5"/>
<eng-data t="2.38" f="6.36" m="0.535663" cg="60.5"/>
<eng-data t="2.72" f="0." m="0." cg="60.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="E18W" Type="reloadable" dia="24." len="70." initWt="57."
propWt="20.7" delays="4,8" auto-calc-mass="1" auto-calc-cg="1" avgThrust="18.082"
peakThrust="31." throatDia="0." exitDia="0." Itot="39.78" burn-time="2.2"
massFrac="36.32" Isp="195.96" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<data>
<eng-data t="0." f="0." m="20.7" cg="35."/>
<eng-data t="0.04" f="31." m="20.3774" cg="35."/>
<eng-data t="0.4" f="30." m="14.6638" cg="35."/>
<eng-data t="0.8" f="26.7" m="8.7629" cg="35."/>
<eng-data t="1.2" f="19.1" m="3.99638" cg="35."/>
<eng-data t="1.6" f="8." m="1.17602" cg="35."/>
<eng-data t="2." f="2.2" m="0.11448" cg="35."/>
<eng-data t="2.2" f="0." m="0." cg="35."/>
</data>
</engine>
<engine mfg="Aerotech" code="E20W" Type="single-use" dia="24." len="65." initWt="49."
propWt="16.2" delays="4,7,10" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="19.73" peakThrust="34.677" throatDia="0." exitDia="0." Itot="34.683"
burn-time="1.76" massFrac="33.06" Isp="218.32" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>@File: E20.txt, @Pts-I: 1001, @Pts-O: 32, @Sm: 3, @CO: 5%
@TI: 34.6666, @TIa: 34.5451, @TIe: 0.0%, @ThMax: 34.6991, @ThAvg: 22.1301, @Tb: 1.561
Exported using ThrustCurveTool, www.ThrustGear.com
</comments>
<data>
<eng-data t="0." f="0." m="16.2" cg="32.5"/>
<eng-data t="0." f="0.0290422" m="16.2" cg="32.5"/>
<eng-data t="0.024" f="0.227567" m="16.1986" cg="32.5"/>
<eng-data t="0.038" f="1.39403" m="16.1933" cg="32.5"/>
<eng-data t="0.048" f="2.6721" m="16.1838" cg="32.5"/>
<eng-data t="0.056" f="5.81661" m="16.1679" cg="32.5"/>
<eng-data t="0.06" f="7.76916" m="16.1552" cg="32.5"/>
<eng-data t="0.062" f="9.00446" m="16.1474" cg="32.5"/>
<eng-data t="0.064" f="10.7176" m="16.1382" cg="32.5"/>
<eng-data t="0.072" f="20.3365" m="16.0801" cg="32.5"/>
<eng-data t="0.074" f="22.4147" m="16.0602" cg="32.5"/>
<eng-data t="0.08" f="27.1311" m="15.9908" cg="32.5"/>
<eng-data t="0.084" f="28.9874" m="15.9383" cg="32.5"/>
<eng-data t="0.09" f="30.5394" m="15.8549" cg="32.5"/>
<eng-data t="0.104" f="32.9513" m="15.6473" cg="32.5"/>
<eng-data t="0.124" f="34.2647" m="15.3334" cg="32.5"/>
<eng-data t="0.138" f="34.677" m="15.108" cg="32.5"/>
<eng-data t="0.252" f="33.8465" m="13.2836" cg="32.5"/>
<eng-data t="0.36" f="32.0816" m="11.6208" cg="32.5"/>
<eng-data t="0.63" f="29.8124" m="7.71797" cg="32.5"/>
<eng-data t="0.672" f="28.8301" m="7.14276" cg="32.5"/>
<eng-data t="0.77" f="27.3596" m="5.85675" cg="32.5"/>
<eng-data t="0.8" f="26.3903" m="5.48016" cg="32.5"/>
<eng-data t="0.9" f="24.2069" m="4.29851" cg="32.5"/>
<eng-data t="1.084" f="18.0681" m="2.48189" cg="32.5"/>
<eng-data t="1.134" f="16.8918" m="2.07366" cg="32.5"/>
<eng-data t="1.16" f="15.8701" m="1.87473" cg="32.5"/>
<eng-data t="1.2899" f="12.1921" m="1.02341" cg="32.5"/>
<eng-data t="1.3719" f="9.38065" m="0.610284" cg="32.5"/>
<eng-data t="1.5079" f="4.03928" m="0.184047" cg="32.5"/>
<eng-data t="1.5519" f="2.72185" m="0.114571" cg="32.5"/>
<eng-data t="1.6019" f="1.72082" m="0.0626935" cg="32.5"/>
<eng-data t="1.7579" f="0." m="0." cg="32.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="E23T" Type="reloadable" dia="29." len="124." initWt="103.9"
propWt="17.4" delays="5,8" auto-calc-mass="1" auto-calc-cg="1" avgThrust="22.498"
peakThrust="38.22" throatDia="0." exitDia="0." Itot="35.323" burn-time="1.57"
massFrac="16.75" Isp="207.01" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<comments>Aerotech E23 RASP.ENG file made from NAR published data
File produced July 4, 2000
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="17.4" cg="62."/>
<eng-data t="0.024" f="16.299" m="17.3037" cg="62."/>
<eng-data t="0.035" f="21.959" m="17.2" cg="62."/>
<eng-data t="0.067" f="30.785" m="16.7843" cg="62."/>
<eng-data t="0.09" f="35.774" m="16.4072" cg="62."/>
<eng-data t="0.153" f="37.577" m="15.2691" cg="62."/>
<eng-data t="0.2" f="38.22" m="14.3916" cg="62."/>
<eng-data t="0.24" f="37.357" m="13.647" cg="62."/>
<eng-data t="0.322" f="37.577" m="12.1336" cg="62."/>
<eng-data t="0.393" f="35.093" m="10.8628" cg="62."/>
<eng-data t="0.534" f="32.378" m="8.51964" cg="62."/>
<eng-data t="0.727" f="27.168" m="5.68905" cg="62."/>
<eng-data t="0.766" f="26.938" m="5.16932" cg="62."/>
<eng-data t="0.798" f="25.125" m="4.75898" cg="62."/>
<eng-data t="0.908" f="21.729" m="3.48956" cg="62."/>
<eng-data t="1.057" f="16.98" m="2.06898" cg="62."/>
<eng-data t="1.187" f="12.682" m="1.11923" cg="62."/>
<eng-data t="1.336" f="7.471" m="0.379638" cg="62."/>
<eng-data t="1.45" f="3.169" m="0.0808848" cg="62."/>
<eng-data t="1.497" f="1.584" m="0.0258633" cg="62."/>
<eng-data t="1.532" f="0.679" m="0.00635506" cg="62."/>
<eng-data t="1.57" f="0." m="0." cg="62."/>
</data>
</engine>
<engine mfg="Aerotech" code="E28T" Type="reloadable" dia="24." len="70." initWt="54.5"
propWt="18.4" delays="4,7" auto-calc-mass="1" auto-calc-cg="1" avgThrust="32.532"
peakThrust="50.52" throatDia="0." exitDia="0." Itot="39.689" burn-time="1.22"
massFrac="33.76" Isp="219.95" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<comments>Aerotech E28 RASP.ENG file made from NAR published data
File produced July 4, 2000
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="18.4" cg="35."/>
<eng-data t="0.01" f="29.862" m="18.3308" cg="35."/>
<eng-data t="0.018" f="45.139" m="18.1917" cg="35."/>
<eng-data t="0.038" f="47.562" m="17.7619" cg="35."/>
<eng-data t="0.081" f="50.52" m="16.7843" cg="35."/>
<eng-data t="0.106" f="48.953" m="16.2078" cg="35."/>
<eng-data t="0.146" f="48.263" m="15.3064" cg="35."/>
<eng-data t="0.161" f="48.953" m="14.9684" cg="35."/>
<eng-data t="0.197" f="48.953" m="14.1514" cg="35."/>
<eng-data t="0.242" f="47.562" m="13.1447" cg="35."/>
<eng-data t="0.313" f="46.18" m="11.6018" cg="35."/>
<eng-data t="0.411" f="43.057" m="9.57468" cg="35."/>
<eng-data t="0.494" f="40.624" m="7.96469" cg="35."/>
<eng-data t="0.527" f="39.583" m="7.35115" cg="35."/>
<eng-data t="0.542" f="40.274" m="7.07349" cg="35."/>
<eng-data t="0.562" f="38.542" m="6.70809" cg="35."/>
<eng-data t="0.633" f="36.46" m="5.47371" cg="35."/>
<eng-data t="0.683" f="34.377" m="4.6527" cg="35."/>
<eng-data t="0.743" f="31.244" m="3.74004" cg="35."/>
<eng-data t="0.799" f="29.162" m="2.95591" cg="35."/>
<eng-data t="0.877" f="26.038" m="1.95786" cg="35."/>
<eng-data t="0.97" f="20.832" m="0.947455" cg="35."/>
<eng-data t="1.006" f="17.359" m="0.628755" cg="35."/>
<eng-data t="1.046" f="11.462" m="0.361524" cg="35."/>
<eng-data t="1.089" f="6.943" m="0.178072" cg="35."/>
<eng-data t="1.132" f="3.819" m="0.0708017" cg="35."/>
<eng-data t="1.172" f="1.735" m="0.0193045" cg="35."/>
<eng-data t="1.22" f="0." m="0." cg="35."/>
</data>
</engine>
<engine mfg="Aerotech" code="E30T" Type="single-use" dia="24." len="70." initWt="43.3"
propWt="19.8" delays="4,7" auto-calc-mass="1" auto-calc-cg="1" avgThrust="32.387"
peakThrust="48.27" throatDia="0." exitDia="0." Itot="39.512" burn-time="1.22"
massFrac="45.73" Isp="203.49" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<comments>Aerotech E30 RASP.ENG file made from NAR published data
File produced July 4, 2000
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="19.8" cg="35."/>
<eng-data t="0.013" f="38.847" m="19.6735" cg="35."/>
<eng-data t="0.02" f="45.621" m="19.5253" cg="35."/>
<eng-data t="0.041" f="48.27" m="19.0313" cg="35."/>
<eng-data t="0.059" f="46.502" m="18.6039" cg="35."/>
<eng-data t="0.11" f="46.502" m="17.4154" cg="35."/>
<eng-data t="0.166" f="45.912" m="16.1187" cg="35."/>
<eng-data t="0.184" f="46.792" m="15.7006" cg="35."/>
<eng-data t="0.217" f="45.912" m="14.9341" cg="35."/>
<eng-data t="0.265" f="45.912" m="13.8298" cg="35."/>
<eng-data t="0.319" f="45.031" m="12.5993" cg="35."/>
<eng-data t="0.383" f="44.15" m="11.1692" cg="35."/>
<eng-data t="0.482" f="42.089" m="9.03006" cg="35."/>
<eng-data t="0.594" f="38.847" m="6.7588" cg="35."/>
<eng-data t="0.615" f="39.437" m="6.3469" cg="35."/>
<eng-data t="0.628" f="37.376" m="6.0967" cg="35."/>
<eng-data t="0.684" f="35.314" m="5.07677" cg="35."/>
<eng-data t="0.742" f="33.263" m="4.08018" cg="35."/>
<eng-data t="0.804" f="30.021" m="3.0971" cg="35."/>
<eng-data t="0.88" f="25.607" m="2.03781" cg="35."/>
<eng-data t="0.962" f="20.014" m="1.10049" cg="35."/>
<eng-data t="1.038" f="12.949" m="0.472798" cg="35."/>
<eng-data t="1.089" f="7.358" m="0.213307" cg="35."/>
<eng-data t="1.151" f="3.237" m="0.0487181" cg="35."/>
<eng-data t="1.186" f="1.176" m="0.0100183" cg="35."/>
<eng-data t="1.22" f="0." m="0." cg="35."/>
</data>
</engine>
<engine mfg="Aerotech" code="E6T-RC" Type="reloadable" dia="24." len="70." initWt="52.7"
propWt="21.5" delays="1000" auto-calc-mass="1" auto-calc-cg="1" avgThrust="5.266"
peakThrust="11.9" throatDia="0." exitDia="0." Itot="37.496" burn-time="7.12"
massFrac="40.8" Isp="177.84" tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1."
FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Aerotech E6TRC RASP.ENG file made from NAR published data
File produced July 4, 2000
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="21.5" cg="35."/>
<eng-data t="0.047" f="10.866" m="21.3536" cg="35."/>
<eng-data t="0.127" f="11.693" m="20.8362" cg="35."/>
<eng-data t="0.19" f="11.9" m="20.41" cg="35."/>
<eng-data t="0.316" f="11.622" m="19.5603" cg="35."/>
<eng-data t="0.522" f="10.593" m="18.2483" cg="35."/>
<eng-data t="0.743" f="9.287" m="16.9887" cg="35."/>
<eng-data t="0.996" f="7.842" m="15.7463" cg="35."/>
<eng-data t="1.249" f="6.19" m="14.7284" cg="35."/>
<eng-data t="1.47" f="5.296" m="14.0007" cg="35."/>
<eng-data t="1.787" f="4.747" m="13.0879" cg="35."/>
<eng-data t="2.372" f="4.471" m="11.5419" cg="35."/>
<eng-data t="3.02" f="4.403" m="9.8933" cg="35."/>
<eng-data t="3.747" f="4.264" m="8.08683" cg="35."/>
<eng-data t="4.49" f="4.403" m="6.24061" cg="35."/>
<eng-data t="5.375" f="4.333" m="4.02404" cg="35."/>
<eng-data t="6.087" f="4.264" m="2.26914" cg="35."/>
<eng-data t="6.719" f="4.264" m="0.723924" cg="35."/>
<eng-data t="6.877" f="4.196" m="0.3407" cg="35."/>
<eng-data t="6.957" f="3.783" m="0.157694" cg="35."/>
<eng-data t="7.004" f="2.614" m="0.0714955" cg="35."/>
<eng-data t="7.036" f="1.513" m="0.0336329" cg="35."/>
<eng-data t="7.083" f="0.55" m="0.00583432" cg="35."/>
<eng-data t="7.12" f="0." m="0." cg="35."/>
</data>
</engine>
<engine mfg="Aerotech" code="E7T-RC" Type="reloadable" dia="24." len="70." initWt="48.4"
propWt="17.1" delays="1000" auto-calc-mass="1" auto-calc-cg="1" avgThrust="5.405"
peakThrust="11.58" throatDia="0." exitDia="0." Itot="29.351" burn-time="5.43"
massFrac="35.33" Isp="175.03" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<comments>Aerotech E7TRC RASP.ENG file made from NAR published data
File produced July 4, 2000
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="17.1" cg="35."/>
<eng-data t="0.038" f="6.636" m="17.0265" cg="35."/>
<eng-data t="0.063" f="10.056" m="16.905" cg="35."/>
<eng-data t="0.087" f="11.019" m="16.7576" cg="35."/>
<eng-data t="0.134" f="11.42" m="16.4504" cg="35."/>
<eng-data t="0.206" f="11.58" m="15.968" cg="35."/>
<eng-data t="0.312" f="11.149" m="15.2662" cg="35."/>
<eng-data t="0.466" f="10.738" m="14.2843" cg="35."/>
<eng-data t="0.667" f="9.777" m="13.0831" cg="35."/>
<eng-data t="0.94" f="8.132" m="11.6589" cg="35."/>
<eng-data t="1.223" f="6.281" m="10.4707" cg="35."/>
<eng-data t="1.484" f="5.182" m="9.59916" cg="35."/>
<eng-data t="1.709" f="4.701" m="8.95139" cg="35."/>
<eng-data t="2.112" f="4.423" m="7.88027" cg="35."/>
<eng-data t="2.776" f="4.279" m="6.19708" cg="35."/>
<eng-data t="3.31" f="4.205" m="4.87734" cg="35."/>
<eng-data t="3.926" f="4.266" m="3.35727" cg="35."/>
<eng-data t="4.401" f="4.192" m="2.18694" cg="35."/>
<eng-data t="4.638" f="4.258" m="1.60356" cg="35."/>
<eng-data t="4.744" f="4.119" m="1.34489" cg="35."/>
<eng-data t="5.124" f="3.979" m="0.448479" cg="35."/>
<eng-data t="5.219" f="3.977" m="0.228306" cg="35."/>
<eng-data t="5.266" f="3.156" m="0.130646" cg="35."/>
<eng-data t="5.313" f="1.992" m="0.0601628" cg="35."/>
<eng-data t="5.36" f="0.965" m="0.0196776" cg="35."/>
<eng-data t="5.43" f="0." m="0." cg="35."/>
</data>
</engine>
<engine mfg="Aerotech" code="E12J-RC" Type="reloadable" dia="24." len="70."
initWt="59.4" propWt="30.3" delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="11.22" peakThrust="18.33" throatDia="0." exitDia="0." Itot="34.222"
burn-time="3.05" massFrac="51.01" Isp="115.17" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Aerotech E12JRC RASP.ENG file made from NAR published data
File produced July 4, 2000
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="30.3" cg="35."/>
<eng-data t="0.054" f="16.764" m="29.8992" cg="35."/>
<eng-data t="0.095" f="18.33" m="29.2623" cg="35."/>
<eng-data t="0.197" f="16.545" m="27.6875" cg="35."/>
<eng-data t="0.313" f="16.654" m="25.9826" cg="35."/>
<eng-data t="0.36" f="17.211" m="25.278" cg="35."/>
<eng-data t="0.401" f="16.316" m="24.6695" cg="35."/>
<eng-data t="0.442" f="17.55" m="24.0548" cg="35."/>
<eng-data t="0.476" f="16.206" m="23.5467" cg="35."/>
<eng-data t="0.578" f="16.316" m="22.0782" cg="35."/>
<eng-data t="0.666" f="16.764" m="20.7895" cg="35."/>
<eng-data t="0.7" f="15.649" m="20.3016" cg="35."/>
<eng-data t="0.768" f="16.316" m="19.3393" cg="35."/>
<eng-data t="0.89" f="16.097" m="17.5887" cg="35."/>
<eng-data t="1.019" f="15.649" m="15.7758" cg="35."/>
<eng-data t="1.162" f="14.983" m="13.8366" cg="35."/>
<eng-data t="1.23" f="14.983" m="12.9346" cg="35."/>
<eng-data t="1.25" f="13.968" m="12.6782" cg="35."/>
<eng-data t="1.291" f="14.754" m="12.1569" cg="35."/>
<eng-data t="1.332" f="13.749" m="11.6396" cg="35."/>
<eng-data t="1.373" f="14.197" m="11.1323" cg="35."/>
<eng-data t="1.434" f="13.53" m="10.3836" cg="35."/>
<eng-data t="1.488" f="13.749" m="9.73145" cg="35."/>
<eng-data t="1.597" f="12.635" m="8.45831" cg="35."/>
<eng-data t="1.726" f="11.401" m="7.08567" cg="35."/>
<eng-data t="1.828" f="10.615" m="6.09154" cg="35."/>
<eng-data t="1.889" f="9.613" m="5.54529" cg="35."/>
<eng-data t="1.957" f="9.613" m="4.96652" cg="35."/>
<eng-data t="1.998" f="8.495" m="4.63785" cg="35."/>
<eng-data t="2.093" f="8.607" m="3.91861" cg="35."/>
<eng-data t="2.277" f="7.042" m="2.6439" cg="35."/>
<eng-data t="2.487" f="5.813" m="1.44882" cg="35."/>
<eng-data t="3.05" f="0." m="0." cg="35."/>
</data>
</engine>
<engine mfg="Aerotech" code="F12J" Type="reloadable" dia="24." len="70." initWt="66.7"
propWt="30.3" delays="2,5" auto-calc-mass="1" auto-calc-cg="1" avgThrust="14.742"
peakThrust="23.54" throatDia="0." exitDia="0." Itot="43.195" burn-time="2.93"
massFrac="45.43" Isp="145.37" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<comments>Aerotech F12 RASP.ENG file made from NAR published data
File produced July 4, 2000
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="30.3" cg="35."/>
<eng-data t="0.037" f="20.894" m="30.0289" cg="35."/>
<eng-data t="0.054" f="22.152" m="29.7722" cg="35."/>
<eng-data t="0.101" f="22.152" m="29.0419" cg="35."/>
<eng-data t="0.148" f="22.571" m="28.3046" cg="35."/>
<eng-data t="0.165" f="23.409" m="28.0305" cg="35."/>
<eng-data t="0.2" f="22.421" m="27.4679" cg="35."/>
<eng-data t="0.281" f="22.142" m="26.2019" cg="35."/>
<eng-data t="0.369" f="22.132" m="24.8354" cg="35."/>
<eng-data t="0.474" f="22.271" m="23.2002" cg="35."/>
<eng-data t="0.526" f="23.54" m="22.3647" cg="35."/>
<eng-data t="0.549" f="21.982" m="21.9974" cg="35."/>
<eng-data t="0.637" f="22.122" m="20.6362" cg="35."/>
<eng-data t="0.724" f="21.842" m="19.2947" cg="35."/>
<eng-data t="0.8" f="21.413" m="18.1417" cg="35."/>
<eng-data t="0.823" f="22.251" m="17.7895" cg="35."/>
<eng-data t="0.846" f="20.714" m="17.4429" cg="35."/>
<eng-data t="0.881" f="21.553" m="16.924" cg="35."/>
<eng-data t="0.945" f="21.123" m="15.9661" cg="35."/>
<eng-data t="1.021" f="20.704" m="14.8511" cg="35."/>
<eng-data t="1.114" f="20.554" m="13.5054" cg="35."/>
<eng-data t="1.213" f="19.296" m="12.1217" cg="35."/>
<eng-data t="1.382" f="18.298" m="9.89334" cg="35."/>
<eng-data t="1.481" f="18.019" m="8.63232" cg="35."/>
<eng-data t="1.737" f="15.343" m="5.63682" cg="35."/>
<eng-data t="1.79" f="17.3" m="5.03003" cg="35."/>
<eng-data t="1.883" f="13.936" m="4.01116" cg="35."/>
<eng-data t="2.051" f="11.26" m="2.52654" cg="35."/>
<eng-data t="2.22" f="7.468" m="1.41646" cg="35."/>
<eng-data t="2.447" f="3.671" m="0.529609" cg="35."/>
<eng-data t="2.709" f="1.135" m="0.0879761" cg="35."/>
<eng-data t="2.93" f="0." m="0." cg="35."/>
</data>
</engine>
<engine mfg="Aerotech" code="F20W" Type="single-use" dia="29." len="83." initWt="74.6"
propWt="30." delays="4,7" auto-calc-mass="1" auto-calc-cg="1" avgThrust="22.602"
peakThrust="52.08" throatDia="0." exitDia="0." Itot="60.573" burn-time="2.68"
massFrac="40.21" Isp="205.89" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<data>
<eng-data t="0." f="0." m="30." cg="41.5"/>
<eng-data t="0.01" f="52.08" m="29.871" cg="41.5"/>
<eng-data t="0.03" f="49.81" m="29.3664" cg="41.5"/>
<eng-data t="0.06" f="46.98" m="28.6473" cg="41.5"/>
<eng-data t="0.1" f="45.56" m="27.7307" cg="41.5"/>
<eng-data t="0.15" f="44.49" m="26.6157" cg="41.5"/>
<eng-data t="0.18" f="45.55" m="25.9468" cg="41.5"/>
<eng-data t="0.21" f="43.42" m="25.2859" cg="41.5"/>
<eng-data t="0.24" f="43.78" m="24.6381" cg="41.5"/>
<eng-data t="0.32" f="43.77" m="22.9036" cg="41.5"/>
<eng-data t="0.36" f="44.11" m="22.0331" cg="41.5"/>
<eng-data t="0.44" f="43.04" m="20.3066" cg="41.5"/>
<eng-data t="0.45" f="40.58" m="20.0996" cg="41.5"/>
<eng-data t="0.53" f="39.86" m="18.506" cg="41.5"/>
<eng-data t="0.62" f="38.08" m="16.7689" cg="41.5"/>
<eng-data t="0.76" f="36.3" m="14.1903" cg="41.5"/>
<eng-data t="0.8" f="37.35" m="13.4608" cg="41.5"/>
<eng-data t="0.84" f="34.88" m="12.7453" cg="41.5"/>
<eng-data t="0.89" f="36.99" m="11.8554" cg="41.5"/>
<eng-data t="0.9" f="33.46" m="11.681" cg="41.5"/>
<eng-data t="1.03" f="30.61" m="9.6184" cg="41.5"/>
<eng-data t="1.06" f="32.02" m="9.15312" cg="41.5"/>
<eng-data t="1.09" f="29.55" m="8.69571" cg="41.5"/>
<eng-data t="1.23" f="26." m="6.76986" cg="41.5"/>
<eng-data t="1.32" f="22.45" m="5.69006" cg="41.5"/>
<eng-data t="1.35" f="23.16" m="5.35122" cg="41.5"/>
<eng-data t="1.36" f="21.39" m="5.2409" cg="41.5"/>
<eng-data t="1.58" f="16.42" m="3.18103" cg="41.5"/>
<eng-data t="1.8" f="11.1" m="1.68176" cg="41.5"/>
<eng-data t="2.01" f="6.48" m="0.767541" cg="41.5"/>
<eng-data t="2.19" f="3.63" m="0.316897" cg="41.5"/>
<eng-data t="2.39" f="1.13" m="0.0811496" cg="41.5"/>
<eng-data t="2.68" f="0." m="0." cg="41.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="F22J" Type="reloadable" dia="29." len="125." initWt="134.2"
propWt="46.3" delays="4,7" auto-calc-mass="1" auto-calc-cg="1" avgThrust="19.637"
peakThrust="31.15" throatDia="0." exitDia="0." Itot="64.997" burn-time="3.31"
massFrac="34.5" Isp="143.15" tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1."
FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Aerotech F22 RASP.ENG file made from NAR published data
File produced July 4, 2000
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="46.3" cg="62.5"/>
<eng-data t="0.014" f="11.527" m="46.2425" cg="62.5"/>
<eng-data t="0.075" f="20.126" m="45.5548" cg="62.5"/>
<eng-data t="0.157" f="26.572" m="44.191" cg="62.5"/>
<eng-data t="0.293" f="29.113" m="41.4936" cg="62.5"/>
<eng-data t="0.382" f="30.278" m="39.611" cg="62.5"/>
<eng-data t="0.45" f="29.69" m="38.1586" cg="62.5"/>
<eng-data t="0.539" f="30.667" m="36.2453" cg="62.5"/>
<eng-data t="0.614" f="30.089" m="34.6223" cg="62.5"/>
<eng-data t="0.662" f="31.15" m="33.5754" cg="62.5"/>
<eng-data t="0.771" f="30.478" m="31.1828" cg="62.5"/>
<eng-data t="0.948" f="29.89" m="27.3771" cg="62.5"/>
<eng-data t="0.996" f="28.714" m="26.3752" cg="62.5"/>
<eng-data t="1.078" f="28.136" m="24.7148" cg="62.5"/>
<eng-data t="1.187" f="27.738" m="22.5457" cg="62.5"/>
<eng-data t="1.289" f="26.761" m="20.5658" cg="62.5"/>
<eng-data t="1.337" f="26.96" m="19.6473" cg="62.5"/>
<eng-data t="1.412" f="25.984" m="18.2331" cg="62.5"/>
<eng-data t="1.474" f="25.008" m="17.107" cg="62.5"/>
<eng-data t="1.515" f="26.173" m="16.3596" cg="62.5"/>
<eng-data t="1.542" f="24.808" m="15.8694" cg="62.5"/>
<eng-data t="1.706" f="22.856" m="13.0852" cg="62.5"/>
<eng-data t="1.938" f="20.903" m="9.46934" cg="62.5"/>
<eng-data t="2.101" f="18.173" m="7.20075" cg="62.5"/>
<eng-data t="2.129" f="19.338" m="6.82667" cg="62.5"/>
<eng-data t="2.251" f="16.21" m="5.28201" cg="62.5"/>
<eng-data t="2.402" f="13.48" m="3.68523" cg="62.5"/>
<eng-data t="2.64" f="8.791" m="1.79735" cg="62.5"/>
<eng-data t="2.961" f="3.32" m="0.412687" cg="62.5"/>
<eng-data t="3.31" f="0." m="0." cg="62.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="F24W" Type="reloadable" dia="24." len="70." initWt="62.5"
propWt="19." delays="4,7" auto-calc-mass="1" auto-calc-cg="1" avgThrust="22.209"
peakThrust="40.95" throatDia="0." exitDia="0." Itot="47.306" burn-time="2.13"
massFrac="30.4" Isp="253.89" tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1."
FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Aerotech F24 RASP.ENG file made from NAR published data
File produced July 4, 2000
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="19." cg="35."/>
<eng-data t="0.033" f="15.942" m="18.8944" cg="35."/>
<eng-data t="0.112" f="40.146" m="18.0045" cg="35."/>
<eng-data t="0.125" f="40.95" m="17.7928" cg="35."/>
<eng-data t="0.18" f="40.427" m="16.894" cg="35."/>
<eng-data t="0.245" f="40.126" m="15.8425" cg="35."/>
<eng-data t="0.281" f="40.417" m="15.2602" cg="35."/>
<eng-data t="0.355" f="39.524" m="14.0722" cg="35."/>
<eng-data t="0.438" f="39.213" m="12.7598" cg="35."/>
<eng-data t="0.543" f="37.727" m="11.1374" cg="35."/>
<eng-data t="0.603" f="36.532" m="10.2427" cg="35."/>
<eng-data t="0.658" f="33.279" m="9.47159" cg="35."/>
<eng-data t="0.685" f="34.163" m="9.10591" cg="35."/>
<eng-data t="0.726" f="29.434" m="8.58227" cg="35."/>
<eng-data t="0.772" f="29.716" m="8.03586" cg="35."/>
<eng-data t="0.951" f="26.453" m="6.01675" cg="35."/>
<eng-data t="1.071" f="24.666" m="4.78485" cg="35."/>
<eng-data t="1.107" f="22.588" m="4.44323" cg="35."/>
<eng-data t="1.185" f="20.811" m="3.76342" cg="35."/>
<eng-data t="1.383" f="16.644" m="2.27411" cg="35."/>
<eng-data t="1.649" f="10.41" m="0.828926" cg="35."/>
<eng-data t="1.828" f="5.369" m="0.261717" cg="35."/>
<eng-data t="1.938" f="2.403" m="0.0900311" cg="35."/>
<eng-data t="1.988" f="1.806" m="0.0477682" cg="35."/>
<eng-data t="2.048" f="0.912" m="0.0150182" cg="35."/>
<eng-data t="2.13" f="0." m="0." cg="35."/>
</data>
</engine>
<engine mfg="Aerotech" code="F25W" Type="single-use" dia="29." len="98." initWt="97.2"
propWt="38.8" delays="4,6,9" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="26.307" peakThrust="57.631" throatDia="0." exitDia="0." Itot="70.767"
burn-time="2.69" massFrac="39.92" Isp="185.98" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>F25 Motor Thrust Curve created by Tim Van Milligan
for RockSim Users - www.rocksim.com
file produced March 2, 2005
Based on data supplied by Aerotech for the newer molded case F25.
</comments>
<data>
<eng-data t="0." f="0." m="38.8" cg="49."/>
<eng-data t="0.039" f="57.631" m="38.1838" cg="49."/>
<eng-data t="0.187" f="53.491" m="33.6753" cg="49."/>
<eng-data t="0.342" f="51.239" m="29.2252" cg="49."/>
<eng-data t="0.5" f="47.86" m="24.9328" cg="49."/>
<eng-data t="1." f="33.806" m="13.7388" cg="49."/>
<eng-data t="1.5" f="22.94" m="5.96068" cg="49."/>
<eng-data t="2." f="10.135" m="1.42709" cg="49."/>
<eng-data t="2.207" f="4.504" m="0.596372" cg="49."/>
<eng-data t="2.69" f="0." m="0." cg="49."/>
</data>
</engine>
<engine mfg="Aerotech" code="F27R" Type="single-use" dia="29." len="83." initWt="80."
propWt="28.4" delays="4,8" auto-calc-mass="1" auto-calc-cg="1" avgThrust="20.432"
peakThrust="35.968" throatDia="0." exitDia="0." Itot="49.546" burn-time="2.42"
massFrac="35.5" Isp="177.9" tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1."
FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Exported using ThrustCurveTool, www.ThrustGear.com
@File: 060603WF27Composite.txt, @Pts-I: 1001, @Pts-O: 32, @Sm: 5, @CO: 5%
@TI: 49.5446, @TIa: 49.299, @TIe: 0.0%, @ThMax: 36.2491, @ThAvg: 24.1799, @Tb: 2.049
</comments>
<data>
<eng-data t="0." f="0." m="28.4" cg="41.5"/>
<eng-data t="0." f="4.84718" m="28.4" cg="41.5"/>
<eng-data t="0.0125" f="15.5374" m="28.327" cg="41.5"/>
<eng-data t="0.0175" f="18.8183" m="28.2777" cg="41.5"/>
<eng-data t="0.025" f="22.5311" m="28.1889" cg="41.5"/>
<eng-data t="0.0325" f="25.2547" m="28.0861" cg="41.5"/>
<eng-data t="0.04" f="27.3204" m="27.9731" cg="41.5"/>
<eng-data t="0.0575" f="30.3657" m="27.6838" cg="41.5"/>
<eng-data t="0.0725" f="31.4597" m="27.418" cg="41.5"/>
<eng-data t="0.0975" f="32.2507" m="26.9615" cg="41.5"/>
<eng-data t="0.265" f="35.0238" m="23.732" cg="41.5"/>
<eng-data t="0.295" f="35.9203" m="23.122" cg="41.5"/>
<eng-data t="0.4675" f="35.9684" m="19.568" cg="41.5"/>
<eng-data t="0.59" f="35.065" m="17.0741" cg="41.5"/>
<eng-data t="0.8" f="32.0145" m="13.0368" cg="41.5"/>
<eng-data t="0.825" f="31.2773" m="12.5834" cg="41.5"/>
<eng-data t="0.8575" f="31.1102" m="12.0022" cg="41.5"/>
<eng-data t="0.9025" f="29.9308" m="11.215" cg="41.5"/>
<eng-data t="0.955" f="29.7244" m="10.3174" cg="41.5"/>
<eng-data t="1.045" f="27.2951" m="8.84664" cg="41.5"/>
<eng-data t="1.085" f="27.2663" m="8.22115" cg="41.5"/>
<eng-data t="1.1175" f="25.9881" m="7.72511" cg="41.5"/>
<eng-data t="1.1475" f="26.0014" m="7.27811" cg="41.5"/>
<eng-data t="1.235" f="23.2853" m="6.04212" cg="41.5"/>
<eng-data t="1.28" f="22.9001" m="5.44647" cg="41.5"/>
<eng-data t="1.3425" f="21.0771" m="4.65873" cg="41.5"/>
<eng-data t="1.52" f="17.256" m="2.70867" cg="41.5"/>
<eng-data t="1.8075" f="6.85478" m="0.722004" cg="41.5"/>
<eng-data t="1.9175" f="4.16387" m="0.37463" cg="41.5"/>
<eng-data t="2.05" f="1.78386" m="0.148769" cg="41.5"/>
<eng-data t="2.1775" f="0.488016" m="0.0657508" cg="41.5"/>
<eng-data t="2.4225" f="0.44385" m="0.000318018" cg="41.5"/>
<eng-data t="2.425" f="0." m="0." cg="41.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="F32T" Type="single-use" dia="24." len="90." initWt="65."
propWt="25.8" delays="4,6,8" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="31.14" peakThrust="58.76" throatDia="0." exitDia="0." Itot="56.924"
burn-time="1.83" massFrac="39.69" Isp="224.98" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Input by Tim Van Milligan based on NAR Certification document Jan 14, 2009
Created using Thrust Curve Tracer.</comments>
<data>
<eng-data t="0." f="0." m="25.8" cg="45."/>
<eng-data t="0.028" f="2.636" m="25.7833" cg="45."/>
<eng-data t="0.035" f="5.891" m="25.7697" cg="45."/>
<eng-data t="0.054" f="53.488" m="25.5141" cg="45."/>
<eng-data t="0.061" f="57.364" m="25.3382" cg="45."/>
<eng-data t="0.068" f="58.76" m="25.154" cg="45."/>
<eng-data t="0.089" f="58.76" m="24.5947" cg="45."/>
<eng-data t="0.114" f="55.504" m="23.9474" cg="45."/>
<eng-data t="0.177" f="51.783" m="22.4156" cg="45."/>
<eng-data t="0.24" f="49.302" m="20.9724" cg="45."/>
<eng-data t="0.319" f="47.132" m="19.246" cg="45."/>
<eng-data t="0.429" f="44.651" m="16.958" cg="45."/>
<eng-data t="0.545" f="41.86" m="14.6838" cg="45."/>
<eng-data t="0.611" f="41.55" m="13.4362" cg="45."/>
<eng-data t="0.627" f="40.465" m="13.1389" cg="45."/>
<eng-data t="0.676" f="40.155" m="12.2436" cg="45."/>
<eng-data t="0.772" f="38.76" m="10.5268" cg="45."/>
<eng-data t="0.904" f="36.744" m="8.26819" cg="45."/>
<eng-data t="1.005" f="34.884" m="6.62872" cg="45."/>
<eng-data t="1.119" f="32.403" m="4.89038" cg="45."/>
<eng-data t="1.212" f="30.543" m="3.56376" cg="45."/>
<eng-data t="1.277" f="28.527" m="2.69364" cg="45."/>
<eng-data t="1.298" f="27.597" m="2.42654" cg="45."/>
<eng-data t="1.322" f="26.512" m="2.13225" cg="45."/>
<eng-data t="1.338" f="24.961" m="1.94561" cg="45."/>
<eng-data t="1.385" f="21.55" m="1.45022" cg="45."/>
<eng-data t="1.445" f="15.969" m="0.940067" cg="45."/>
<eng-data t="1.51" f="10.543" m="0.549537" cg="45."/>
<eng-data t="1.597" f="5.581" m="0.231638" cg="45."/>
<eng-data t="1.676" f="2.636" m="0.0845292" cg="45."/>
<eng-data t="1.746" f="1.24" m="0.0230427" cg="45."/>
<eng-data t="1.828" f="0." m="0." cg="45."/>
</data>
</engine>
<engine mfg="Aerotech" code="F35W" Type="reloadable" dia="24." len="95." initWt="85."
propWt="30." delays="5,8,11" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="36.006" peakThrust="58.363" throatDia="0." exitDia="0." Itot="57.61"
burn-time="1.6" massFrac="35.29" Isp="195.82" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Curve fit of AT Instruction Sheet by C. Kobel 7/29/08</comments>
<data>
<eng-data t="0." f="0." m="30." cg="47.5"/>
<eng-data t="0.007" f="39.452" m="29.9281" cg="47.5"/>
<eng-data t="0.012" f="51.842" m="29.8092" cg="47.5"/>
<eng-data t="0.019" f="49.885" m="29.6238" cg="47.5"/>
<eng-data t="0.034" f="57.873" m="29.203" cg="47.5"/>
<eng-data t="0.048" f="58.363" m="28.7793" cg="47.5"/>
<eng-data t="0.058" f="57.221" m="28.4783" cg="47.5"/>
<eng-data t="0.077" f="54.45" m="27.9259" cg="47.5"/>
<eng-data t="0.098" f="54.939" m="27.3278" cg="47.5"/>
<eng-data t="0.106" f="53.961" m="27.1009" cg="47.5"/>
<eng-data t="0.201" f="53.472" m="24.4435" cg="47.5"/>
<eng-data t="0.299" f="53.309" m="21.7188" cg="47.5"/>
<eng-data t="0.398" f="52.005" m="19.0042" cg="47.5"/>
<eng-data t="0.498" f="52.005" m="16.296" cg="47.5"/>
<eng-data t="0.549" f="49.559" m="14.9474" cg="47.5"/>
<eng-data t="0.601" f="48.907" m="13.6142" cg="47.5"/>
<eng-data t="0.653" f="47.277" m="12.3119" cg="47.5"/>
<eng-data t="0.702" f="45.647" m="11.1264" cg="47.5"/>
<eng-data t="0.752" f="44.669" m="9.95059" cg="47.5"/>
<eng-data t="0.802" f="43.201" m="8.80664" cg="47.5"/>
<eng-data t="0.898" f="39.778" m="6.73251" cg="47.5"/>
<eng-data t="0.946" f="39.615" m="5.74027" cg="47.5"/>
<eng-data t="0.984" f="36.843" m="4.98378" cg="47.5"/>
<eng-data t="1.003" f="37.332" m="4.61683" cg="47.5"/>
<eng-data t="1.102" f="33.583" m="2.78886" cg="47.5"/>
<eng-data t="1.144" f="30.159" m="2.0918" cg="47.5"/>
<eng-data t="1.2" f="22.334" m="1.32641" cg="47.5"/>
<eng-data t="1.298" f="10.923" m="0.477807" cg="47.5"/>
<eng-data t="1.346" f="6.521" m="0.259793" cg="47.5"/>
<eng-data t="1.398" f="3.26" m="0.127365" cg="47.5"/>
<eng-data t="1.448" f="1.793" m="0.0615815" cg="47.5"/>
<eng-data t="1.497" f="0.978" m="0.0262284" cg="47.5"/>
<eng-data t="1.6" f="0." m="0." cg="47.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="F37W" Type="reloadable" dia="29." len="99." initWt="108.6"
propWt="28.2" delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="31.669" peakThrust="46.47" throatDia="0." exitDia="0." Itot="50.671"
burn-time="1.6" massFrac="25.97" Isp="183.23" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Aerotech F37 RASP.ENG file made from NAR published data
File produced July 4, 2000
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="28.2" cg="49.5"/>
<eng-data t="0.018" f="7.251" m="28.1637" cg="49.5"/>
<eng-data t="0.053" f="13.626" m="27.9604" cg="49.5"/>
<eng-data t="0.088" f="22.331" m="27.6102" cg="49.5"/>
<eng-data t="0.106" f="25.227" m="27.3719" cg="49.5"/>
<eng-data t="0.141" f="26.385" m="26.8693" cg="49.5"/>
<eng-data t="0.183" f="28.411" m="26.2289" cg="49.5"/>
<eng-data t="0.26" f="37.685" m="24.8127" cg="49.5"/>
<eng-data t="0.31" f="41.449" m="23.7117" cg="49.5"/>
<eng-data t="0.422" f="44.035" m="21.0475" cg="49.5"/>
<eng-data t="0.524" f="45.183" m="18.5152" cg="49.5"/>
<eng-data t="0.59" f="46.47" m="16.8319" cg="49.5"/>
<eng-data t="0.682" f="45.153" m="14.4863" cg="49.5"/>
<eng-data t="0.864" f="43.386" m="10.0023" cg="49.5"/>
<eng-data t="0.934" f="40.471" m="8.3689" cg="49.5"/>
<eng-data t="1.042" f="35.23" m="6.09388" cg="49.5"/>
<eng-data t="1.151" f="29.699" m="4.12452" cg="49.5"/>
<eng-data t="1.246" f="25.037" m="2.67756" cg="49.5"/>
<eng-data t="1.354" f="19.796" m="1.3302" cg="49.5"/>
<eng-data t="1.445" f="13.397" m="0.489683" cg="49.5"/>
<eng-data t="1.498" f="7.586" m="0.180223" cg="49.5"/>
<eng-data t="1.54" f="3.226" m="0.0538612" cg="49.5"/>
<eng-data t="1.6" f="0." m="0." cg="49.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="F39T" Type="reloadable" dia="24." len="70." initWt="60."
propWt="22.7" delays="3,6,9" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="37.337" peakThrust="59.47" throatDia="0." exitDia="0." Itot="49.658"
burn-time="1.33" massFrac="37.83" Isp="223.07" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Aerotech F39 RASP.ENG file made from NAR published data
File produced July 4, 2000
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="22.7" cg="35."/>
<eng-data t="0.01" f="45.057" m="22.597" cg="35."/>
<eng-data t="0.016" f="54.131" m="22.461" cg="35."/>
<eng-data t="0.046" f="58.321" m="21.6899" cg="35."/>
<eng-data t="0.079" f="59.47" m="20.8015" cg="35."/>
<eng-data t="0.103" f="58.311" m="20.1554" cg="35."/>
<eng-data t="0.13" f="57.253" m="19.4422" cg="35."/>
<eng-data t="0.172" f="55.491" m="18.3599" cg="35."/>
<eng-data t="0.235" f="53.738" m="16.7871" cg="35."/>
<eng-data t="0.321" f="51.271" m="14.723" cg="35."/>
<eng-data t="0.363" f="50.566" m="13.7454" cg="35."/>
<eng-data t="0.387" f="49.509" m="13.1965" cg="35."/>
<eng-data t="0.408" f="50.203" m="12.7179" cg="35."/>
<eng-data t="0.426" f="48.804" m="12.3106" cg="35."/>
<eng-data t="0.453" f="47.746" m="11.7147" cg="35."/>
<eng-data t="0.48" f="47.041" m="11.1298" cg="35."/>
<eng-data t="0.68" f="41.059" m="7.10253" cg="35."/>
<eng-data t="0.716" f="39.649" m="6.43844" cg="35."/>
<eng-data t="0.752" f="38.944" m="5.79176" cg="35."/>
<eng-data t="0.809" f="36.487" m="4.80905" cg="35."/>
<eng-data t="0.86" f="34.382" m="3.98296" cg="35."/>
<eng-data t="0.893" f="33.324" m="3.47228" cg="35."/>
<eng-data t="0.917" f="32.619" m="3.11055" cg="35."/>
<eng-data t="1." f="28.752" m="1.94631" cg="35."/>
<eng-data t="1.075" f="25.247" m="1.02065" cg="35."/>
<eng-data t="1.105" f="22.095" m="0.696033" cg="35."/>
<eng-data t="1.126" f="17.201" m="0.507421" cg="35."/>
<eng-data t="1.144" f="13.001" m="0.383167" cg="35."/>
<eng-data t="1.174" f="8.109" m="0.238419" cg="35."/>
<eng-data t="1.219" f="4.606" m="0.107641" cg="35."/>
<eng-data t="1.261" f="2.5" m="0.0394269" cg="35."/>
<eng-data t="1.33" f="0." m="0." cg="35."/>
</data>
</engine>
<engine mfg="Aerotech" code="F40W" Type="reloadable" dia="29." len="124." initWt="126."
propWt="40." delays="4,7,10" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="37.91" peakThrust="68.07" throatDia="0." exitDia="0." Itot="78.094"
burn-time="2.06" massFrac="31.75" Isp="199.08" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Aerotech F40 RASP.ENG file made from NAR published data
File produced July 4, 2000
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="40." cg="62."/>
<eng-data t="0.015" f="17.776" m="39.9317" cg="62."/>
<eng-data t="0.049" f="41.016" m="39.4198" cg="62."/>
<eng-data t="0.089" f="58.793" m="38.3973" cg="62."/>
<eng-data t="0.124" f="62.9" m="37.3065" cg="62."/>
<eng-data t="0.148" f="65.173" m="36.5193" cg="62."/>
<eng-data t="0.183" f="62.442" m="35.3754" cg="62."/>
<eng-data t="0.242" f="68.07" m="33.4034" cg="62."/>
<eng-data t="0.292" f="60.617" m="31.7556" cg="62."/>
<eng-data t="0.321" f="61.524" m="30.8484" cg="62."/>
<eng-data t="0.415" f="60.617" m="27.908" cg="62."/>
<eng-data t="0.524" f="58.334" m="24.5875" cg="62."/>
<eng-data t="0.741" f="52.412" m="18.4329" cg="62."/>
<eng-data t="0.87" f="48.314" m="15.1052" cg="62."/>
<eng-data t="0.889" f="49.221" m="14.6306" cg="62."/>
<eng-data t="0.914" f="47.397" m="14.012" cg="62."/>
<eng-data t="1.102" f="40.109" m="9.79883" cg="62."/>
<eng-data t="1.285" f="33.728" m="6.33834" cg="62."/>
<eng-data t="1.492" f="25.064" m="3.22159" cg="62."/>
<eng-data t="1.665" f="15.952" m="1.40435" cg="62."/>
<eng-data t="1.808" f="8.659" m="0.503032" cg="62."/>
<eng-data t="1.942" f="3.19" m="0.0964019" cg="62."/>
<eng-data t="2.06" f="0." m="0." cg="62."/>
</data>
</engine>
<engine mfg="Aerotech" code="F42T" Type="single-use" dia="29." len="83." initWt="76."
propWt="27." delays="4,8" auto-calc-mass="1" auto-calc-cg="1" avgThrust="38.004"
peakThrust="68.694" throatDia="0." exitDia="0." Itot="55.866" burn-time="1.47"
massFrac="35.53" Isp="210.99" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<comments>F42T Motor Thrust Curve created by Tim Van Milligan
for RockSim Users - www.rocksim.com
Based on data supplied by Aerotech prior to NAR certification.
</comments>
<data>
<eng-data t="0." f="0." m="27." cg="41.5"/>
<eng-data t="0.01" f="68.694" m="26.834" cg="41.5"/>
<eng-data t="0.029" f="65.879" m="26.2161" cg="41.5"/>
<eng-data t="0.202" f="62.5" m="20.8492" cg="41.5"/>
<eng-data t="0.511" f="51.802" m="12.3143" cg="41.5"/>
<eng-data t="0.739" f="43.356" m="7.07144" cg="41.5"/>
<eng-data t="0.993" f="31.532" m="2.47488" cg="41.5"/>
<eng-data t="1.02" f="29.279" m="2.07812" cg="41.5"/>
<eng-data t="1.072" f="23.086" m="1.42011" cg="41.5"/>
<eng-data t="1.199" f="9.572" m="0.41785" cg="41.5"/>
<eng-data t="1.262" f="4.505" m="0.203543" cg="41.5"/>
<eng-data t="1.319" f="2.815" m="0.102717" cg="41.5"/>
<eng-data t="1.47" f="0." m="0." cg="41.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="F44W" Type="single-use" dia="24." len="70." initWt="48."
propWt="19.7" delays="4,8" auto-calc-mass="1" auto-calc-cg="1" avgThrust="42.263"
peakThrust="65.218" throatDia="0." exitDia="0." Itot="42.178" burn-time="1."
massFrac="41.04" Isp="218.32" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<comments>F44W Economax</comments>
<data>
<eng-data t="0." f="0." m="19.7" cg="35."/>
<eng-data t="0.02" f="2.676" m="19.6875" cg="35."/>
<eng-data t="0.026" f="6.02" m="19.6753" cg="35."/>
<eng-data t="0.034" f="11.204" m="19.6431" cg="35."/>
<eng-data t="0.063" f="24.917" m="19.3985" cg="35."/>
<eng-data t="0.135" f="59.031" m="17.987" cg="35."/>
<eng-data t="0.15" f="61.372" m="17.5652" cg="35."/>
<eng-data t="0.2" f="63.212" m="16.1105" cg="35."/>
<eng-data t="0.299" f="65.218" m="13.1412" cg="35."/>
<eng-data t="0.4" f="65.051" m="10.0686" cg="35."/>
<eng-data t="0.5" f="63.379" m="7.06935" cg="35."/>
<eng-data t="0.6" f="58.529" m="4.22241" cg="35."/>
<eng-data t="0.668" f="55.017" m="2.41928" cg="35."/>
<eng-data t="0.686" f="53.68" m="1.96236" cg="35."/>
<eng-data t="0.687" f="54.014" m="1.93721" cg="35."/>
<eng-data t="0.7" f="49.165" m="1.62397" cg="35."/>
<eng-data t="0.719" f="43.813" m="1.21141" cg="35."/>
<eng-data t="0.774" f="22.074" m="0.365144" cg="35."/>
<eng-data t="0.795" f="13.211" m="0.1921" cg="35."/>
<eng-data t="0.812" f="7.86" m="0.108447" cg="35."/>
<eng-data t="0.825" f="4.515" m="0.0708773" cg="35."/>
<eng-data t="0.854" f="2.007" m="0.0267074" cg="35."/>
<eng-data t="0.899" f="0.167" m="0.00386099" cg="35."/>
<eng-data t="0.998" f="0." m="0." cg="35."/>
</data>
</engine>
<engine mfg="Aerotech" code="F50T" Type="single-use" dia="29." len="98." initWt="89.8"
propWt="33.6" delays="4,6,9" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="48.051" peakThrust="73.762" throatDia="0." exitDia="0." Itot="68.713"
burn-time="1.43" massFrac="37.42" Isp="208.54" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Aerotech F50 RASP.ENG file made by Tim Van Milligan
For RockSim www.RockSim.com
File Created March 2, 2005
Thrust curve supplied by Aerotech for the molded case F50T motors.
</comments>
<data>
<eng-data t="0." f="0." m="33.6" cg="49."/>
<eng-data t="0.013" f="73.762" m="33.3656" cg="49."/>
<eng-data t="0.0326" f="70.383" m="32.6748" cg="49."/>
<eng-data t="0.267" f="69.82" m="24.6398" cg="49."/>
<eng-data t="0.518" f="67.005" m="16.2431" cg="49."/>
<eng-data t="0.792" f="56.87" m="7.94451" cg="49."/>
<eng-data t="0.906" f="50.676" m="4.94694" cg="49."/>
<eng-data t="1." f="44.482" m="2.75997" cg="49."/>
<eng-data t="1.036" f="39.978" m="2.01657" cg="49."/>
<eng-data t="1.107" f="23.649" m="0.912055" cg="49."/>
<eng-data t="1.199" f="6.194" m="0.24078" cg="49."/>
<eng-data t="1.316" f="1.126" m="0.0313844" cg="49."/>
<eng-data t="1.43" f="0." m="0." cg="49."/>
</data>
</engine>
<engine mfg="Aerotech" code="F52T" Type="reloadable" dia="29." len="124." initWt="121.4"
propWt="36.6" delays="5,8,11" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="51.374" peakThrust="78.95" throatDia="0." exitDia="0." Itot="72.95"
burn-time="1.42" massFrac="30.15" Isp="203.25" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Aerotech F52 RASP.ENG file made from NAR published data
File produced July 4, 2000
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="36.6" cg="62."/>
<eng-data t="0.012" f="46.899" m="36.4588" cg="62."/>
<eng-data t="0.033" f="61.778" m="35.8863" cg="62."/>
<eng-data t="0.056" f="69.441" m="35.1292" cg="62."/>
<eng-data t="0.097" f="73.483" m="33.6592" cg="62."/>
<eng-data t="0.115" f="76.636" m="32.9814" cg="62."/>
<eng-data t="0.13" f="74.381" m="32.4131" cg="62."/>
<eng-data t="0.153" f="74.82" m="31.5523" cg="62."/>
<eng-data t="0.168" f="78.422" m="30.9757" cg="62."/>
<eng-data t="0.182" f="78.95" m="30.423" cg="62."/>
<eng-data t="0.206" f="77.963" m="29.4783" cg="62."/>
<eng-data t="0.238" f="77.504" m="28.2303" cg="62."/>
<eng-data t="0.258" f="73.892" m="27.4707" cg="62."/>
<eng-data t="0.314" f="72.974" m="25.4076" cg="62."/>
<eng-data t="0.39" f="72.046" m="22.6428" cg="62."/>
<eng-data t="0.428" f="70.679" m="21.2822" cg="62."/>
<eng-data t="0.501" f="65.699" m="18.7848" cg="62."/>
<eng-data t="0.565" f="62.975" m="16.719" cg="62."/>
<eng-data t="0.688" f="58.874" m="12.9593" cg="62."/>
<eng-data t="0.749" f="56.15" m="11.1992" cg="62."/>
<eng-data t="0.837" f="52.517" m="8.80035" cg="62."/>
<eng-data t="0.901" f="49.793" m="7.15779" cg="62."/>
<eng-data t="0.971" f="46.161" m="5.47285" cg="62."/>
<eng-data t="1.088" f="39.365" m="2.96266" cg="62."/>
<eng-data t="1.144" f="34.386" m="1.92661" cg="62."/>
<eng-data t="1.173" f="29.417" m="1.46246" cg="62."/>
<eng-data t="1.222" f="20.376" m="0.850406" cg="62."/>
<eng-data t="1.275" f="13.151" m="0.404654" cg="62."/>
<eng-data t="1.339" f="5.461" m="0.105843" cg="62."/>
<eng-data t="1.389" f="1.838" m="0.0142932" cg="62."/>
<eng-data t="1.42" f="0." m="0." cg="62."/>
</data>
</engine>
<engine mfg="Aerotech" code="F62T" Type="reloadable" dia="29." len="99." initWt="109."
propWt="25." delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="50.998" peakThrust="59.51" throatDia="0." exitDia="0." Itot="50.998"
burn-time="1." massFrac="22.94" Isp="208.02" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="25." cg="49.5"/>
<eng-data t="0." f="47.82" m="25." cg="49.5"/>
<eng-data t="0.2" f="59.51" m="19.7386" cg="49.5"/>
<eng-data t="0.5" f="59.51" m="10.9868" cg="49.5"/>
<eng-data t="0.6" f="55.56" m="8.16642" cg="49.5"/>
<eng-data t="0.7" f="51.55" m="5.54109" cg="49.5"/>
<eng-data t="0.8" f="43.63" m="3.20818" cg="49.5"/>
<eng-data t="0.9" f="43.63" m="1.06939" cg="49.5"/>
<eng-data t="1." f="0." m="0." cg="49.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="F63R" Type="reloadable" dia="24." len="95." initWt="81."
propWt="27.6" delays="10" auto-calc-mass="1" auto-calc-cg="1" avgThrust="61.927"
peakThrust="72.931" throatDia="0." exitDia="0." Itot="49.542" burn-time="0.8"
massFrac="34.07" Isp="183.04" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<comments>Curve Fit From AT Instruction Sheet by C. Kobel 5/2/18
delay times assumed by adjusting provided 10-sec delay grain
</comments>
<data>
<eng-data t="0." f="0." m="27.6" cg="47.5"/>
<eng-data t="0.002" f="52.189" m="27.5709" cg="47.5"/>
<eng-data t="0.018" f="59.103" m="27.0749" cg="47.5"/>
<eng-data t="0.035" f="63.341" m="26.4951" cg="47.5"/>
<eng-data t="0.063" f="66.686" m="25.481" cg="47.5"/>
<eng-data t="0.1" f="68.916" m="24.0834" cg="47.5"/>
<eng-data t="0.2" f="72.485" m="20.1446" cg="47.5"/>
<eng-data t="0.3" f="72.931" m="16.094" cg="47.5"/>
<eng-data t="0.35" f="71.816" m="14.078" cg="47.5"/>
<eng-data t="0.4" f="70.478" m="12.0962" cg="47.5"/>
<eng-data t="0.5" f="67.578" m="8.25062" cg="47.5"/>
<eng-data t="0.6" f="63.118" m="4.61005" cg="47.5"/>
<eng-data t="0.65" f="60.664" m="2.88606" cg="47.5"/>
<eng-data t="0.665" f="58.657" m="2.3875" cg="47.5"/>
<eng-data t="0.685" f="53.081" m="1.765" cg="47.5"/>
<eng-data t="0.7" f="48.175" m="1.34193" cg="47.5"/>
<eng-data t="0.8" f="0." m="0." cg="47.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="F67W" Type="single-use" dia="29." len="83." initWt="80."
propWt="30." delays="4,6,9" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="67.474" peakThrust="86.146" throatDia="0." exitDia="0." Itot="62.076"
burn-time="0.92" massFrac="37.5" Isp="211." tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="30." cg="41.5"/>
<eng-data t="0.002" f="66.662" m="29.9678" cg="41.5"/>
<eng-data t="0.008" f="71.441" m="29.7676" cg="41.5"/>
<eng-data t="0.016" f="74.505" m="29.4854" cg="41.5"/>
<eng-data t="0.039" f="77.936" m="28.6382" cg="41.5"/>
<eng-data t="0.068" f="80.632" m="27.527" cg="41.5"/>
<eng-data t="0.099" f="82.592" m="26.3043" cg="41.5"/>
<eng-data t="0.148" f="84.43" m="24.3267" cg="41.5"/>
<eng-data t="0.201" f="85.533" m="22.15" cg="41.5"/>
<eng-data t="0.257" f="86.146" m="19.8269" cg="41.5"/>
<eng-data t="0.298" f="86.023" m="18.1212" cg="41.5"/>
<eng-data t="0.399" f="84.185" m="13.9672" cg="41.5"/>
<eng-data t="0.483" f="82.96" m="10.5745" cg="41.5"/>
<eng-data t="0.499" f="82.347" m="9.93537" cg="41.5"/>
<eng-data t="0.568" f="80.019" m="7.22822" cg="41.5"/>
<eng-data t="0.601" f="78.794" m="5.96183" cg="41.5"/>
<eng-data t="0.625" f="77.936" m="5.05289" cg="41.5"/>
<eng-data t="0.654" f="78.058" m="3.95976" cg="41.5"/>
<eng-data t="0.672" f="75.853" m="3.29032" cg="41.5"/>
<eng-data t="0.687" f="71.073" m="2.75777" cg="41.5"/>
<eng-data t="0.7" f="67.52" m="2.3224" cg="41.5"/>
<eng-data t="0.714" f="62.005" m="1.88423" cg="41.5"/>
<eng-data t="0.731" f="53.06" m="1.41155" cg="41.5"/>
<eng-data t="0.748" f="44.482" m="1.01086" cg="41.5"/>
<eng-data t="0.764" f="35.659" m="0.701019" cg="41.5"/>
<eng-data t="0.778" f="26.836" m="0.489601" cg="41.5"/>
<eng-data t="0.789" f="20.954" m="0.362573" cg="41.5"/>
<eng-data t="0.797" f="18.013" m="0.287245" cg="41.5"/>
<eng-data t="0.812" f="12.499" m="0.176651" cg="41.5"/>
<eng-data t="0.832" f="7.107" m="0.0818995" cg="41.5"/>
<eng-data t="0.849" f="3.676" m="0.0376042" cg="41.5"/>
<eng-data t="0.87" f="1.225" m="0.0127344" cg="41.5"/>
<eng-data t="0.898" f="0.368" m="0.00195632" cg="41.5"/>
<eng-data t="0.92" f="0." m="0." cg="41.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="F23FJ" Type="single-use" dia="29." len="83." initWt="83.9"
propWt="33." delays="4,7" auto-calc-mass="1" auto-calc-cg="1" avgThrust="23.778"
peakThrust="48.7" throatDia="0." exitDia="0." Itot="52.787" burn-time="2.22"
massFrac="39.33" Isp="163.12" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<comments>F23FJ Motor Thrust Curve created by Tim Van Milligan
for RockSim Users - www.rocksim.com
file produced March 2, 2005
Based on data supplied by Aerotech for the newer molded case F23 econojet.
</comments>
<data>
<eng-data t="0." f="0." m="33." cg="41.5"/>
<eng-data t="0.03" f="48.7" m="32.5433" cg="41.5"/>
<eng-data t="0.05" f="43.11" m="31.9694" cg="41.5"/>
<eng-data t="0.08" f="41.41" m="31.1768" cg="41.5"/>
<eng-data t="0.1" f="42.26" m="30.6538" cg="41.5"/>
<eng-data t="0.13" f="40.84" m="29.8745" cg="41.5"/>
<eng-data t="0.17" f="39.42" m="28.871" cg="41.5"/>
<eng-data t="0.23" f="38.85" m="27.4031" cg="41.5"/>
<eng-data t="0.27" f="38.85" m="26.4316" cg="41.5"/>
<eng-data t="0.3" f="37.44" m="25.7162" cg="41.5"/>
<eng-data t="0.31" f="38.57" m="25.4786" cg="41.5"/>
<eng-data t="0.36" f="37.72" m="24.2863" cg="41.5"/>
<eng-data t="0.43" f="36.59" m="22.6604" cg="41.5"/>
<eng-data t="0.5" f="36.02" m="21.0717" cg="41.5"/>
<eng-data t="0.56" f="36.02" m="19.7206" cg="41.5"/>
<eng-data t="0.59" f="34.6" m="19.0584" cg="41.5"/>
<eng-data t="0.69" f="33.18" m="16.9397" cg="41.5"/>
<eng-data t="0.77" f="32.61" m="15.2946" cg="41.5"/>
<eng-data t="0.85" f="31.2" m="13.699" cg="41.5"/>
<eng-data t="0.94" f="29.5" m="11.9914" cg="41.5"/>
<eng-data t="1.04" f="27.79" m="10.2006" cg="41.5"/>
<eng-data t="1.18" f="24.39" m="7.91721" cg="41.5"/>
<eng-data t="1.2" f="25.24" m="7.60695" cg="41.5"/>
<eng-data t="1.25" f="22.97" m="6.85349" cg="41.5"/>
<eng-data t="1.37" f="20.98" m="5.20497" cg="41.5"/>
<eng-data t="1.53" f="16.73" m="3.31901" cg="41.5"/>
<eng-data t="1.69" f="12.48" m="1.85816" cg="41.5"/>
<eng-data t="1.83" f="9.07" m="0.915125" cg="41.5"/>
<eng-data t="1.95" f="5.11" m="0.383248" cg="41.5"/>
<eng-data t="2.07" f="2.27" m="0.106432" cg="41.5"/>
<eng-data t="2.22" f="0." m="0." cg="41.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="F26FJ" Type="single-use" dia="29." len="98." initWt="100.7"
propWt="43.1" delays="6,9" auto-calc-mass="1" auto-calc-cg="1" avgThrust="23.947"
peakThrust="38.289" throatDia="0." exitDia="0." Itot="62.501" burn-time="2.61"
massFrac="42.8" Isp="147.87" tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1."
FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>F26FJ Motor Thrust Curve created by Tim Van Milligan
for RockSim Users - www.rocksim.com
File created March 2, 2005
Based on data supplied by Aerotech prior to NAR certification.
</comments>
<data>
<eng-data t="0." f="0." m="43.1" cg="49."/>
<eng-data t="0.041" f="38.289" m="42.5587" cg="49."/>
<eng-data t="0.114" f="36.318" m="40.6809" cg="49."/>
<eng-data t="0.293" f="34.347" m="36.3196" cg="49."/>
<eng-data t="0.497" f="32.939" m="31.5868" cg="49."/>
<eng-data t="0.774" f="32.376" m="25.3487" cg="49."/>
<eng-data t="1." f="31.25" m="20.3907" cg="49."/>
<eng-data t="1.254" f="28.716" m="15.139" cg="49."/>
<eng-data t="1.498" f="25.338" m="10.5915" cg="49."/>
<eng-data t="1.743" f="22.241" m="6.57226" cg="49."/>
<eng-data t="2.003" f="17.737" m="2.98837" cg="49."/>
<eng-data t="2.077" f="15.484" m="2.14074" cg="49."/>
<eng-data t="2.304" f="5.349" m="0.510176" cg="49."/>
<eng-data t="2.484" f="1.689" m="0.0733771" cg="49."/>
<eng-data t="2.61" f="0." m="0." cg="49."/>
</data>
</engine>
<engine mfg="Aerotech" code="F30FJ" Type="single-use" dia="24." len="90." initWt="70."
propWt="31.8" delays="4,6,8" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="29.452" peakThrust="38.241" throatDia="0." exitDia="0." Itot="47.123"
burn-time="1.6" massFrac="45.43" Isp="151.11" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>From AT Instruction Sheet by C. Kobel 1/4/11</comments>
<data>
<eng-data t="0." f="0." m="31.8" cg="45."/>
<eng-data t="0.056" f="22.706" m="31.371" cg="45."/>
<eng-data t="0.102" f="34.315" m="30.4859" cg="45."/>
<eng-data t="0.134" f="36.363" m="29.7228" cg="45."/>
<eng-data t="0.2" f="36.876" m="28.0918" cg="45."/>
<eng-data t="0.3" f="36.705" m="25.6091" cg="45."/>
<eng-data t="0.4" f="37.217" m="23.1149" cg="45."/>
<eng-data t="0.5" f="38.241" m="20.5688" cg="45."/>
<eng-data t="0.6" f="37.9" m="17.9997" cg="45."/>
<eng-data t="0.7" f="37.9" m="15.4421" cg="45."/>
<eng-data t="0.8" f="37.217" m="12.9075" cg="45."/>
<eng-data t="0.9" f="36.363" m="10.4248" cg="45."/>
<eng-data t="1." f="35.168" m="8.01128" cg="45."/>
<eng-data t="1.1" f="33.291" m="5.70137" cg="45."/>
<eng-data t="1.175" f="32.608" m="4.03373" cg="45."/>
<eng-data t="1.2" f="31.413" m="3.49369" cg="45."/>
<eng-data t="1.26" f="26.974" m="2.31165" cg="45."/>
<eng-data t="1.3" f="22.706" m="1.64114" cg="45."/>
<eng-data t="1.4" f="9.219" m="0.563943" cg="45."/>
<eng-data t="1.453" f="5.805" m="0.295269" cg="45."/>
<eng-data t="1.5" f="4.097" m="0.138239" cg="45."/>
<eng-data t="1.6" f="0." m="0." cg="45."/>
</data>
</engine>
<engine mfg="Aerotech" code="F51NT" Type="reloadable" dia="24." len="95." initWt="82."
propWt="26.5" delays="10" auto-calc-mass="1" auto-calc-cg="1" avgThrust="50.339"
peakThrust="71.343" throatDia="0." exitDia="0." Itot="52.856" burn-time="1.05"
massFrac="32.32" Isp="203.39" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<comments>Curve Fit From AT Instruction Sheet by C. Kobel 5/2/18
delay times assumed by adjusting provided 10-sec delay grain
</comments>
<data>
<eng-data t="0." f="0." m="26.5" cg="47.5"/>
<eng-data t="0.004" f="68.776" m="26.431" cg="47.5"/>
<eng-data t="0.013" f="69.033" m="26.1201" cg="47.5"/>
<eng-data t="0.018" f="70.316" m="25.9455" cg="47.5"/>
<eng-data t="0.027" f="71.343" m="25.6259" cg="47.5"/>
<eng-data t="0.06" f="71.343" m="24.4455" cg="47.5"/>
<eng-data t="0.1" f="70.829" m="23.0199" cg="47.5"/>
<eng-data t="0.2" f="68.52" m="19.5267" cg="47.5"/>
<eng-data t="0.3" f="66.723" m="16.1365" cg="47.5"/>
<eng-data t="0.4" f="64.414" m="12.8492" cg="47.5"/>
<eng-data t="0.5" f="62.361" m="9.67117" cg="47.5"/>
<eng-data t="0.6" f="59.281" m="6.62186" cg="47.5"/>
<eng-data t="0.7" f="54.918" m="3.75913" cg="47.5"/>
<eng-data t="0.722" f="53.635" m="3.16047" cg="47.5"/>
<eng-data t="0.738" f="52.352" m="2.73537" cg="47.5"/>
<eng-data t="0.757" f="48.759" m="2.25379" cg="47.5"/>
<eng-data t="0.775" f="44.397" m="1.83345" cg="47.5"/>
<eng-data t="0.8" f="36.441" m="1.32684" cg="47.5"/>
<eng-data t="0.85" f="18.477" m="0.638498" cg="47.5"/>
<eng-data t="0.875" f="12.318" m="0.445507" cg="47.5"/>
<eng-data t="0.9" f="8.982" m="0.31202" cg="47.5"/>
<eng-data t="0.95" f="4.876" m="0.138325" cg="47.5"/>
<eng-data t="1." f="3.08" m="0.0386046" cg="47.5"/>
<eng-data t="1.05" f="0." m="0." cg="47.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="F62FJ" Type="reloadable" dia="24." len="95." initWt="87."
propWt="32.2" delays="10" auto-calc-mass="1" auto-calc-cg="1" avgThrust="60.193"
peakThrust="72.196" throatDia="0." exitDia="0." Itot="46.95" burn-time="0.78"
massFrac="37.01" Isp="148.68" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<comments>Curve Fit From AT Instruction Sheet by C. Kobel 5/2/18
delay times assumed by adjusting provided 10-sec delay grain
</comments>
<data>
<eng-data t="0." f="0." m="32.2" cg="47.5"/>
<eng-data t="0.002" f="52.854" m="32.1638" cg="47.5"/>
<eng-data t="0.018" f="54.428" m="31.5751" cg="47.5"/>
<eng-data t="0.035" f="55.553" m="30.934" cg="47.5"/>
<eng-data t="0.059" f="56.902" m="30.0085" cg="47.5"/>
<eng-data t="0.1" f="59.151" m="28.3768" cg="47.5"/>
<eng-data t="0.2" f="63.65" m="24.1658" cg="47.5"/>
<eng-data t="0.3" f="68.148" m="19.6462" cg="47.5"/>
<eng-data t="0.4" f="71.521" m="14.8567" cg="47.5"/>
<eng-data t="0.459" f="72.196" m="11.949" cg="47.5"/>
<eng-data t="0.5" f="72.196" m="9.91896" cg="47.5"/>
<eng-data t="0.541" f="70.622" m="7.911" cg="47.5"/>
<eng-data t="0.584" f="68.148" m="5.86478" cg="47.5"/>
<eng-data t="0.6" f="67.923" m="5.1182" cg="47.5"/>
<eng-data t="0.618" f="67.248" m="4.28386" cg="47.5"/>
<eng-data t="0.634" f="65.674" m="3.55456" cg="47.5"/>
<eng-data t="0.654" f="60.726" m="2.68767" cg="47.5"/>
<eng-data t="0.7" f="40.034" m="1.09826" cg="47.5"/>
<eng-data t="0.78" f="0." m="0." cg="47.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="F13J-RC" Type="reloadable" dia="32." len="107."
initWt="110.5" propWt="32.3" delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="12.17" peakThrust="19.98" throatDia="0." exitDia="0." Itot="62.067"
burn-time="5.1" massFrac="29.23" Isp="195.95" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Aerotech F13RCJ RASP.ENG file made from NAR published data
File produced July 4, 2000
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="32.3" cg="53.5"/>
<eng-data t="0.048" f="15.309" m="32.1088" cg="53.5"/>
<eng-data t="0.084" f="18.629" m="31.7909" cg="53.5"/>
<eng-data t="0.143" f="19.98" m="31.1982" cg="53.5"/>
<eng-data t="0.311" f="18.968" m="29.4956" cg="53.5"/>
<eng-data t="0.538" f="18.172" m="27.3019" cg="53.5"/>
<eng-data t="0.729" f="17.138" m="25.5471" cg="53.5"/>
<eng-data t="0.992" f="15.428" m="23.3185" cg="53.5"/>
<eng-data t="1.279" f="13.828" m="21.1337" cg="53.5"/>
<eng-data t="1.673" f="12.456" m="18.4391" cg="53.5"/>
<eng-data t="1.984" f="11.879" m="16.4698" cg="53.5"/>
<eng-data t="2.044" f="12.227" m="16.0935" cg="53.5"/>
<eng-data t="2.139" f="11.313" m="15.5116" cg="53.5"/>
<eng-data t="2.378" f="11.193" m="14.112" cg="53.5"/>
<eng-data t="2.51" f="11.084" m="13.3469" cg="53.5"/>
<eng-data t="2.558" f="12.108" m="13.0572" cg="53.5"/>
<eng-data t="2.641" f="10.855" m="12.5613" cg="53.5"/>
<eng-data t="2.976" f="10.736" m="10.6793" cg="53.5"/>
<eng-data t="3.49" f="10.627" m="7.82211" cg="53.5"/>
<eng-data t="3.873" f="10.507" m="5.71596" cg="53.5"/>
<eng-data t="3.992" f="10.965" m="5.0511" cg="53.5"/>
<eng-data t="4.028" f="10.627" m="4.84884" cg="53.5"/>
<eng-data t="4.41" f="10.507" m="2.74819" cg="53.5"/>
<eng-data t="4.625" f="10.736" m="1.55979" cg="53.5"/>
<eng-data t="4.769" f="9.941" m="0.785045" cg="53.5"/>
<eng-data t="4.829" f="8.684" m="0.49427" cg="53.5"/>
<eng-data t="4.865" f="6.742" m="0.349771" cg="53.5"/>
<eng-data t="4.96" f="3.199" m="0.104039" cg="53.5"/>
<eng-data t="5.02" f="1.485" m="0.0309119" cg="53.5"/>
<eng-data t="5.1" f="0." m="0." cg="53.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="F16J-RC" Type="reloadable" dia="32." len="107."
initWt="140.4" propWt="62.5" delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="13.266" peakThrust="26.35" throatDia="0." exitDia="0." Itot="75.483"
burn-time="5.69" massFrac="44.52" Isp="123.15" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Aerotech F16RCJ RASP.ENG file made from NAR published data
File produced July 4, 2000
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="62.5" cg="53.5"/>
<eng-data t="0.046" f="26.35" m="61.9982" cg="53.5"/>
<eng-data t="0.116" f="22.388" m="60.5858" cg="53.5"/>
<eng-data t="0.139" f="21.374" m="60.1691" cg="53.5"/>
<eng-data t="0.185" f="21.886" m="59.3452" cg="53.5"/>
<eng-data t="0.22" f="20.54" m="58.7305" cg="53.5"/>
<eng-data t="0.301" f="19.696" m="57.3812" cg="53.5"/>
<eng-data t="0.498" f="18.35" m="54.2783" cg="53.5"/>
<eng-data t="0.579" f="19.194" m="53.0193" cg="53.5"/>
<eng-data t="0.637" f="16.492" m="52.1624" cg="53.5"/>
<eng-data t="0.718" f="18.35" m="50.994" cg="53.5"/>
<eng-data t="0.834" f="18.35" m="49.2315" cg="53.5"/>
<eng-data t="0.95" f="18.35" m="47.4691" cg="53.5"/>
<eng-data t="1.054" f="19.194" m="45.8526" cg="53.5"/>
<eng-data t="1.147" f="17.848" m="44.4264" cg="53.5"/>
<eng-data t="1.181" f="18.853" m="43.9098" cg="53.5"/>
<eng-data t="1.263" f="17.336" m="42.6813" cg="53.5"/>
<eng-data t="1.436" f="18.009" m="40.1498" cg="53.5"/>
<eng-data t="1.633" f="17.165" m="37.2811" cg="53.5"/>
<eng-data t="1.784" f="17.336" m="35.1243" cg="53.5"/>
<eng-data t="1.865" f="18.682" m="33.9165" cg="53.5"/>
<eng-data t="1.934" f="16.834" m="32.9019" cg="53.5"/>
<eng-data t="1.981" f="17.336" m="32.2371" cg="53.5"/>
<eng-data t="2.178" f="16.332" m="29.4912" cg="53.5"/>
<eng-data t="2.375" f="16.332" m="26.8272" cg="53.5"/>
<eng-data t="2.502" f="18.18" m="25.0126" cg="53.5"/>
<eng-data t="2.664" f="15.659" m="22.7431" cg="53.5"/>
<eng-data t="2.896" f="15.488" m="19.7515" cg="53.5"/>
<eng-data t="3.29" f="13.8" m="14.9742" cg="53.5"/>
<eng-data t="3.718" f="11.611" m="10.4716" cg="53.5"/>
<eng-data t="4.181" f="9.426" m="6.4392" cg="53.5"/>
<eng-data t="4.888" f="5.891" m="1.95597" cg="53.5"/>
<eng-data t="5.69" f="0." m="0." cg="53.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="F23SK-RC" Type="reloadable" dia="32." len="107."
initWt="128.7" propWt="37.8" delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="19.435" peakThrust="36." throatDia="0." exitDia="0." Itot="67.44"
burn-time="3.47" massFrac="29.37" Isp="181.93" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Aerotech F23RCWSK RASP.ENG file made from NAR published data
File produced July 4, 2000
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="37.8" cg="53.5"/>
<eng-data t="0.042" f="22.644" m="37.5335" cg="53.5"/>
<eng-data t="0.133" f="28.191" m="36.237" cg="53.5"/>
<eng-data t="0.161" f="27.261" m="35.8019" cg="53.5"/>
<eng-data t="0.189" f="29.57" m="35.3559" cg="53.5"/>
<eng-data t="0.252" f="31.419" m="34.2791" cg="53.5"/>
<eng-data t="0.343" f="32.578" m="32.647" cg="53.5"/>
<eng-data t="0.399" f="32.348" m="31.6281" cg="53.5"/>
<eng-data t="0.441" f="33.737" m="30.8502" cg="53.5"/>
<eng-data t="0.476" f="30.729" m="30.2179" cg="53.5"/>
<eng-data t="0.539" f="33.507" m="29.0837" cg="53.5"/>
<eng-data t="0.609" f="34.197" m="27.7556" cg="53.5"/>
<eng-data t="0.777" f="34.886" m="24.503" cg="53.5"/>
<eng-data t="0.826" f="34.656" m="23.548" cg="53.5"/>
<eng-data t="0.896" f="36." m="22.1619" cg="53.5"/>
<eng-data t="0.938" f="34.656" m="21.3302" cg="53.5"/>
<eng-data t="1.015" f="34.656" m="19.8345" cg="53.5"/>
<eng-data t="1.071" f="34.197" m="18.754" cg="53.5"/>
<eng-data t="1.12" f="33.038" m="17.8307" cg="53.5"/>
<eng-data t="1.218" f="32.578" m="16.0286" cg="53.5"/>
<eng-data t="1.267" f="29.81" m="15.1718" cg="53.5"/>
<eng-data t="1.351" f="29.34" m="13.7794" cg="53.5"/>
<eng-data t="1.393" f="27.731" m="13.1076" cg="53.5"/>
<eng-data t="1.54" f="26.802" m="10.861" cg="53.5"/>
<eng-data t="1.645" f="24.263" m="9.35836" cg="53.5"/>
<eng-data t="1.799" f="21.255" m="7.39386" cg="53.5"/>
<eng-data t="1.862" f="19.866" m="6.66784" cg="53.5"/>
<eng-data t="2.051" f="15.479" m="4.7957" cg="53.5"/>
<eng-data t="2.317" f="11.552" m="2.78063" cg="53.5"/>
<eng-data t="2.618" f="6.7" m="1.24097" cg="53.5"/>
<eng-data t="2.884" f="3.234" m="0.500425" cg="53.5"/>
<eng-data t="3.185" f="1.386" m="0.110702" cg="53.5"/>
<eng-data t="3.47" f="0." m="0." cg="53.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="G142" Type="reloadable" dia="29." len="113." initWt="97.6"
propWt="38.6" delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="93.892" peakThrust="173.384" throatDia="0." exitDia="0." Itot="84.597"
burn-time="0.9" massFrac="39.55" Isp="223.48" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>@File: G142_Typical.txt, @Pts-I: 451, @Pts-O: 32, @Sm: 0, @CO: 5%
@TI: 84.5422, @TIa: 84.2303, @TIe: 0.0%, @ThMax: 173.4408, @ThAvg: 135.8554, @Tb: 0.62
Exported using ThrustCurveTool, www.ThrustGear.com
</comments>
<data>
<eng-data t="0." f="0." m="38.6" cg="56.5"/>
<eng-data t="0.016" f="4.06052" m="38.5852" cg="56.5"/>
<eng-data t="0.018" f="6.53754" m="38.5803" cg="56.5"/>
<eng-data t="0.02" f="13.4407" m="38.5712" cg="56.5"/>
<eng-data t="0.022" f="24.4211" m="38.554" cg="56.5"/>
<eng-data t="0.024" f="43.7388" m="38.5229" cg="56.5"/>
<eng-data t="0.026" f="72.8495" m="38.4697" cg="56.5"/>
<eng-data t="0.028" f="106.943" m="38.3876" cg="56.5"/>
<eng-data t="0.03" f="132.008" m="38.2786" cg="56.5"/>
<eng-data t="0.032" f="141.542" m="38.1538" cg="56.5"/>
<eng-data t="0.034" f="147.684" m="38.0218" cg="56.5"/>
<eng-data t="0.038" f="154.115" m="37.7464" cg="56.5"/>
<eng-data t="0.054" f="165.567" m="36.5795" cg="56.5"/>
<eng-data t="0.076" f="166.321" m="34.9137" cg="56.5"/>
<eng-data t="0.084" f="168.761" m="34.3021" cg="56.5"/>
<eng-data t="0.118" f="172.94" m="31.6516" cg="56.5"/>
<eng-data t="0.15" f="173.384" m="29.1233" cg="56.5"/>
<eng-data t="0.224" f="171.843" m="23.2951" cg="56.5"/>
<eng-data t="0.3" f="164.78" m="17.4585" cg="56.5"/>
<eng-data t="0.372" f="156.654" m="12.1786" cg="56.5"/>
<eng-data t="0.418" f="148.959" m="8.97132" cg="56.5"/>
<eng-data t="0.432" f="144.99" m="8.03245" cg="56.5"/>
<eng-data t="0.452" f="137.096" m="6.74535" cg="56.5"/>
<eng-data t="0.518" f="96.8779" m="3.22233" cg="56.5"/>
<eng-data t="0.568" f="69.3937" m="1.32567" cg="56.5"/>
<eng-data t="0.576" f="63.1618" m="1.08374" cg="56.5"/>
<eng-data t="0.618" f="21.4754" m="0.272755" cg="56.5"/>
<eng-data t="0.628" f="13.5705" m="0.192802" cg="56.5"/>
<eng-data t="0.64" f="7.98504" m="0.133789" cg="56.5"/>
<eng-data t="0.652" f="2.92169" m="0.10393" cg="56.5"/>
<eng-data t="0.672" f="0.966347" m="0.0861899" cg="56.5"/>
<eng-data t="0.9" f="0.687625" m="0.000156875" cg="56.5"/>
<eng-data t="0.901" f="0." m="0." cg="56.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="G25W" Type="reloadable" dia="29." len="124." initWt="119.7"
propWt="62.5" delays="10" auto-calc-mass="1" auto-calc-cg="1" avgThrust="22.17"
peakThrust="41.18" throatDia="0." exitDia="0." Itot="117.499" burn-time="5.3"
massFrac="52.21" Isp="191.71" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<comments>Aerotech G25 RASP.ENG file made from NAR published data
File produced July 4, 2000
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="62.5" cg="62."/>
<eng-data t="0.035" f="30.499" m="62.2161" cg="62."/>
<eng-data t="0.047" f="36.712" m="62.0016" cg="62."/>
<eng-data t="0.059" f="41.18" m="61.753" cg="62."/>
<eng-data t="0.13" f="40.669" m="60.2074" cg="62."/>
<eng-data t="0.177" f="38.969" m="59.212" cg="62."/>
<eng-data t="0.295" f="38.969" m="56.766" cg="62."/>
<eng-data t="0.343" f="40.947" m="55.7458" cg="62."/>
<eng-data t="0.413" f="40.38" m="54.2317" cg="62."/>
<eng-data t="0.437" f="38.69" m="53.727" cg="62."/>
<eng-data t="0.484" f="39.824" m="52.7456" cg="62."/>
<eng-data t="0.532" f="37.845" m="51.7541" cg="62."/>
<eng-data t="0.65" f="37.557" m="49.3877" cg="62."/>
<eng-data t="0.721" f="38.969" m="47.9427" cg="62."/>
<eng-data t="0.803" f="38.69" m="46.249" cg="62."/>
<eng-data t="0.85" f="37.279" m="45.2994" cg="62."/>
<eng-data t="0.98" f="39.535" m="42.6436" cg="62."/>
<eng-data t="1.063" f="36.434" m="40.9666" cg="62."/>
<eng-data t="1.098" f="38.124" m="40.2726" cg="62."/>
<eng-data t="1.252" f="37.845" m="37.1611" cg="62."/>
<eng-data t="1.37" f="37.279" m="34.8034" cg="62."/>
<eng-data t="1.583" f="37." m="30.5956" cg="62."/>
<eng-data t="1.819" f="35.3" m="26.0576" cg="62."/>
<eng-data t="1.984" f="33.61" m="23.0336" cg="62."/>
<eng-data t="2.185" f="31.344" m="19.5613" cg="62."/>
<eng-data t="2.315" f="28.809" m="17.4815" cg="62."/>
<eng-data t="2.622" f="24.286" m="13.1463" cg="62."/>
<eng-data t="3.024" f="18.917" m="8.52727" cg="62."/>
<eng-data t="3.39" f="13.838" m="5.33886" cg="62."/>
<eng-data t="3.839" f="7.624" m="2.77596" cg="62."/>
<eng-data t="4.323" f="4.518" m="1.213" cg="62."/>
<eng-data t="4.783" f="2.541" m="0.34939" cg="62."/>
<eng-data t="5.3" f="0." m="0." cg="62."/>
</data>
</engine>
<engine mfg="Aerotech" code="G33J" Type="reloadable" dia="29." len="124." initWt="159.3"
propWt="72.2" delays="5,7" auto-calc-mass="1" auto-calc-cg="1" avgThrust="30.09"
peakThrust="50.92" throatDia="0." exitDia="0." Itot="98.394" burn-time="3.27"
massFrac="45.32" Isp="138.97" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<comments>Aerotech G33 RASP.ENG file made from NAR published data
File produced July 4, 2000
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="72.2" cg="62."/>
<eng-data t="0.027" f="22.642" m="71.9757" cg="62."/>
<eng-data t="0.061" f="42.201" m="71.1668" cg="62."/>
<eng-data t="0.117" f="47.354" m="69.3268" cg="62."/>
<eng-data t="0.243" f="46.678" m="64.9799" cg="62."/>
<eng-data t="0.34" f="46.339" m="61.6695" cg="62."/>
<eng-data t="0.438" f="47.384" m="58.2997" cg="62."/>
<eng-data t="0.48" f="50.92" m="56.7848" cg="62."/>
<eng-data t="0.508" f="46.359" m="55.7855" cg="62."/>
<eng-data t="0.543" f="47.732" m="54.5772" cg="62."/>
<eng-data t="0.662" f="45.693" m="50.4983" cg="62."/>
<eng-data t="0.851" f="42.28" m="44.398" cg="62."/>
<eng-data t="1.039" f="41.266" m="38.6353" cg="62."/>
<eng-data t="1.116" f="42.987" m="36.2551" cg="62."/>
<eng-data t="1.193" f="39.226" m="33.9325" cg="62."/>
<eng-data t="1.221" f="42.31" m="33.0949" cg="62."/>
<eng-data t="1.312" f="38.888" m="30.3839" cg="62."/>
<eng-data t="1.326" f="40.609" m="29.9756" cg="62."/>
<eng-data t="1.479" f="38.221" m="25.5505" cg="62."/>
<eng-data t="1.675" f="35.157" m="20.2738" cg="62."/>
<eng-data t="1.843" f="32.77" m="16.0869" cg="62."/>
<eng-data t="1.878" f="36.888" m="15.1924" cg="62."/>
<eng-data t="1.899" f="32.093" m="14.6609" cg="62."/>
<eng-data t="1.997" f="30.382" m="12.4146" cg="62."/>
<eng-data t="2.13" f="26.622" m="9.63298" cg="62."/>
<eng-data t="2.263" f="23.547" m="7.18489" cg="62."/>
<eng-data t="2.444" f="19.11" m="4.35213" cg="62."/>
<eng-data t="2.591" f="13.977" m="2.56764" cg="62."/>
<eng-data t="2.752" f="8.502" m="1.23981" cg="62."/>
<eng-data t="2.892" f="4.743" m="0.559481" cg="62."/>
<eng-data t="3.053" f="2.014" m="0.160346" cg="62."/>
<eng-data t="3.27" f="0." m="0." cg="62."/>
</data>
</engine>
<engine mfg="Aerotech" code="G40W" Type="single-use" dia="29." len="124." initWt="123."
propWt="53.8" delays="4,7,10" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="43.052" peakThrust="74.325" throatDia="0." exitDia="0." Itot="99.02"
burn-time="2.3" massFrac="43.74" Isp="187.68" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Aerotech G40W RASP.ENG file made by Tim Van Milligan
For RockSim www.RockSim.com
File Created March 2, 2005
Thrust curve supplied by Aerotech for the molded case G40W motors.
</comments>
<data>
<eng-data t="0." f="0." m="53.8" cg="62."/>
<eng-data t="0.024" f="74.325" m="53.3154" cg="62."/>
<eng-data t="0.057" f="67.005" m="52.0484" cg="62."/>
<eng-data t="0.252" f="65.879" m="45.009" cg="62."/>
<eng-data t="0.5" f="63.063" m="36.3219" cg="62."/>
<eng-data t="0.765" f="60.248" m="27.4447" cg="62."/>
<eng-data t="1." f="54.054" m="20.1476" cg="62."/>
<eng-data t="1.25" f="47.298" m="13.2642" cg="62."/>
<eng-data t="1.502" f="36.599" m="7.52075" cg="62."/>
<eng-data t="1.751" f="25.338" m="3.3311" cg="62."/>
<eng-data t="1.999" f="12.951" m="0.751488" cg="62."/>
<eng-data t="2.121" f="3.941" m="0.191641" cg="62."/>
<eng-data t="2.3" f="0." m="0." cg="62."/>
</data>
</engine>
<engine mfg="Aerotech" code="G54W" Type="reloadable" dia="29." len="124." initWt="136.5"
propWt="46." delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="53.676" peakThrust="81.64" throatDia="0." exitDia="0." Itot="81.05"
burn-time="1.51" massFrac="33.7" Isp="179.67" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Aerotech G54 RASP.ENG file made from NAR published data
File produced July 4, 2000
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="46." cg="62."/>
<eng-data t="0.018" f="10.953" m="45.9441" cg="62."/>
<eng-data t="0.042" f="39.215" m="45.6024" cg="62."/>
<eng-data t="0.083" f="66.888" m="44.3679" cg="62."/>
<eng-data t="0.14" f="72.075" m="42.1202" cg="62."/>
<eng-data t="0.223" f="74.958" m="38.657" cg="62."/>
<eng-data t="0.25" f="76.694" m="37.4951" cg="62."/>
<eng-data t="0.282" f="80.156" m="36.0708" cg="62."/>
<eng-data t="0.315" f="79.577" m="34.575" cg="62."/>
<eng-data t="0.336" f="79.577" m="33.6265" cg="62."/>
<eng-data t="0.354" f="81.64" m="32.803" cg="62."/>
<eng-data t="0.365" f="77.841" m="32.3052" cg="62."/>
<eng-data t="0.374" f="80.724" m="31.9002" cg="62."/>
<eng-data t="0.389" f="76.694" m="31.2302" cg="62."/>
<eng-data t="0.455" f="76.116" m="28.3682" cg="62."/>
<eng-data t="0.523" f="74.39" m="25.4639" cg="62."/>
<eng-data t="0.639" f="70.928" m="20.6804" cg="62."/>
<eng-data t="0.722" f="67.467" m="17.4207" cg="62."/>
<eng-data t="0.82" f="64.005" m="13.7645" cg="62."/>
<eng-data t="0.897" f="58.817" m="11.0807" cg="62."/>
<eng-data t="0.992" f="51.894" m="8.09613" cg="62."/>
<eng-data t="1.084" f="43.824" m="5.5972" cg="62."/>
<eng-data t="1.197" f="34.017" m="3.10111" cg="62."/>
<eng-data t="1.268" f="28.251" m="1.84654" cg="62."/>
<eng-data t="1.283" f="29.987" m="1.59864" cg="62."/>
<eng-data t="1.295" f="27.104" m="1.40423" cg="62."/>
<eng-data t="1.328" f="23.642" m="0.929016" cg="62."/>
<eng-data t="1.366" f="16.719" m="0.493786" cg="62."/>
<eng-data t="1.399" f="9.803" m="0.245419" cg="62."/>
<eng-data t="1.435" f="4.612" m="0.0981575" cg="62."/>
<eng-data t="1.51" f="0." m="0." cg="62."/>
</data>
</engine>
<engine mfg="Aerotech" code="G61W" Type="reloadable" dia="38." len="106.7"
initWt="190.4" propWt="61.3" delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="54.307" peakThrust="81.037" throatDia="0." exitDia="0." Itot="110.787"
burn-time="2.04" massFrac="32.2" Isp="184.29" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>G61W Data Entered by Tim Van Milligan
For RockSim: www.RockSim.com
Based on TRA Certification Test date: June 13, 2004
Not Approved by TRA or Aerotech
</comments>
<data>
<eng-data t="0." f="0." m="61.3" cg="53.35"/>
<eng-data t="0.008" f="3.083" m="61.2932" cg="53.35"/>
<eng-data t="0.054" f="71.348" m="60.3459" cg="53.35"/>
<eng-data t="0.089" f="72.229" m="58.9557" cg="53.35"/>
<eng-data t="0.174" f="75.312" m="55.4861" cg="53.35"/>
<eng-data t="0.216" f="78.394" m="53.7001" cg="53.35"/>
<eng-data t="0.247" f="79.716" m="52.3441" cg="53.35"/>
<eng-data t="0.502" f="81.037" m="41.0034" cg="53.35"/>
<eng-data t="0.753" f="77.073" m="30.024" cg="53.35"/>
<eng-data t="1.001" f="72.669" m="19.7501" cg="53.35"/>
<eng-data t="1.132" f="66.944" m="14.6902" cg="53.35"/>
<eng-data t="1.252" f="55.933" m="10.6108" cg="53.35"/>
<eng-data t="1.503" f="38.316" m="4.06608" cg="53.35"/>
<eng-data t="1.754" f="10.13" m="0.701938" cg="53.35"/>
<eng-data t="1.905" f="3.523" m="0.13158" cg="53.35"/>
<eng-data t="2.04" f="0." m="0." cg="53.35"/>
</data>
</engine>
<engine mfg="Aerotech" code="G64W" Type="reloadable" dia="29." len="124." initWt="151.2"
propWt="62.5" delays="4,8,10" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="56.844" peakThrust="98.31" throatDia="0." exitDia="0." Itot="118.803"
burn-time="2.09" massFrac="41.34" Isp="193.83" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Aerotech G64 RASP.ENG file made from NAR published data
File produced July 4, 2000
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="62.5" cg="62."/>
<eng-data t="0.014" f="54.325" m="62.2999" cg="62."/>
<eng-data t="0.032" f="81.488" m="61.6569" cg="62."/>
<eng-data t="0.059" f="98.31" m="60.38" cg="62."/>
<eng-data t="0.101" f="85.021" m="58.3546" cg="62."/>
<eng-data t="0.165" f="83.847" m="55.5117" cg="62."/>
<eng-data t="0.274" f="85.614" m="50.6531" cg="62."/>
<eng-data t="0.37" f="87.39" m="46.2844" cg="62."/>
<eng-data t="0.476" f="86.798" m="41.4276" cg="62."/>
<eng-data t="0.503" f="91.516" m="40.1612" cg="62."/>
<eng-data t="0.517" f="85.614" m="39.5089" cg="62."/>
<eng-data t="0.585" f="83.847" m="36.4778" cg="62."/>
<eng-data t="0.723" f="80.896" m="30.4977" cg="62."/>
<eng-data t="0.745" f="82.07" m="29.5546" cg="62."/>
<eng-data t="0.773" f="77.945" m="28.3761" cg="62."/>
<eng-data t="0.883" f="75.576" m="23.9341" cg="62."/>
<eng-data t="0.988" f="74.401" m="19.7918" cg="62."/>
<eng-data t="1.093" f="69.673" m="15.8126" cg="62."/>
<eng-data t="1.262" f="61.412" m="9.98534" cg="62."/>
<eng-data t="1.28" f="61.994" m="9.40105" cg="62."/>
<eng-data t="1.326" f="58.451" m="7.94368" cg="62."/>
<eng-data t="1.372" f="54.907" m="6.57206" cg="62."/>
<eng-data t="1.422" f="47.238" m="5.22865" cg="62."/>
<eng-data t="1.505" f="34.841" m="3.43667" cg="62."/>
<eng-data t="1.591" f="23.027" m="2.12761" cg="62."/>
<eng-data t="1.701" f="13.581" m="1.06837" cg="62."/>
<eng-data t="1.829" f="7.085" m="0.372564" cg="62."/>
<eng-data t="1.902" f="4.133" m="0.157156" cg="62."/>
<eng-data t="1.966" f="1.771" m="0.0577648" cg="62."/>
<eng-data t="2.09" f="0." m="0." cg="62."/>
</data>
</engine>
<engine mfg="Aerotech" code="G67R" Type="reloadable" dia="38." len="106.43"
initWt="191." propWt="57.6" delays="6,10" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="68.456" peakThrust="90.425" throatDia="0." exitDia="0." Itot="109.53"
burn-time="1.6" massFrac="30.16" Isp="193.91" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>G67R Data Entered by Tim Van Milligan
For RockSim: www.RockSim.com
Based on Aerotech's Reload Kit Instruction Sheet.
Not Officially Approved by TRA or Aerotech
</comments>
<data>
<eng-data t="0." f="0." m="57.6" cg="53.215"/>
<eng-data t="0.041" f="11.795" m="57.4728" cg="53.215"/>
<eng-data t="0.098" f="57.288" m="56.4375" cg="53.215"/>
<eng-data t="0.119" f="71.329" m="55.7273" cg="53.215"/>
<eng-data t="0.15" f="75.822" m="54.5278" cg="53.215"/>
<eng-data t="0.2" f="80.877" m="52.4677" cg="53.215"/>
<eng-data t="0.3" f="88.74" m="48.0077" cg="53.215"/>
<eng-data t="0.4" f="89.301" m="43.3263" cg="53.215"/>
<eng-data t="0.497" f="90.425" m="38.7423" cg="53.215"/>
<eng-data t="0.606" f="89.301" m="33.5913" cg="53.215"/>
<eng-data t="0.791" f="85.932" m="25.0672" cg="53.215"/>
<eng-data t="1.003" f="75.26" m="16.0818" cg="53.215"/>
<eng-data t="1.19" f="64.589" m="9.20544" cg="53.215"/>
<eng-data t="1.299" f="58.411" m="5.68019" cg="53.215"/>
<eng-data t="1.399" f="55.041" m="2.69707" cg="53.215"/>
<eng-data t="1.423" f="52.233" m="2.02011" cg="53.215"/>
<eng-data t="1.456" f="47.74" m="1.15264" cg="53.215"/>
<eng-data t="1.497" f="22.466" m="0.395774" cg="53.215"/>
<eng-data t="1.518" f="12.356" m="0.203495" cg="53.215"/>
<eng-data t="1.562" f="2.808" m="0.0280569" cg="53.215"/>
<eng-data t="1.6" f="0." m="0." cg="53.215"/>
</data>
</engine>
<engine mfg="Aerotech" code="G69N" Type="reloadable" dia="38." len="106." initWt="201."
propWt="62.2" delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="68.151" peakThrust="86.441" throatDia="0." exitDia="0." Itot="136.301"
burn-time="2." massFrac="30.95" Isp="223.45" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>NAR Test Data
March 23, 2007
</comments>
<data>
<eng-data t="0." f="0." m="62.2" cg="53."/>
<eng-data t="0.001" f="0.05" m="62.2" cg="53."/>
<eng-data t="0.002" f="1.04339" m="62.1997" cg="53."/>
<eng-data t="0.006" f="1.49626" m="62.1974" cg="53."/>
<eng-data t="0.01" f="3.99151" m="62.1924" cg="53."/>
<eng-data t="0.012" f="7.18827" m="62.1873" cg="53."/>
<eng-data t="0.016" f="31.7855" m="62.1517" cg="53."/>
<eng-data t="0.018" f="38.6675" m="62.1196" cg="53."/>
<eng-data t="0.02" f="43.507" m="62.0821" cg="53."/>
<eng-data t="0.028" f="55.3616" m="61.9016" cg="53."/>
<eng-data t="0.034" f="58.4696" m="61.7458" cg="53."/>
<eng-data t="0.04" f="63.3535" m="61.579" cg="53."/>
<eng-data t="0.042" f="66.4615" m="61.5198" cg="53."/>
<eng-data t="0.054" f="74.0094" m="61.1351" cg="53."/>
<eng-data t="0.066" f="76.2294" m="60.7238" cg="53."/>
<eng-data t="0.124" f="75.7854" m="58.712" cg="53."/>
<eng-data t="0.17" f="77.5614" m="57.1025" cg="53."/>
<eng-data t="0.668" f="82.0013" m="38.9716" cg="53."/>
<eng-data t="0.72" f="83.7773" m="37.0046" cg="53."/>
<eng-data t="1.1239" f="86.4412" m="21.3176" cg="53."/>
<eng-data t="1.4159" f="85.9972" m="9.82874" cg="53."/>
<eng-data t="1.4619" f="84.2213" m="8.04215" cg="53."/>
<eng-data t="1.4959" f="80.2253" m="6.76641" cg="53."/>
<eng-data t="1.5439" f="71.7894" m="5.10151" cg="53."/>
<eng-data t="1.7059" f="29.832" m="1.34521" cg="53."/>
<eng-data t="1.7479" f="20.7301" m="0.860669" cg="53."/>
<eng-data t="1.8259" f="9.23064" m="0.327448" cg="53."/>
<eng-data t="1.9019" f="4.21351" m="0.0943133" cg="53."/>
<eng-data t="2." f="0." m="0." cg="53."/>
</data>
</engine>
<engine mfg="Aerotech" code="G71R" Type="reloadable" dia="29." len="124." initWt="147."
propWt="56.9" delays="4,7,10" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="62.879" peakThrust="117.884" throatDia="0." exitDia="0."
Itot="106.894" burn-time="1.7" massFrac="38.71" Isp="191.57" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>G71R based on Aerotech instruction sheet by C. Kobel 3/29/07</comments>
<data>
<eng-data t="0." f="0." m="56.9" cg="62."/>
<eng-data t="0." f="0.389" m="56.9" cg="62."/>
<eng-data t="0.05" f="109.714" m="55.4348" cg="62."/>
<eng-data t="0.1" f="117.884" m="52.406" cg="62."/>
<eng-data t="0.2" f="113.216" m="46.2552" cg="62."/>
<eng-data t="0.3" f="109.714" m="40.3219" cg="62."/>
<eng-data t="0.4" f="105.045" m="34.606" cg="62."/>
<eng-data t="0.5" f="99.21" m="29.1697" cg="62."/>
<eng-data t="0.6" f="92.207" m="24.0751" cg="62."/>
<eng-data t="0.7" f="83.258" m="19.405" cg="62."/>
<eng-data t="0.8" f="75.477" m="15.1803" cg="62."/>
<eng-data t="0.9" f="68.085" m="11.3593" cg="62."/>
<eng-data t="1." f="57.97" m="8.00433" cg="62."/>
<eng-data t="1.1" f="47.465" m="5.19815" cg="62."/>
<eng-data t="1.2" f="33.848" m="3.03398" cg="62."/>
<eng-data t="1.3" f="21.009" m="1.57395" cg="62."/>
<eng-data t="1.4" f="11.283" m="0.714487" cg="62."/>
<eng-data t="1.5" f="5.447" m="0.269213" cg="62."/>
<eng-data t="1.6" f="2.334" m="0.06212" cg="62."/>
<eng-data t="1.7" f="0." m="0." cg="62."/>
</data>
</engine>
<engine mfg="Aerotech" code="G74W" Type="single-use" dia="29." len="83." initWt="87."
propWt="39.3" delays="4,6" auto-calc-mass="1" auto-calc-cg="1" avgThrust="71.549"
peakThrust="91.215" throatDia="0." exitDia="0." Itot="85.287" burn-time="1.19"
massFrac="45.17" Isp="221.29" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<comments>G74W Economax</comments>
<data>
<eng-data t="0." f="0." m="39.3" cg="41.5"/>
<eng-data t="0.023" f="6.551" m="39.2653" cg="41.5"/>
<eng-data t="0.05" f="21.838" m="39.0887" cg="41.5"/>
<eng-data t="0.088" f="44.852" m="38.5048" cg="41.5"/>
<eng-data t="0.124" f="67.362" m="37.5741" cg="41.5"/>
<eng-data t="0.135" f="71.561" m="37.222" cg="41.5"/>
<eng-data t="0.148" f="74.417" m="36.7847" cg="41.5"/>
<eng-data t="0.197" f="80.128" m="35.04" cg="41.5"/>
<eng-data t="0.248" f="85." m="33.0997" cg="41.5"/>
<eng-data t="0.298" f="87.52" m="31.1122" cg="41.5"/>
<eng-data t="0.397" f="89.704" m="27.0698" cg="41.5"/>
<eng-data t="0.499" f="91.215" m="22.8181" cg="41.5"/>
<eng-data t="0.6" f="90.375" m="18.5924" cg="41.5"/>
<eng-data t="0.699" f="90.375" m="14.4696" cg="41.5"/>
<eng-data t="0.751" f="89.536" m="12.3141" cg="41.5"/>
<eng-data t="0.8" f="87.856" m="10.3114" cg="41.5"/>
<eng-data t="0.9" f="84.496" m="6.34045" cg="41.5"/>
<eng-data t="0.954" f="82.144" m="4.26719" cg="41.5"/>
<eng-data t="0.971" f="81.808" m="3.62502" cg="41.5"/>
<eng-data t="0.987" f="79.96" m="3.02868" cg="41.5"/>
<eng-data t="1.002" f="76.433" m="2.48819" cg="41.5"/>
<eng-data t="1.023" f="67.194" m="1.79326" cg="41.5"/>
<eng-data t="1.065" f="44.516" m="0.712267" cg="41.5"/>
<eng-data t="1.094" f="22.174" m="0.266672" cg="41.5"/>
<eng-data t="1.107" f="15.287" m="0.154469" cg="41.5"/>
<eng-data t="1.126" f="6.887" m="0.0574" cg="41.5"/>
<eng-data t="1.138" f="3.36" m="0.0290691" cg="41.5"/>
<eng-data t="1.157" f="1.344" m="0.00847687" cg="41.5"/>
<eng-data t="1.18" f="0.168" m="0.000464486" cg="41.5"/>
<eng-data t="1.192" f="0." m="0." cg="41.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="G75J" Type="reloadable" dia="29." len="195." initWt="227.9"
propWt="105.6" delays="6,10" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="73.377" peakThrust="87.27" throatDia="0." exitDia="0." Itot="161.429"
burn-time="2.2" massFrac="46.34" Isp="155.88" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="105.6" cg="97.5"/>
<eng-data t="0." f="0.04" m="105.6" cg="97.5"/>
<eng-data t="0.1" f="82.64" m="102.896" cg="97.5"/>
<eng-data t="0.2" f="78.06" m="97.6396" cg="97.5"/>
<eng-data t="0.3" f="78.06" m="92.5332" cg="97.5"/>
<eng-data t="0.5" f="87.27" m="81.718" cg="97.5"/>
<eng-data t="1.5" f="87.27" m="24.6297" cg="97.5"/>
<eng-data t="1.7" f="82.64" m="13.5149" cg="97.5"/>
<eng-data t="1.9" f="64.27" m="3.90467" cg="97.5"/>
<eng-data t="2." f="18.37" m="1.20169" cg="97.5"/>
<eng-data t="2.2" f="0." m="0." cg="97.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="G75M" Type="single-use" dia="29." len="124." initWt="131."
propWt="66.8" delays="4,7,10" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="60.51" peakThrust="101.497" throatDia="0." exitDia="0." Itot="119.265"
burn-time="1.97" massFrac="50.99" Isp="182.06" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>29mm Aerotech G75 Metal Storm single use</comments>
<data>
<eng-data t="0." f="0." m="66.8" cg="62."/>
<eng-data t="0.01" f="81.492" m="66.5718" cg="62."/>
<eng-data t="0.013" f="94.731" m="66.4237" cg="62."/>
<eng-data t="0.021" f="101.497" m="65.9841" cg="62."/>
<eng-data t="0.037" f="87.964" m="65.1352" cg="62."/>
<eng-data t="0.068" f="86.199" m="63.6232" cg="62."/>
<eng-data t="0.154" f="87.67" m="59.4357" cg="62."/>
<eng-data t="0.188" f="90.906" m="57.7353" cg="62."/>
<eng-data t="0.211" f="90.024" m="56.5699" cg="62."/>
<eng-data t="0.31" f="95.613" m="51.4232" cg="62."/>
<eng-data t="0.357" f="91.494" m="48.9604" cg="62."/>
<eng-data t="0.464" f="93.848" m="43.4066" cg="62."/>
<eng-data t="0.696" f="92.083" m="31.3264" cg="62."/>
<eng-data t="0.879" f="84.728" m="22.265" cg="62."/>
<eng-data t="0.907" f="85.611" m="20.9293" cg="62."/>
<eng-data t="0.92" f="92.965" m="20.2792" cg="62."/>
<eng-data t="0.939" f="77.667" m="19.3713" cg="62."/>
<eng-data t="1.014" f="72.96" m="16.2075" cg="62."/>
<eng-data t="1.027" f="78.55" m="15.656" cg="62."/>
<eng-data t="1.053" f="71.489" m="14.5635" cg="62."/>
<eng-data t="1.171" f="64.134" m="10.0817" cg="62."/>
<eng-data t="1.304" f="52.367" m="5.74245" cg="62."/>
<eng-data t="1.312" f="56.78" m="5.49792" cg="62."/>
<eng-data t="1.325" f="52.661" m="5.09948" cg="62."/>
<eng-data t="1.374" f="48.542" m="3.71074" cg="62."/>
<eng-data t="1.411" f="44.129" m="2.7505" cg="62."/>
<eng-data t="1.442" f="36.186" m="2.05324" cg="62."/>
<eng-data t="1.492" f="22.359" m="1.23347" cg="62."/>
<eng-data t="1.538" f="14.121" m="0.76352" cg="62."/>
<eng-data t="1.585" f="7.649" m="0.476977" cg="62."/>
<eng-data t="1.643" f="3.825" m="0.290606" cg="62."/>
<eng-data t="1.7" f="2.648" m="0.187279" cg="62."/>
<eng-data t="1.802" f="1.471" m="0.0696199" cg="62."/>
<eng-data t="1.971" f="0." m="0." cg="62."/>
</data>
</engine>
<engine mfg="Aerotech" code="G76G" Type="reloadable" dia="29." len="124." initWt="144."
propWt="60." delays="4,7,10" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="57.226" peakThrust="149.304" throatDia="0." exitDia="0."
Itot="114.503" burn-time="2." massFrac="41.67" Isp="194.6" tDiv="10" tStep="-1."
tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>From Official NAR Certification
@File: G76G_Composite.txt, @Pts-I: 1001, @Pts-O: 33, @Sm: 4, @CO: 5%
@TI: 114.4814, @TIa: 113.4881, @TIe: +0.01%, @ThMax: 149.6117, @ThAvg: 72.3776, @Tb: 1.568
Mojave Green Formulation</comments>
<data>
<eng-data t="0." f="0." m="60." cg="62."/>
<eng-data t="0." f="0.686899" m="60." cg="62."/>
<eng-data t="0.004" f="4.23776" m="59.9948" cg="62."/>
<eng-data t="0.006" f="9.67736" m="59.9875" cg="62."/>
<eng-data t="0.016" f="54.3647" m="59.8198" cg="62."/>
<eng-data t="0.03" f="98.111" m="59.2605" cg="62."/>
<eng-data t="0.034" f="108.445" m="59.044" cg="62."/>
<eng-data t="0.04" f="121.087" m="58.6832" cg="62."/>
<eng-data t="0.048" f="132.968" m="58.1507" cg="62."/>
<eng-data t="0.058" f="142.263" m="57.4296" cg="62."/>
<eng-data t="0.068" f="147.121" m="56.6714" cg="62."/>
<eng-data t="0.082" f="149.304" m="55.5841" cg="62."/>
<eng-data t="0.112" f="146.802" m="53.2567" cg="62."/>
<eng-data t="0.15" f="138.7" m="50.4142" cg="62."/>
<eng-data t="0.17" f="135.958" m="48.975" cg="62."/>
<eng-data t="0.376" f="112.155" m="35.5837" cg="62."/>
<eng-data t="0.466" f="103.018" m="30.5099" cg="62."/>
<eng-data t="0.482" f="104.376" m="29.6405" cg="62."/>
<eng-data t="0.56" f="92.5972" m="25.6152" cg="62."/>
<eng-data t="0.606" f="92.8117" m="23.3806" cg="62."/>
<eng-data t="0.644" f="84.1557" m="21.6187" cg="62."/>
<eng-data t="0.748" f="73.895" m="17.3121" cg="62."/>
<eng-data t="0.76" f="74.2399" m="16.8464" cg="62."/>
<eng-data t="0.79" f="69.6626" m="15.7153" cg="62."/>
<eng-data t="0.804" f="70.558" m="15.201" cg="62."/>
<eng-data t="0.822" f="66.7194" m="14.5536" cg="62."/>
<eng-data t="0.856" f="62.648" m="13.4012" cg="62."/>
<eng-data t="1.154" f="39.9734" m="5.38887" cg="62."/>
<eng-data t="1.3739" f="19.8986" m="1.9394" cg="62."/>
<eng-data t="1.4739" f="12.5124" m="1.09022" cg="62."/>
<eng-data t="1.5739" f="7.4133" m="0.568167" cg="62."/>
<eng-data t="1.7799" f="1.18956" m="0.103851" cg="62."/>
<eng-data t="1.9999" f="0.60939" m="0.000159661" cg="62."/>
<eng-data t="2.0009" f="0." m="0." cg="62."/>
</data>
</engine>
<engine mfg="Aerotech" code="G77R" Type="single-use" dia="29." len="124." initWt="122."
propWt="58.1" delays="4,7,10" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="79.643" peakThrust="99.309" throatDia="0." exitDia="0." Itot="101.704"
burn-time="1.28" massFrac="47.62" Isp="178.5" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Single-Use Casing. Entered by Tim Van Milligan for RockSim Users. Used John
Coker's ThrustCurve Tracer software and NAR cert paperwork dated 7-29-06.
</comments>
<data>
<eng-data t="0." f="0." m="58.1" cg="62."/>
<eng-data t="0.01" f="19.124" m="58.0454" cg="62."/>
<eng-data t="0.018" f="15.668" m="57.9659" cg="62."/>
<eng-data t="0.059" f="66.59" m="57.0026" cg="62."/>
<eng-data t="0.084" f="72.35" m="56.0104" cg="62."/>
<eng-data t="0.122" f="75.115" m="54.4098" cg="62."/>
<eng-data t="0.151" f="77.419" m="53.1463" cg="62."/>
<eng-data t="0.173" f="77.65" m="52.1719" cg="62."/>
<eng-data t="0.271" f="85.945" m="47.5925" cg="62."/>
<eng-data t="0.337" f="88.018" m="44.313" cg="62."/>
<eng-data t="0.424" f="91.935" m="39.8412" cg="62."/>
<eng-data t="0.475" f="93.318" m="37.1425" cg="62."/>
<eng-data t="0.523" f="94.931" m="34.5616" cg="62."/>
<eng-data t="0.57" f="96.313" m="31.9941" cg="62."/>
<eng-data t="0.61" f="96.313" m="29.7933" cg="62."/>
<eng-data t="0.644" f="99.309" m="27.8935" cg="62."/>
<eng-data t="0.656" f="96.774" m="27.2215" cg="62."/>
<eng-data t="0.728" f="95.622" m="23.2647" cg="62."/>
<eng-data t="0.799531" f="94.1176" m="19.388" cg="62."/>
<eng-data t="0.902" f="91.014" m="13.9695" cg="62."/>
<eng-data t="0.961" f="88.479" m="10.9446" cg="62."/>
<eng-data t="1.017" f="88.018" m="8.12146" cg="62."/>
<eng-data t="1.047" f="84.562" m="6.64262" cg="62."/>
<eng-data t="1.071" f="81.106" m="5.50694" cg="62."/>
<eng-data t="1.099" f="76.037" m="4.25015" cg="62."/>
<eng-data t="1.127" f="69.355" m="3.08734" cg="62."/>
<eng-data t="1.158" f="61.06" m="1.93257" cg="62."/>
<eng-data t="1.188" f="44.931" m="1.02433" cg="62."/>
<eng-data t="1.213" f="30.184" m="0.487948" cg="62."/>
<eng-data t="1.231" f="18.203" m="0.239172" cg="62."/>
<eng-data t="1.277" f="0." m="0." cg="62."/>
</data>
</engine>
<engine mfg="Aerotech" code="G77R" Type="reloadable" dia="29." len="149.86"
initWt="155." propWt="58." delays="6,10" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="77.716" peakThrust="96.892" throatDia="0." exitDia="0." Itot="104.139"
burn-time="1.34" massFrac="35.74" Isp="191.68" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>G77R Data Entered by Tim Van Milligan
For RockSim: www.RockSim.com
Based on Aerotech's Reload Kit Instruction Sheet.
Not Officially Approved by TRA or Aerotech
</comments>
<data>
<eng-data t="0." f="0." m="55.4" cg="74.93"/>
<eng-data t="0.04" f="45.143" m="54.9197" cg="74.93"/>
<eng-data t="0.071" f="53.951" m="54.1026" cg="74.93"/>
<eng-data t="0.096" f="60.558" m="53.3411" cg="74.93"/>
<eng-data t="0.139" f="68.265" m="51.8677" cg="74.93"/>
<eng-data t="0.198" f="75.972" m="49.6041" cg="74.93"/>
<eng-data t="0.294" f="83.679" m="45.5274" cg="74.93"/>
<eng-data t="0.396" f="89.185" m="40.8375" cg="74.93"/>
<eng-data t="0.51" f="91.387" m="35.362" cg="74.93"/>
<eng-data t="0.6" f="93.589" m="30.9338" cg="74.93"/>
<eng-data t="0.801" f="96.892" m="20.75" cg="74.93"/>
<eng-data t="1.002" f="93.589" m="10.5661" cg="74.93"/>
<eng-data t="1.1" f="89.185" m="5.80169" cg="74.93"/>
<eng-data t="1.134" f="83.679" m="4.23837" cg="74.93"/>
<eng-data t="1.168" f="77.073" m="2.78458" cg="74.93"/>
<eng-data t="1.199" f="59.456" m="1.6588" cg="74.93"/>
<eng-data t="1.236" f="34.132" m="0.737741" cg="74.93"/>
<eng-data t="1.277" f="13.213" m="0.221415" cg="74.93"/>
<eng-data t="1.34" f="0." m="0." cg="74.93"/>
</data>
</engine>
<engine mfg="Aerotech" code="G78G" Type="single-use" dia="29." len="146." initWt="125."
propWt="59.7" delays="4,7,10" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="74.585" peakThrust="102.242" throatDia="0." exitDia="0."
Itot="109.782" burn-time="1.47" massFrac="47.76" Isp="187.51" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>@File: G78G_Typ.txt, @Pts-I: 1001, @Pts-O: 31, @Sm: 0, @CO: 5%
@TI: 109.776, @TIa: 109.5639, @TIe: 0.0%, @ThMax: 102.242, @ThAvg: 79.5671, @Tb: 1.377
Exported using ThrustCurveTool, www.ThrustGear.com
</comments>
<data>
<eng-data t="0." f="0." m="59.7" cg="73."/>
<eng-data t="0.004" f="2.76203" m="59.697" cg="73."/>
<eng-data t="0.006" f="34.7707" m="59.6766" cg="73."/>
<eng-data t="0.008" f="44.326" m="59.6336" cg="73."/>
<eng-data t="0.01" f="41.2789" m="59.587" cg="73."/>
<eng-data t="0.012" f="28.5933" m="59.549" cg="73."/>
<eng-data t="0.014" f="27.3926" m="59.5186" cg="73."/>
<eng-data t="0.016" f="38.0574" m="59.483" cg="73."/>
<eng-data t="0.02" f="47.7036" m="59.3897" cg="73."/>
<eng-data t="0.022" f="48.2012" m="59.3376" cg="73."/>
<eng-data t="0.03" f="56.4344" m="59.11" cg="73."/>
<eng-data t="0.042" f="61.4034" m="58.7255" cg="73."/>
<eng-data t="0.06" f="65.883" m="58.1025" cg="73."/>
<eng-data t="0.212" f="84.526" m="51.8862" cg="73."/>
<eng-data t="0.266" f="88.9218" m="49.3395" cg="73."/>
<eng-data t="0.404" f="95.5932" m="42.416" cg="73."/>
<eng-data t="0.43" f="98.9746" m="41.0405" cg="73."/>
<eng-data t="0.466" f="100.536" m="39.0876" cg="73."/>
<eng-data t="0.58" f="102.242" m="32.8021" cg="73."/>
<eng-data t="0.694" f="101.319" m="26.4924" cg="73."/>
<eng-data t="0.86" f="95.4526" m="17.6109" cg="73."/>
<eng-data t="1.1" f="90.4186" m="5.48158" cg="73."/>
<eng-data t="1.132" f="82.5618" m="3.9765" cg="73."/>
<eng-data t="1.156" f="72.6383" m="2.96372" cg="73."/>
<eng-data t="1.168" f="64.903" m="2.51494" cg="73."/>
<eng-data t="1.194" f="42.3389" m="1.7568" cg="73."/>
<eng-data t="1.216" f="28.3424" m="1.33399" cg="73."/>
<eng-data t="1.226" f="24.9802" m="1.18901" cg="73."/>
<eng-data t="1.2559" f="17.4005" m="0.844455" cg="73."/>
<eng-data t="1.2859" f="13.0465" m="0.596096" cg="73."/>
<eng-data t="1.3819" f="5.05295" m="0.123652" cg="73."/>
<eng-data t="1.4719" f="0." m="0." cg="73."/>
</data>
</engine>
<engine mfg="Aerotech" code="G79W" Type="reloadable" dia="29." len="149.86"
initWt="154." propWt="60.9" delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="75.39" peakThrust="99.645" throatDia="0." exitDia="0." Itot="107.054"
burn-time="1.42" massFrac="39.55" Isp="179.25" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>G79W Data Entered by Tim Van Milligan
For RockSim: www.RockSim.com
Based on TRA Certification Test date: June 13, 2004
Not Approved by TRA or Aerotech
</comments>
<data>
<eng-data t="0." f="0." m="60.9" cg="74.93"/>
<eng-data t="0.015" f="7.157" m="60.8695" cg="74.93"/>
<eng-data t="0.074" f="91.937" m="59.2065" cg="74.93"/>
<eng-data t="0.09" f="91.387" m="58.3722" cg="74.93"/>
<eng-data t="0.114" f="84.781" m="57.1696" cg="74.93"/>
<eng-data t="0.145" f="84.23" m="55.6793" cg="74.93"/>
<eng-data t="0.201" f="89.185" m="52.9171" cg="74.93"/>
<eng-data t="0.291" f="94.69" m="48.21" cg="74.93"/>
<eng-data t="0.4" f="98.544" m="42.219" cg="74.93"/>
<eng-data t="0.6" f="99.645" m="30.9446" cg="74.93"/>
<eng-data t="0.708" f="96.892" m="24.9071" cg="74.93"/>
<eng-data t="0.8" f="93.038" m="19.937" cg="74.93"/>
<eng-data t="0.915" f="85.331" m="14.1025" cg="74.93"/>
<eng-data t="1." f="77.624" m="10.1627" cg="74.93"/>
<eng-data t="1.085" f="71.017" m="6.56901" cg="74.93"/>
<eng-data t="1.175" f="68.265" m="3.00348" cg="74.93"/>
<eng-data t="1.199" f="44.59" m="2.23308" cg="74.93"/>
<eng-data t="1.28" f="22.021" m="0.698401" cg="74.93"/>
<eng-data t="1.36" f="4.955" m="0.0845631" cg="74.93"/>
<eng-data t="1.42" f="0." m="0." cg="74.93"/>
</data>
</engine>
<engine mfg="Aerotech" code="G79W" Type="single-use" dia="29." len="146." initWt="124."
propWt="60.1" delays="4,7,10" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="55.211" peakThrust="82.108" throatDia="0." exitDia="0." Itot="106.446"
burn-time="1.93" massFrac="484.68" Isp="180.61" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Exported using ThrustCurveTool, www.ThrustGear.com
@File: G79_Ave.txt, @Pts-I: 1162, @Pts-O: 33, @Sm: 5, @CO: 5%
@TI: 106.4155, @TIa: 106.0632, @TIe: 0.0%, @ThMax: 82.1771, @ThAvg: 64.1443, @Tb: 1.659
</comments>
<data>
<eng-data t="0." f="0." m="60.1" cg="73."/>
<eng-data t="0." f="0.4562" m="60.1" cg="73."/>
<eng-data t="0.014" f="1.1376" m="60.0937" cg="73."/>
<eng-data t="0.018" f="3.2129" m="60.0888" cg="73."/>
<eng-data t="0.022" f="6.2017" m="60.0782" cg="73."/>
<eng-data t="0.034" f="27.3705" m="59.9644" cg="73."/>
<eng-data t="0.04" f="33.5757" m="59.8612" cg="73."/>
<eng-data t="0.044" f="34.8528" m="59.7839" cg="73."/>
<eng-data t="0.062" f="33.5201" m="59.4365" cg="73."/>
<eng-data t="0.096" f="39.9175" m="58.7316" cg="73."/>
<eng-data t="0.128" f="56.9842" m="57.8562" cg="73."/>
<eng-data t="0.138" f="60.0917" m="57.5257" cg="73."/>
<eng-data t="0.182" f="59.6191" m="56.0388" cg="73."/>
<eng-data t="0.23" f="68.8942" m="54.2973" cg="73."/>
<eng-data t="0.266" f="71.344" m="52.8721" cg="73."/>
<eng-data t="0.3" f="71.6246" m="51.4998" cg="73."/>
<eng-data t="0.36" f="75.8167" m="49.0025" cg="73."/>
<eng-data t="0.484" f="79.6244" m="43.5611" cg="73."/>
<eng-data t="0.516" f="78.6333" m="42.1315" cg="73."/>
<eng-data t="0.678" f="82.1075" m="34.7803" cg="73."/>
<eng-data t="0.7" f="78.836" m="33.7808" cg="73."/>
<eng-data t="0.72" f="78.179" m="32.8942" cg="73."/>
<eng-data t="0.772" f="79.5565" m="30.5787" cg="73."/>
<eng-data t="1.054" f="73.7176" m="18.3766" cg="73."/>
<eng-data t="1.086" f="71.152" m="17.0679" cg="73."/>
<eng-data t="1.182" f="68.8555" m="13.2736" cg="73."/>
<eng-data t="1.42" f="57.2479" m="4.80092" cg="73."/>
<eng-data t="1.52" f="40.7567" m="2.03422" cg="73."/>
<eng-data t="1.562" f="30.5794" m="1.18841" cg="73."/>
<eng-data t="1.628" f="11.8028" m="0.398742" cg="73."/>
<eng-data t="1.652" f="7.1707" m="0.270191" cg="73."/>
<eng-data t="1.68" f="3.9601" m="0.182208" cg="73."/>
<eng-data t="1.738" f="1.6764" m="0.0899181" cg="73."/>
<eng-data t="1.928" f="0." m="0." cg="73."/>
</data>
</engine>
<engine mfg="Aerotech" code="G104T" Type="reloadable" dia="29." len="125."
initWt="135.6" propWt="40.8" delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="92.069" peakThrust="118.5" throatDia="0." exitDia="0." Itot="82.862"
burn-time="0.9" massFrac="30.09" Isp="207.1" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="40.8" cg="62.5"/>
<eng-data t="0." f="118.5" m="40.8" cg="62.5"/>
<eng-data t="0.1" f="114.14" m="35.0726" cg="62.5"/>
<eng-data t="0.2" f="114.14" m="29.4525" cg="62.5"/>
<eng-data t="0.3" f="109.91" m="23.9366" cg="62.5"/>
<eng-data t="0.4" f="109.91" m="18.5248" cg="62.5"/>
<eng-data t="0.5" f="105.68" m="13.2171" cg="62.5"/>
<eng-data t="0.6" f="84.56" m="8.53352" cg="62.5"/>
<eng-data t="0.7" f="71.83" m="4.68332" cg="62.5"/>
<eng-data t="0.8" f="59.2" m="1.45746" cg="62.5"/>
<eng-data t="0.9" f="0." m="0." cg="62.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="G125T" Type="single-use" dia="29." len="127." initWt="127."
propWt="62." delays="14" auto-calc-mass="1" auto-calc-cg="1" avgThrust="124.681"
peakThrust="155.17" throatDia="0." exitDia="0." Itot="124.805" burn-time="1."
massFrac="48.82" Isp="205.27" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<comments>At DMS G125</comments>
<data>
<eng-data t="0." f="0." m="62." cg="63.5"/>
<eng-data t="0.008" f="89.654" m="61.8218" cg="63.5"/>
<eng-data t="0.017" f="117.24" m="61.3593" cg="63.5"/>
<eng-data t="0.027" f="119.654" m="60.7709" cg="63.5"/>
<eng-data t="0.047" f="111.033" m="59.6249" cg="63.5"/>
<eng-data t="0.115" f="124.826" m="55.6412" cg="63.5"/>
<eng-data t="0.2" f="134.136" m="50.1738" cg="63.5"/>
<eng-data t="0.399" f="149.308" m="36.1634" cg="63.5"/>
<eng-data t="0.601" f="155.17" m="20.8865" cg="63.5"/>
<eng-data t="0.8" f="138.274" m="6.38183" cg="63.5"/>
<eng-data t="0.824" f="133.791" m="4.75997" cg="63.5"/>
<eng-data t="0.878" f="88.964" m="1.77218" cg="63.5"/>
<eng-data t="0.914" f="44.482" m="0.578913" cg="63.5"/>
<eng-data t="0.933" f="22.414" m="0.263207" cg="63.5"/>
<eng-data t="0.974" f="2.069" m="0.0138756" cg="63.5"/>
<eng-data t="1.001" f="0." m="0." cg="63.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="G138T" Type="reloadable" dia="29." len="123.8"
initWt="152." propWt="70.4" delays="14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="151.68" peakThrust="194.691" throatDia="0." exitDia="0."
Itot="166.697" burn-time="1.1" massFrac="46.32" Isp="241.45" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>AeroTech G138T
from the reload instruction sheet 08/11/2010
Created by Scott Sager 10/10/2010
</comments>
<data>
<eng-data t="0." f="0." m="70.4" cg="61.9"/>
<eng-data t="0.002" f="113.497" m="70.3521" cg="61.9"/>
<eng-data t="0.043" f="118.736" m="68.3415" cg="61.9"/>
<eng-data t="0.098" f="125.065" m="65.51" cg="61.9"/>
<eng-data t="0.138" f="126.157" m="63.3881" cg="61.9"/>
<eng-data t="0.198" f="133.578" m="60.0973" cg="61.9"/>
<eng-data t="0.251" f="140.999" m="57.0243" cg="61.9"/>
<eng-data t="0.293" f="146.019" m="54.4788" cg="61.9"/>
<eng-data t="0.347" f="148.856" m="51.1164" cg="61.9"/>
<eng-data t="0.398" f="156.932" m="47.8233" cg="61.9"/>
<eng-data t="0.447" f="160.861" m="44.5352" cg="61.9"/>
<eng-data t="0.5" f="165.881" m="40.8784" cg="61.9"/>
<eng-data t="0.548" f="169.591" m="37.4781" cg="61.9"/>
<eng-data t="0.601" f="173.738" m="33.6357" cg="61.9"/>
<eng-data t="0.646" f="177.449" m="30.2987" cg="61.9"/>
<eng-data t="0.697" f="183.123" m="26.4156" cg="61.9"/>
<eng-data t="0.739" f="182.032" m="23.1771" cg="61.9"/>
<eng-data t="0.798" f="182.469" m="18.6359" cg="61.9"/>
<eng-data t="0.839" f="181.159" m="15.4878" cg="61.9"/>
<eng-data t="0.901" f="182.469" m="10.7271" cg="61.9"/>
<eng-data t="0.947" f="194.691" m="7.0636" cg="61.9"/>
<eng-data t="0.972" f="185.306" m="5.05758" cg="61.9"/>
<eng-data t="0.986" f="174.611" m="3.99357" cg="61.9"/>
<eng-data t="0.998" f="161.515" m="3.14184" cg="61.9"/>
<eng-data t="1." f="156.714" m="3.00745" cg="61.9"/>
<eng-data t="1.012" f="143.618" m="2.24642" cg="61.9"/>
<eng-data t="1.018" f="133.796" m="1.89495" cg="61.9"/>
<eng-data t="1.026" f="120.263" m="1.46577" cg="61.9"/>
<eng-data t="1.031" f="111.969" m="1.22057" cg="61.9"/>
<eng-data t="1.036" f="98.437" m="0.998424" cg="61.9"/>
<eng-data t="1.041" f="89.052" m="0.800472" cg="61.9"/>
<eng-data t="1.044" f="77.484" m="0.694974" cg="61.9"/>
<eng-data t="1.049" f="67.662" m="0.541727" cg="61.9"/>
<eng-data t="1.054" f="54.784" m="0.412447" cg="61.9"/>
<eng-data t="1.059" f="46.708" m="0.305291" cg="61.9"/>
<eng-data t="1.064" f="33.176" m="0.220949" cg="61.9"/>
<eng-data t="1.073" f="23.136" m="0.11393" cg="61.9"/>
<eng-data t="1.082" f="12.659" m="0.0459034" cg="61.9"/>
<eng-data t="1.098" f="0.873" m="0.000184344" cg="61.9"/>
<eng-data t="1.099" f="0." m="0." cg="61.9"/>
</data>
</engine>
<engine mfg="Aerotech" code="G339N" Type="reloadable" dia="38." len="97." initWt="190."
propWt="49." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="312.214" peakThrust="375." throatDia="0." exitDia="0." Itot="112.085"
burn-time="0.36" massFrac="25.79" Isp="233.25" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Created from TRA Certification Record issued 23 Nov 2006
Bill Wagstaff - 04/30/07
</comments>
<data>
<eng-data t="0." f="0." m="49." cg="48.5"/>
<eng-data t="0.009" f="371." m="48.2701" cg="48.5"/>
<eng-data t="0.05" f="375." m="41.5845" cg="48.5"/>
<eng-data t="0.1" f="375." m="33.3876" cg="48.5"/>
<eng-data t="0.15" f="364." m="25.3109" cg="48.5"/>
<eng-data t="0.2" f="349." m="17.5184" cg="48.5"/>
<eng-data t="0.25" f="310." m="10.3161" cg="48.5"/>
<eng-data t="0.3" f="264." m="4.04271" cg="48.5"/>
<eng-data t="0.324" f="257." m="1.30954" cg="48.5"/>
<eng-data t="0.342" f="39." m="0.144921" cg="48.5"/>
<eng-data t="0.359" f="0." m="0." cg="48.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="G38FJ" Type="single-use" dia="29." len="124."
initWt="126.4" propWt="59.7" delays="4,7" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="32.886" peakThrust="52.928" throatDia="0." exitDia="0." Itot="86.818"
burn-time="2.64" massFrac="47.23" Isp="148.29" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Aerotech G38FJ RASP.ENG file made by Tim Van Milligan
For RockSim www.RockSim.com
File Created March 2, 2005
Thrust curve supplied by Aerotech for the molded case G38FJ motors.
</comments>
<data>
<eng-data t="0." f="0." m="59.7" cg="62."/>
<eng-data t="0.024" f="52.928" m="59.2633" cg="62."/>
<eng-data t="0.171" f="48.424" m="54.1407" cg="62."/>
<eng-data t="0.497" f="45.045" m="43.6641" cg="62."/>
<eng-data t="1." f="42.23" m="28.5705" cg="62."/>
<eng-data t="1.279" f="39.978" m="20.6845" cg="62."/>
<eng-data t="1.498" f="36.599" m="14.9185" cg="62."/>
<eng-data t="1.783" f="30.406" m="8.35267" cg="62."/>
<eng-data t="2.011" f="23.086" m="4.15934" cg="62."/>
<eng-data t="2.272" f="10.135" m="1.17815" cg="62."/>
<eng-data t="2.467" f="3.941" m="0.234417" cg="62."/>
<eng-data t="2.64" f="0." m="0." cg="62."/>
</data>
</engine>
<engine mfg="Aerotech" code="G53FJ" Type="reloadable" dia="29." len="124." initWt="152."
propWt="60." delays="5,7,10" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="49.81" peakThrust="86.47" throatDia="0." exitDia="0." Itot="92.148"
burn-time="1.85" massFrac="39.47" Isp="156.61" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>G53FJ based on Aerotech instruction sheet by C. Kobel 12/9/07</comments>
<data>
<eng-data t="0." f="0." m="60." cg="62."/>
<eng-data t="0.012" f="44.898" m="59.8246" cg="62."/>
<eng-data t="0.031" f="71.504" m="59.1046" cg="62."/>
<eng-data t="0.064" f="80.234" m="57.4744" cg="62."/>
<eng-data t="0.081" f="83.976" m="56.5655" cg="62."/>
<eng-data t="0.1" f="86.47" m="55.5112" cg="62."/>
<eng-data t="0.15" f="84.599" m="52.7265" cg="62."/>
<eng-data t="0.2" f="81.897" m="50.0162" cg="62."/>
<eng-data t="0.3" f="78.571" m="44.792" cg="62."/>
<eng-data t="0.4" f="76.493" m="39.7437" cg="62."/>
<eng-data t="0.5" f="73.583" m="34.8577" cg="62."/>
<eng-data t="0.6" f="70.881" m="30.1545" cg="62."/>
<eng-data t="0.7" f="67.347" m="25.6543" cg="62."/>
<eng-data t="0.8" f="63.813" m="21.3842" cg="62."/>
<eng-data t="0.9" f="60.072" m="17.351" cg="62."/>
<eng-data t="1." f="54.667" m="13.6155" cg="62."/>
<eng-data t="1.1" f="47.392" m="10.2928" cg="62."/>
<eng-data t="1.2" f="39.909" m="7.45064" cg="62."/>
<eng-data t="1.3" f="32.426" m="5.09567" cg="62."/>
<eng-data t="1.4" f="25.983" m="3.19409" cg="62."/>
<eng-data t="1.5" f="20.578" m="1.67823" cg="62."/>
<eng-data t="1.6" f="10.601" m="0.663157" cg="62."/>
<eng-data t="1.7" f="3.949" m="0.189462" cg="62."/>
<eng-data t="1.8" f="1.247" m="0.0202989" cg="62."/>
<eng-data t="1.85" f="0." m="0." cg="62."/>
</data>
</engine>
<engine mfg="Aerotech" code="G72DM" Type="single-use" dia="29." len="156."
initWt="131.6" propWt="62.5" delays="14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="74.849" peakThrust="103.671" throatDia="0." exitDia="0."
Itot="105.537" burn-time="1.41" massFrac="47.49" Isp="172.19" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="62.5" cg="78."/>
<eng-data t="0.001" f="0.187354" m="62.4999" cg="78."/>
<eng-data t="0.025" f="5.28838" m="62.461" cg="78."/>
<eng-data t="0.038" f="13.595" m="62.3883" cg="78."/>
<eng-data t="0.055" f="38.1282" m="62.128" cg="78."/>
<eng-data t="0.097" f="59.7405" m="60.9109" cg="78."/>
<eng-data t="0.207" f="73.1239" m="56.5833" cg="78."/>
<eng-data t="0.319" f="83.6428" m="51.3843" cg="78."/>
<eng-data t="0.427" f="93.7455" m="45.7116" cg="78."/>
<eng-data t="0.64" f="97.6411" m="33.6409" cg="78."/>
<eng-data t="0.75" f="103.671" m="27.0838" cg="78."/>
<eng-data t="0.968" f="93.1495" m="14.379" cg="78."/>
<eng-data t="1.137" f="92.3494" m="5.09635" cg="78."/>
<eng-data t="1.245" f="31.1559" m="1.14675" cg="78."/>
<eng-data t="1.344" f="4.88298" m="0.0902964" cg="78."/>
<eng-data t="1.4" f="0.477307" m="0.00141332" cg="78."/>
<eng-data t="1.41" f="0." m="0." cg="78."/>
</data>
</engine>
<engine mfg="Aerotech" code="G80NT" Type="single-use" dia="29." len="123.83"
initWt="129." propWt="69." delays="4,7,10" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="79.735" peakThrust="106.954" throatDia="0." exitDia="0."
Itot="135.628" burn-time="1.7" massFrac="53.49" Isp="200.44" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>G80 New Blue Thunder</comments>
<data>
<eng-data t="0." f="0." m="69." cg="61.9125"/>
<eng-data t="0.013" f="89.054" m="68.7055" cg="61.9125"/>
<eng-data t="0.018" f="101.584" m="68.463" cg="61.9125"/>
<eng-data t="0.029" f="105.388" m="67.8839" cg="61.9125"/>
<eng-data t="0.047" f="102.927" m="66.9301" cg="61.9125"/>
<eng-data t="0.104" f="100.018" m="63.9876" cg="61.9125"/>
<eng-data t="0.19" f="102.255" m="59.5627" cg="61.9125"/>
<eng-data t="0.268" f="104.94" m="55.4517" cg="61.9125"/>
<eng-data t="0.306" f="104.269" m="53.4295" cg="61.9125"/>
<eng-data t="0.352" f="105.835" m="50.971" cg="61.9125"/>
<eng-data t="0.41" f="104.94" m="47.8614" cg="61.9125"/>
<eng-data t="0.432" f="106.73" m="46.6768" cg="61.9125"/>
<eng-data t="0.512" f="105.612" m="42.3557" cg="61.9125"/>
<eng-data t="0.563" f="106.954" m="39.5981" cg="61.9125"/>
<eng-data t="0.591" f="104.493" m="38.0921" cg="61.9125"/>
<eng-data t="0.62" f="106.283" m="36.5372" cg="61.9125"/>
<eng-data t="0.715" f="103.15" m="31.4762" cg="61.9125"/>
<eng-data t="0.76" f="103.374" m="29.1122" cg="61.9125"/>
<eng-data t="0.806" f="101.36" m="26.7166" cg="61.9125"/>
<eng-data t="0.848" f="102.032" m="24.5436" cg="61.9125"/>
<eng-data t="1.2" f="88.383" m="7.49412" cg="61.9125"/>
<eng-data t="1.243" f="77.866" m="5.6757" cg="61.9125"/>
<eng-data t="1.269" f="57.952" m="4.77744" cg="61.9125"/>
<eng-data t="1.302" f="44.079" m="3.92097" cg="61.9125"/>
<eng-data t="1.329" f="34.011" m="3.38464" cg="61.9125"/>
<eng-data t="1.367" f="26.403" m="2.80067" cg="61.9125"/>
<eng-data t="1.398" f="22.823" m="2.4125" cg="61.9125"/>
<eng-data t="1.433" f="20.585" m="2.02604" cg="61.9125"/>
<eng-data t="1.48" f="21.704" m="1.52046" cg="61.9125"/>
<eng-data t="1.508" f="20.809" m="1.21766" cg="61.9125"/>
<eng-data t="1.584" f="13.201" m="0.560172" cg="61.9125"/>
<eng-data t="1.604" f="11.635" m="0.433821" cg="61.9125"/>
<eng-data t="1.652" f="11.188" m="0.155156" cg="61.9125"/>
<eng-data t="1.683" f="5.37" m="0.0245875" cg="61.9125"/>
<eng-data t="1.701" f="0." m="0." cg="61.9125"/>
</data>
</engine>
<engine mfg="Aerotech" code="G12T-RC" Type="reloadable" dia="32." len="107."
initWt="131." propWt="51.1" delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="10.201" peakThrust="20.64" throatDia="0." exitDia="0." Itot="87.216"
burn-time="8.55" massFrac="39.01" Isp="174.04" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Aerotech G12RC RASP.ENG file made from NAR published data
File produced July 4, 2000
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="51.1" cg="53.5"/>
<eng-data t="0.03" f="18.549" m="50.937" cg="53.5"/>
<eng-data t="0.117" f="19.96" m="49.9555" cg="53.5"/>
<eng-data t="0.239" f="20.64" m="48.5045" cg="53.5"/>
<eng-data t="0.362" f="20.111" m="47.0361" cg="53.5"/>
<eng-data t="0.519" f="18.982" m="45.2381" cg="53.5"/>
<eng-data t="0.694" f="17.138" m="43.3864" cg="53.5"/>
<eng-data t="0.886" f="15.02" m="41.5776" cg="53.5"/>
<eng-data t="1.131" f="13.186" m="39.5532" cg="53.5"/>
<eng-data t="1.375" f="11.915" m="37.759" cg="53.5"/>
<eng-data t="1.689" f="11.069" m="35.6448" cg="53.5"/>
<eng-data t="2.021" f="10.363" m="33.5603" cg="53.5"/>
<eng-data t="2.422" f="10.232" m="31.141" cg="53.5"/>
<eng-data t="3.172" f="9.677" m="26.7667" cg="53.5"/>
<eng-data t="4.114" f="9.267" m="21.539" cg="53.5"/>
<eng-data t="5.039" f="8.857" m="16.6278" cg="53.5"/>
<eng-data t="6.137" f="8.733" m="10.9698" cg="53.5"/>
<eng-data t="7.132" f="8.607" m="5.91546" cg="53.5"/>
<eng-data t="7.795" f="8.335" m="2.62489" cg="53.5"/>
<eng-data t="7.952" f="8.196" m="1.86458" cg="53.5"/>
<eng-data t="8.074" f="8.055" m="1.28377" cg="53.5"/>
<eng-data t="8.179" f="6.924" m="0.823023" cg="53.5"/>
<eng-data t="8.319" f="4.661" m="0.347889" cg="53.5"/>
<eng-data t="8.476" f="1.973" m="0.0427712" cg="53.5"/>
<eng-data t="8.55" f="0." m="0." cg="53.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="H45W" Type="single-use" dia="38." len="202.7" initWt="364."
propWt="180." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="51.126" peakThrust="86.004" throatDia="0." exitDia="0." Itot="316.263"
burn-time="6.19" massFrac="49.45" Isp="179.17" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>From AT DMS announcement May 2014.</comments>
<data>
<eng-data t="0." f="0." m="180." cg="101.35"/>
<eng-data t="0.04" f="84.004" m="179.044" cg="101.35"/>
<eng-data t="0.854" f="86.004" m="139.663" cg="101.35"/>
<eng-data t="1.377" f="84.804" m="114.241" cg="101.35"/>
<eng-data t="2.046" f="79.204" m="83.0171" cg="101.35"/>
<eng-data t="2.70504" f="64.3275" m="56.0986" cg="101.35"/>
<eng-data t="3.35252" f="47.9532" m="35.4102" cg="101.35"/>
<eng-data t="4.40288" f="27.4854" m="12.8613" cg="101.35"/>
<eng-data t="5.042" f="16.001" m="4.95207" cg="101.35"/>
<eng-data t="5.429" f="9.2" m="2.17668" cg="101.35"/>
<eng-data t="5.82734" f="5.26316" m="0.537188" cg="101.35"/>
<eng-data t="6.186" f="0." m="0." cg="101.35"/>
</data>
</engine>
<engine mfg="Aerotech" code="H55W" Type="single-use" dia="29." len="191."
initWt="188.16" propWt="98.56" delays="6,10,14" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="58.693" peakThrust="98.019" throatDia="0."
exitDia="0." Itot="161.231" burn-time="2.75" massFrac="52.38" Isp="166.81"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>AeroTech H55W
Copyright Tripoli Motor Testing 1998 (www.tripoli.org)
provided by ThrustCurve.org (www.thrustcurve.org)
</comments>
<data>
<eng-data t="0." f="0." m="98.56" cg="95.5"/>
<eng-data t="0.052" f="92.752" m="97.0858" cg="95.5"/>
<eng-data t="0.159" f="98.019" m="90.8468" cg="95.5"/>
<eng-data t="0.268" f="95.821" m="84.3888" cg="95.5"/>
<eng-data t="0.375" f="96.162" m="78.1101" cg="95.5"/>
<eng-data t="0.482" f="97.146" m="71.7881" cg="95.5"/>
<eng-data t="0.591" f="96.927" m="65.3224" cg="95.5"/>
<eng-data t="0.699" f="95.915" m="58.9567" cg="95.5"/>
<eng-data t="0.806" f="94.447" m="52.731" cg="95.5"/>
<eng-data t="0.914" f="92.001" m="46.5763" cg="95.5"/>
<eng-data t="1.022" f="88.756" m="40.6095" cg="95.5"/>
<eng-data t="1.129" f="86.97" m="34.8625" cg="95.5"/>
<eng-data t="1.236" f="84.072" m="29.2687" cg="95.5"/>
<eng-data t="1.345" f="80.172" m="23.7968" cg="95.5"/>
<eng-data t="1.453" f="74.343" m="18.6962" cg="95.5"/>
<eng-data t="1.56" f="64.99" m="14.1394" cg="95.5"/>
<eng-data t="1.668" f="46.38" m="10.4631" cg="95.5"/>
<eng-data t="1.776" f="32.835" m="7.84816" cg="95.5"/>
<eng-data t="1.883" f="25.734" m="5.93269" cg="95.5"/>
<eng-data t="1.991" f="19.92" m="4.42565" cg="95.5"/>
<eng-data t="2.099" f="16.229" m="3.23237" cg="95.5"/>
<eng-data t="2.207" f="13.059" m="2.26557" cg="95.5"/>
<eng-data t="2.315" f="10.451" m="1.4895" cg="95.5"/>
<eng-data t="2.422" f="7.7" m="0.89588" cg="95.5"/>
<eng-data t="2.53" f="5.696" m="0.453677" cg="95.5"/>
<eng-data t="2.639" f="3.979" m="0.131347" cg="95.5"/>
<eng-data t="2.747" f="0." m="0." cg="95.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="H73J" Type="reloadable" dia="38." len="154." initWt="308.3"
propWt="140." delays="6,10" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="51.443" peakThrust="69.57" throatDia="0." exitDia="0." Itot="180.052"
burn-time="3.5" massFrac="45.41" Isp="131.14" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="140." cg="77."/>
<eng-data t="0." f="69.57" m="140." cg="77."/>
<eng-data t="0.5" f="61.43" m="114.535" cg="77."/>
<eng-data t="1.5" f="57.38" m="68.3444" cg="77."/>
<eng-data t="2.2" f="57.38" m="37.1131" cg="77."/>
<eng-data t="2.6" f="49.15" m="20.5465" cg="77."/>
<eng-data t="2.7" f="45.06" m="16.8838" cg="77."/>
<eng-data t="2.9" f="36.87" m="10.5133" cg="77."/>
<eng-data t="3.1" f="32.78" m="5.09765" cg="77."/>
<eng-data t="3.2" f="28.69" m="2.70784" cg="77."/>
<eng-data t="3.4" f="4.09" m="0.15901" cg="77."/>
<eng-data t="3.5" f="0." m="0." cg="77."/>
</data>
</engine>
<engine mfg="Aerotech" code="H97J" Type="reloadable" dia="29." len="239." initWt="281.5"
propWt="140.9" delays="6,10" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="115.78" peakThrust="127.92" throatDia="0." exitDia="0." Itot="185.248"
burn-time="1.6" massFrac="50.05" Isp="134.07" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="140.9" cg="119.5"/>
<eng-data t="0." f="117.56" m="140.9" cg="119.5"/>
<eng-data t="0.1" f="111.24" m="132.199" cg="119.5"/>
<eng-data t="0.2" f="111.24" m="123.738" cg="119.5"/>
<eng-data t="0.3" f="111.24" m="115.277" cg="119.5"/>
<eng-data t="0.4" f="116.8" m="106.604" cg="119.5"/>
<eng-data t="0.5" f="127.92" m="97.2977" cg="119.5"/>
<eng-data t="0.6" f="116.8" m="87.991" cg="119.5"/>
<eng-data t="0.7" f="122.36" m="78.8957" cg="119.5"/>
<eng-data t="1.1" f="127.92" m="40.823" cg="119.5"/>
<eng-data t="1.3" f="116.8" m="22.2096" cg="119.5"/>
<eng-data t="1.5" f="116.8" m="4.44192" cg="119.5"/>
<eng-data t="1.6" f="0." m="0." cg="119.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="H100W" Type="single-use" dia="38." len="157.5"
initWt="261." propWt="121." delays="10" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="95.248" peakThrust="130.245" throatDia="0." exitDia="0."
Itot="228.405" burn-time="2.4" massFrac="46.36" Isp="192.49" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>H100W DMS</comments>
<data>
<eng-data t="0." f="0." m="121." cg="78.75"/>
<eng-data t="0.004" f="46.916" m="120.95" cg="78.75"/>
<eng-data t="0.031" f="66.29" m="120.141" cg="78.75"/>
<eng-data t="0.047" f="97.334" m="119.447" cg="78.75"/>
<eng-data t="0.096" f="109.005" m="116.769" cg="78.75"/>
<eng-data t="0.193" f="116.474" m="110.976" cg="78.75"/>
<eng-data t="0.302" f="124.877" m="104.008" cg="78.75"/>
<eng-data t="0.391" f="123.01" m="98.1637" cg="78.75"/>
<eng-data t="0.498" f="127.911" m="91.0521" cg="78.75"/>
<eng-data t="0.604" f="128.845" m="83.8431" cg="78.75"/>
<eng-data t="0.696" f="130.245" m="77.5293" cg="78.75"/>
<eng-data t="0.798" f="128.612" m="70.5355" cg="78.75"/>
<eng-data t="0.902" f="128.845" m="63.4432" cg="78.75"/>
<eng-data t="0.998" f="127.445" m="56.9262" cg="78.75"/>
<eng-data t="1.098" f="126.511" m="50.1994" cg="78.75"/>
<eng-data t="1.2" f="116.941" m="43.6218" cg="78.75"/>
<eng-data t="1.3" f="114.607" m="37.4886" cg="78.75"/>
<eng-data t="1.4" f="110.172" m="31.5346" cg="78.75"/>
<eng-data t="1.5" f="98.268" m="26.0134" cg="78.75"/>
<eng-data t="1.6" f="90.798" m="21.0054" cg="78.75"/>
<eng-data t="1.7" f="80.061" m="16.4797" cg="78.75"/>
<eng-data t="1.802" f="68.624" m="12.4626" cg="78.75"/>
<eng-data t="1.9" f="65.356" m="8.98469" cg="78.75"/>
<eng-data t="2." f="56.953" m="5.74497" cg="78.75"/>
<eng-data t="2.1" f="49.484" m="2.92566" cg="78.75"/>
<eng-data t="2.202" f="25.209" m="0.907619" cg="78.75"/>
<eng-data t="2.298" f="5.135" m="0.136016" cg="78.75"/>
<eng-data t="2.398" f="0." m="0." cg="78.75"/>
</data>
</engine>
<engine mfg="Aerotech" code="H112J" Type="reloadable" dia="38." len="191."
initWt="384.8" propWt="187.5" delays="6,10,14" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="82.554" peakThrust="126.62" throatDia="0."
exitDia="0." Itot="280.685" burn-time="3.4" massFrac="48.73" Isp="152.65"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Data Entered by Tim Van Milligan
For RockSim Users. http://www.rocksim.com
Based on Aerotech's RMS 38/240-360 Black Jack Instr. Sheet
</comments>
<data>
<eng-data t="0." f="0." m="187.5" cg="95.5"/>
<eng-data t="0.1705" f="120.014" m="180.665" cg="95.5"/>
<eng-data t="0.2" f="126.62" m="178.235" cg="95.5"/>
<eng-data t="0.224" f="109.003" m="176.347" cg="95.5"/>
<eng-data t="0.278" f="106.801" m="172.454" cg="95.5"/>
<eng-data t="0.378" f="107.902" m="165.283" cg="95.5"/>
<eng-data t="0.502" f="113.408" m="156.117" cg="95.5"/>
<eng-data t="0.996" f="103.498" m="120.328" cg="95.5"/>
<eng-data t="1.499" f="103.498" m="85.552" cg="95.5"/>
<eng-data t="1.731" f="96.892" m="70.0239" cg="95.5"/>
<eng-data t="2.017" f="92.487" m="51.9335" cg="95.5"/>
<eng-data t="2.496" f="73.77" m="25.3343" cg="95.5"/>
<eng-data t="2.998" f="42.94" m="5.76554" cg="95.5"/>
<eng-data t="3.4" f="0." m="0." cg="95.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="H123W" Type="reloadable" dia="38." len="154."
initWt="293.3" propWt="125." delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="81.308" peakThrust="138.42" throatDia="0." exitDia="0." Itot="211.4"
burn-time="2.6" massFrac="42.62" Isp="172.45" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="125." cg="77."/>
<eng-data t="0." f="138.42" m="125." cg="77."/>
<eng-data t="0.2" f="116.45" m="109.93" cg="77."/>
<eng-data t="0.6" f="116.45" m="82.3872" cg="77."/>
<eng-data t="0.7" f="112.18" m="75.6278" cg="77."/>
<eng-data t="0.8" f="107.82" m="69.1235" cg="77."/>
<eng-data t="1.3" f="86.29" m="40.4295" cg="77."/>
<eng-data t="1.5" f="81.93" m="30.4827" cg="77."/>
<eng-data t="1.8" f="64.72" m="17.4757" cg="77."/>
<eng-data t="2.1" f="47.46" m="7.526" cg="77."/>
<eng-data t="2.2" f="43.15" m="4.84714" cg="77."/>
<eng-data t="2.3" f="30.2" m="2.67857" cg="77."/>
<eng-data t="2.6" f="0." m="0." cg="77."/>
</data>
</engine>
<engine mfg="Aerotech" code="H128W" Type="reloadable" dia="29." len="195."
initWt="214.5" propWt="92.2" delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="103.863" peakThrust="157.28" throatDia="0." exitDia="0."
Itot="155.795" burn-time="1.5" massFrac="42.98" Isp="172.31" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="92.2" cg="97.5"/>
<eng-data t="0." f="0.62" m="92.2" cg="97.5"/>
<eng-data t="0.1" f="157.28" m="87.5277" cg="97.5"/>
<eng-data t="0.2" f="129.75" m="79.0344" cg="97.5"/>
<eng-data t="0.3" f="129.75" m="71.3558" cg="97.5"/>
<eng-data t="0.4" f="125.26" m="63.81" cg="97.5"/>
<eng-data t="0.5" f="125.26" m="56.3971" cg="97.5"/>
<eng-data t="0.9" f="125.26" m="26.7454" cg="97.5"/>
<eng-data t="1." f="120.81" m="19.4641" cg="97.5"/>
<eng-data t="1.2" f="102.93" m="6.22311" cg="97.5"/>
<eng-data t="1.3" f="44.75" m="1.85323" cg="97.5"/>
<eng-data t="1.4" f="8.94" m="0.264536" cg="97.5"/>
<eng-data t="1.5" f="0." m="0." cg="97.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="H130W" Type="reloadable" dia="38." len="152." initWt="237."
propWt="120." delays="14" auto-calc-mass="1" auto-calc-cg="1" avgThrust="128.733"
peakThrust="260.237" throatDia="0." exitDia="0." Itot="210.221" burn-time="1.63"
massFrac="50.63" Isp="178.64" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<comments>38/240 Non hazmat H123 equivalalent</comments>
<data>
<eng-data t="0." f="0." m="120." cg="76."/>
<eng-data t="0.011" f="90.913" m="119.715" cg="76."/>
<eng-data t="0.029" f="180.689" m="118.319" cg="76."/>
<eng-data t="0.04" f="207.962" m="117.099" cg="76."/>
<eng-data t="0.055" f="235.236" m="115.202" cg="76."/>
<eng-data t="0.086" f="260.237" m="110.818" cg="76."/>
<eng-data t="0.11" f="250.578" m="107.319" cg="76."/>
<eng-data t="0.147" f="246.6" m="102.068" cg="76."/>
<eng-data t="0.19" f="252.85" m="95.9387" cg="76."/>
<eng-data t="0.226" f="242.623" m="90.8477" cg="76."/>
<eng-data t="0.266" f="235.236" m="85.3922" cg="76."/>
<eng-data t="0.304" f="238.645" m="80.2527" cg="76."/>
<eng-data t="0.348" f="226.713" m="74.4086" cg="76."/>
<eng-data t="0.4" f="215.349" m="67.8477" cg="76."/>
<eng-data t="0.419" f="220.463" m="65.4844" cg="76."/>
<eng-data t="0.432" f="207.962" m="63.8947" cg="76."/>
<eng-data t="0.531" f="177.279" m="53.0094" cg="76."/>
<eng-data t="0.601" f="151.71" m="46.4365" cg="76."/>
<eng-data t="1.184" f="69.321" m="9.65773" cg="76."/>
<eng-data t="1.216" f="69.321" m="8.39148" cg="76."/>
<eng-data t="1.351" f="46.593" m="3.92521" cg="76."/>
<eng-data t="1.402" f="40.342" m="2.65977" cg="76."/>
<eng-data t="1.633" f="0." m="0." cg="76."/>
</data>
</engine>
<engine mfg="Aerotech" code="H135W" Type="single-use" dia="29." len="216." initWt="212."
propWt="82." delays="14" auto-calc-mass="1" auto-calc-cg="1" avgThrust="110.537"
peakThrust="159.806" throatDia="0." exitDia="0." Itot="229.032" burn-time="2.07"
massFrac="38.68" Isp="284.81" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<comments>AeroTech Pro-SU 29mm H135 14sec adjustable delay.
From Tripoli Data Sheet updated 2013/02/10
Created by Robert Belknap 2013/03/04
</comments>
<data>
<eng-data t="0." f="0." m="82." cg="108."/>
<eng-data t="0.014" f="159.806" m="81.5995" cg="108."/>
<eng-data t="0.045" f="110.931" m="80.0971" cg="108."/>
<eng-data t="0.104" f="144.43" m="77.4" cg="108."/>
<eng-data t="0.131" f="135.643" m="76.0463" cg="108."/>
<eng-data t="0.252" f="154.315" m="69.7656" cg="108."/>
<eng-data t="0.293" f="130.701" m="67.6737" cg="108."/>
<eng-data t="0.387" f="149.921" m="62.9515" cg="108."/>
<eng-data t="1.005" f="140.037" m="30.8732" cg="108."/>
<eng-data t="1.261" f="119.168" m="18.9944" cg="108."/>
<eng-data t="1.297" f="142.233" m="17.3098" cg="108."/>
<eng-data t="1.324" f="109.833" m="16.0915" cg="108."/>
<eng-data t="1.387" f="120.267" m="13.4964" cg="108."/>
<eng-data t="1.518" f="110.382" m="8.08751" cg="108."/>
<eng-data t="1.595" f="80.727" m="5.45324" cg="108."/>
<eng-data t="1.685" f="60.408" m="3.17938" cg="108."/>
<eng-data t="1.797" f="33.499" m="1.29658" cg="108."/>
<eng-data t="1.896" f="14.278" m="0.449851" cg="108."/>
<eng-data t="2.072" f="0." m="0." cg="108."/>
</data>
</engine>
<engine mfg="Aerotech" code="H148R" Type="reloadable" dia="38." len="152." initWt="313."
propWt="150." delays="6,11,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="142.786" peakThrust="192.5" throatDia="0." exitDia="0." Itot="214.18"
burn-time="1.5" massFrac="47.92" Isp="145.6" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="150." cg="76."/>
<eng-data t="0.03" f="77.23" m="149.189" cg="76."/>
<eng-data t="0.09" f="174.3" m="143.904" cg="76."/>
<eng-data t="0.15" f="185.05" m="136.354" cg="76."/>
<eng-data t="0.21" f="190.46" m="128.464" cg="76."/>
<eng-data t="0.27" f="192.5" m="120.418" cg="76."/>
<eng-data t="0.33" f="192." m="112.34" cg="76."/>
<eng-data t="0.39" f="188.79" m="104.339" cg="76."/>
<eng-data t="0.45" f="187.55" m="96.432" cg="76."/>
<eng-data t="0.51" f="182.7" m="88.6529" cg="76."/>
<eng-data t="0.57" f="178.15" m="81.0713" cg="76."/>
<eng-data t="0.63" f="172.91" m="73.6954" cg="76."/>
<eng-data t="0.69" f="169.61" m="66.4989" cg="76."/>
<eng-data t="0.75" f="164.51" m="59.4789" cg="76."/>
<eng-data t="0.81" f="158.38" m="52.6948" cg="76."/>
<eng-data t="0.87" f="153.02" m="46.1522" cg="76."/>
<eng-data t="0.93" f="146.81" m="39.8526" cg="76."/>
<eng-data t="0.99" f="139.44" m="33.8384" cg="76."/>
<eng-data t="1.05" f="132." m="28.1353" cg="76."/>
<eng-data t="1.11" f="123.27" m="22.772" cg="76."/>
<eng-data t="1.17" f="112.56" m="17.8171" cg="76."/>
<eng-data t="1.23" f="104.74" m="13.2516" cg="76."/>
<eng-data t="1.29" f="97.66" m="8.99907" cg="76."/>
<eng-data t="1.35" f="94.93" m="4.95268" cg="76."/>
<eng-data t="1.41" f="60.64" m="1.68409" cg="76."/>
<eng-data t="1.47" f="13.01" m="0.136673" cg="76."/>
<eng-data t="1.5" f="0." m="0." cg="76."/>
</data>
</engine>
<engine mfg="Aerotech" code="H165R" Type="reloadable" dia="29." len="194." initWt="204."
propWt="91." delays="10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="153.221" peakThrust="190.49" throatDia="0." exitDia="0."
Itot="160.882" burn-time="1.05" massFrac="44.61" Isp="180.28" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="91." cg="97."/>
<eng-data t="0.02" f="55.05" m="90.6886" cg="97."/>
<eng-data t="0.06" f="157.26" m="88.2868" cg="97."/>
<eng-data t="0.1" f="168.51" m="84.6015" cg="97."/>
<eng-data t="0.14" f="173.22" m="80.7356" cg="97."/>
<eng-data t="0.19" f="179.24" m="75.7516" cg="97."/>
<eng-data t="0.23" f="183.95" m="71.6429" cg="97."/>
<eng-data t="0.27" f="187.87" m="67.4367" cg="97."/>
<eng-data t="0.31" f="188.13" m="63.1831" cg="97."/>
<eng-data t="0.36" f="188.92" m="57.8513" cg="97."/>
<eng-data t="0.4" f="190.49" m="53.5592" cg="97."/>
<eng-data t="0.44" f="187.35" m="49.2849" cg="97."/>
<eng-data t="0.48" f="189.18" m="45.0253" cg="97."/>
<eng-data t="0.53" f="186.55" m="39.7122" cg="97."/>
<eng-data t="0.57" f="185.52" m="35.5031" cg="97."/>
<eng-data t="0.61" f="180.81" m="31.3589" cg="97."/>
<eng-data t="0.65" f="177.67" m="27.3036" cg="97."/>
<eng-data t="0.69" f="170.6" m="23.3637" cg="97."/>
<eng-data t="0.74" f="167.2" m="18.587" cg="97."/>
<eng-data t="0.78" f="158.83" m="14.8987" cg="97."/>
<eng-data t="0.82" f="155.69" m="11.3407" cg="97."/>
<eng-data t="0.86" f="153.33" m="7.84483" cg="97."/>
<eng-data t="0.91" f="136.32" m="3.74895" cg="97."/>
<eng-data t="0.95" f="73.53" m="1.37499" cg="97."/>
<eng-data t="0.99" f="20.67" m="0.309344" cg="97."/>
<eng-data t="1.03" f="4.45" m="0.0251706" cg="97."/>
<eng-data t="1.05" f="0." m="0." cg="97."/>
</data>
</engine>
<engine mfg="Aerotech" code="H170M" Type="reloadable" dia="38." len="191." initWt="330."
propWt="182.5" delays="14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="148.737" peakThrust="205.821" throatDia="0." exitDia="0." Itot="318."
burn-time="2.14" massFrac="55.3" Isp="177.68" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>AT H170 Metalstorm for 38-360</comments>
<data>
<eng-data t="0." f="0." m="182.5" cg="95.5"/>
<eng-data t="0.017" f="182.491" m="181.61" cg="95.5"/>
<eng-data t="0.032" f="199.6" m="179.965" cg="95.5"/>
<eng-data t="0.104" f="195.971" m="171.793" cg="95.5"/>
<eng-data t="0.205" f="180.936" m="160.869" cg="95.5"/>
<eng-data t="0.292" f="188.712" m="151.641" cg="95.5"/>
<eng-data t="0.314" f="198.563" m="149.196" cg="95.5"/>
<eng-data t="0.324" f="187.157" m="148.089" cg="95.5"/>
<eng-data t="0.364" f="180.936" m="143.864" cg="95.5"/>
<eng-data t="0.423" f="192.86" m="137.536" cg="95.5"/>
<eng-data t="0.458" f="189.231" m="133.698" cg="95.5"/>
<eng-data t="0.574" f="197.526" m="120.825" cg="95.5"/>
<eng-data t="0.616" f="205.821" m="115.964" cg="95.5"/>
<eng-data t="0.663" f="190.268" m="110.622" cg="95.5"/>
<eng-data t="0.71" f="190.268" m="105.49" cg="95.5"/>
<eng-data t="0.735" f="197.526" m="102.708" cg="95.5"/>
<eng-data t="0.876" f="188.712" m="87.0805" cg="95.5"/>
<eng-data t="0.963" f="193.897" m="77.5288" cg="95.5"/>
<eng-data t="1.22" f="176.788" m="50.1923" cg="95.5"/>
<eng-data t="1.245" f="185.083" m="47.5963" cg="95.5"/>
<eng-data t="1.279" f="172.122" m="44.1113" cg="95.5"/>
<eng-data t="1.46" f="152.422" m="27.2552" cg="95.5"/>
<eng-data t="1.47" f="159.68" m="26.3596" cg="95.5"/>
<eng-data t="1.515" f="147.237" m="22.3964" cg="95.5"/>
<eng-data t="1.591" f="136.35" m="16.2119" cg="95.5"/>
<eng-data t="1.7" f="131.165" m="7.84471" cg="95.5"/>
<eng-data t="1.73" f="114.575" m="5.72926" cg="95.5"/>
<eng-data t="1.782" f="67.397" m="3.01398" cg="95.5"/>
<eng-data t="1.824" f="39.401" m="1.72686" cg="95.5"/>
<eng-data t="1.886" f="18.145" m="0.70307" cg="95.5"/>
<eng-data t="1.93" f="8.813" m="0.362704" cg="95.5"/>
<eng-data t="2." f="3.111" m="0.123193" cg="95.5"/>
<eng-data t="2.138" f="0." m="0." cg="95.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="H180W" Type="reloadable" dia="29." len="239."
initWt="263.6" propWt="123." delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="151.459" peakThrust="305.84" throatDia="0." exitDia="0."
Itot="212.042" burn-time="1.4" massFrac="46.66" Isp="175.79" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="123." cg="119.5"/>
<eng-data t="0." f="305.84" m="123." cg="119.5"/>
<eng-data t="0.1" f="196.56" m="108.429" cg="119.5"/>
<eng-data t="0.3" f="187.79" m="86.1335" cg="119.5"/>
<eng-data t="0.5" f="200.87" m="63.5884" cg="119.5"/>
<eng-data t="0.6" f="174.67" m="52.6964" cg="119.5"/>
<eng-data t="0.7" f="161.6" m="42.9433" cg="119.5"/>
<eng-data t="0.8" f="152.88" m="33.8223" cg="119.5"/>
<eng-data t="0.9" f="144.12" m="25.2082" cg="119.5"/>
<eng-data t="1." f="139.71" m="16.9761" cg="119.5"/>
<eng-data t="1.1" f="135.4" m="8.99692" cg="119.5"/>
<eng-data t="1.2" f="74.28" m="2.91544" cg="119.5"/>
<eng-data t="1.3" f="13.12" m="0.380527" cg="119.5"/>
<eng-data t="1.4" f="0." m="0." cg="119.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="H182R" Type="single-use" dia="29." len="203.2"
initWt="207." propWt="115." delays="14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="175.017" peakThrust="200.81" throatDia="0." exitDia="0."
Itot="216.146" burn-time="1.24" massFrac="55.56" Isp="191.66" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>From AT DMS announcement May 2014.</comments>
<data>
<eng-data t="0." f="0." m="115." cg="101.6"/>
<eng-data t="0.007" f="82.404" m="114.847" cg="101.6"/>
<eng-data t="0.031" f="159.208" m="113.304" cg="101.6"/>
<eng-data t="0.091" f="158.408" m="108.234" cg="101.6"/>
<eng-data t="0.186" f="182.409" m="99.6211" cg="101.6"/>
<eng-data t="0.5" f="192.009" m="68.3455" cg="101.6"/>
<eng-data t="0.904" f="188.809" m="27.4176" cg="101.6"/>
<eng-data t="1.054" f="175.209" m="12.8919" cg="101.6"/>
<eng-data t="1.106" f="180.809" m="7.96707" cg="101.6"/>
<eng-data t="1.144" f="200.81" m="4.10932" cg="101.6"/>
<eng-data t="1.163" f="162.408" m="2.27345" cg="101.6"/>
<eng-data t="1.201" f="36.802" m="0.259654" cg="101.6"/>
<eng-data t="1.212" f="16.801" m="0.102798" cg="101.6"/>
<eng-data t="1.235" f="0." m="0." cg="101.6"/>
</data>
</engine>
<engine mfg="Aerotech" code="H210R" Type="reloadable" dia="29." len="238." initWt="249."
propWt="122." delays="10,1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="207.998" peakThrust="260.22" throatDia="0." exitDia="0."
Itot="210.078" burn-time="1.01" massFrac="49." Isp="175.59" tDiv="10" tStep="-1."
tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="122." cg="119."/>
<eng-data t="0.02" f="105.92" m="121.385" cg="119."/>
<eng-data t="0.06" f="211.29" m="117.701" cg="119."/>
<eng-data t="0.1" f="219.77" m="112.694" cg="119."/>
<eng-data t="0.14" f="229.64" m="107.474" cg="119."/>
<eng-data t="0.18" f="235.08" m="102.077" cg="119."/>
<eng-data t="0.22" f="241.59" m="96.5402" cg="119."/>
<eng-data t="0.26" f="242.71" m="90.9152" cg="119."/>
<eng-data t="0.3" f="245.35" m="85.2465" cg="119."/>
<eng-data t="0.34" f="249.1" m="79.5036" cg="119."/>
<eng-data t="0.38" f="253.41" m="73.6671" cg="119."/>
<eng-data t="0.42" f="258.55" m="67.7208" cg="119."/>
<eng-data t="0.46" f="260.22" m="61.6955" cg="119."/>
<eng-data t="0.5" f="258." m="55.6765" cg="119."/>
<eng-data t="0.54" f="259.25" m="49.6688" cg="119."/>
<eng-data t="0.58" f="256.61" m="43.6772" cg="119."/>
<eng-data t="0.62" f="252.44" m="37.7647" cg="119."/>
<eng-data t="0.66" f="245.06" m="31.9864" cg="119."/>
<eng-data t="0.7" f="219.91" m="26.5859" cg="119."/>
<eng-data t="0.74" f="209.34" m="21.6003" cg="119."/>
<eng-data t="0.78" f="200.59" m="16.8391" cg="119."/>
<eng-data t="0.82" f="193.57" m="12.261" cg="119."/>
<eng-data t="0.86" f="184.32" m="7.87196" cg="119."/>
<eng-data t="0.91" f="153.88" m="2.96184" cg="119."/>
<eng-data t="0.94" f="58.24" m="1.11405" cg="119."/>
<eng-data t="0.99" f="13.21" m="0.0767152" cg="119."/>
<eng-data t="1.01" f="0." m="0." cg="119."/>
</data>
</engine>
<engine mfg="Aerotech" code="H220T" Type="reloadable" dia="29." len="238." initWt="246."
propWt="106.4" delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="215.406" peakThrust="275.73" throatDia="0." exitDia="0."
Itot="215.406" burn-time="1." massFrac="43.25" Isp="206.44" tDiv="10" tStep="-1."
tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Aerotech H220 RASP.ENG file made from NAR published data
File produced July 4, 2000
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="106.4" cg="119."/>
<eng-data t="0.007" f="214.072" m="106.03" cg="119."/>
<eng-data t="0.013" f="251.967" m="105.339" cg="119."/>
<eng-data t="0.024" f="275.73" m="103.906" cg="119."/>
<eng-data t="0.032" f="265.065" m="102.837" cg="119."/>
<eng-data t="0.036" f="269.464" m="102.309" cg="119."/>
<eng-data t="0.058" f="250.567" m="99.4836" cg="119."/>
<eng-data t="0.098" f="250.567" m="94.5329" cg="119."/>
<eng-data t="0.165" f="256.466" m="86.1428" cg="119."/>
<eng-data t="0.269" f="259.566" m="72.8883" cg="119."/>
<eng-data t="0.408" f="259.766" m="55.0598" cg="119."/>
<eng-data t="0.449" f="256.966" m="49.8274" cg="119."/>
<eng-data t="0.463" f="261.366" m="48.0352" cg="119."/>
<eng-data t="0.483" f="254.066" m="45.4892" cg="119."/>
<eng-data t="0.576" f="248.367" m="33.949" cg="119."/>
<eng-data t="0.657" f="244.168" m="24.0958" cg="119."/>
<eng-data t="0.688" f="245.668" m="20.3455" cg="119."/>
<eng-data t="0.742" f="245.668" m="13.7927" cg="119."/>
<eng-data t="0.756" f="241.368" m="12.1087" cg="119."/>
<eng-data t="0.775" f="222.471" m="9.93214" cg="119."/>
<eng-data t="0.793" f="210.872" m="8.00569" cg="119."/>
<eng-data t="0.813" f="187.575" m="6.03756" cg="119."/>
<eng-data t="0.834" f="161.379" m="4.22771" cg="119."/>
<eng-data t="0.852" f="135.182" m="2.90933" cg="119."/>
<eng-data t="0.866" f="98.817" m="2.10024" cg="119."/>
<eng-data t="0.88" f="65.351" m="1.53261" cg="119."/>
<eng-data t="0.897" f="47.903" m="1.0571" cg="119."/>
<eng-data t="0.917" f="36.285" m="0.641254" cg="119."/>
<eng-data t="0.939" f="23.206" m="0.318012" cg="119."/>
<eng-data t="0.964" f="11.598" m="0.103119" cg="119."/>
<eng-data t="1." f="0." m="0." cg="119."/>
</data>
</engine>
<engine mfg="Aerotech" code="H238T" Type="reloadable" dia="29." len="195."
initWt="202.1" propWt="79.8" delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="204.002" peakThrust="265.1" throatDia="0." exitDia="0." Itot="163.202"
burn-time="0.8" massFrac="39.49" Isp="208.55" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="79.8" cg="97.5"/>
<eng-data t="0." f="239.12" m="79.8" cg="97.5"/>
<eng-data t="0.1" f="239.04" m="68.1098" cg="97.5"/>
<eng-data t="0.2" f="252.07" m="56.1031" cg="97.5"/>
<eng-data t="0.3" f="265.1" m="43.4592" cg="97.5"/>
<eng-data t="0.4" f="265.1" m="30.4967" cg="97.5"/>
<eng-data t="0.5" f="221.69" m="18.5956" cg="97.5"/>
<eng-data t="0.6" f="191.22" m="8.50065" cg="97.5"/>
<eng-data t="0.7" f="78.24" m="1.91283" cg="97.5"/>
<eng-data t="0.8" f="0." m="0." cg="97.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="H242T" Type="reloadable" dia="38." len="154."
initWt="279.1" propWt="110.8" delays="6,10,14" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="195.182" peakThrust="286.05" throatDia="0."
exitDia="0." Itot="234.218" burn-time="1.2" massFrac="39.7" Isp="215.56"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="110.8" cg="77."/>
<eng-data t="0." f="286.05" m="110.8" cg="77."/>
<eng-data t="0.1" f="255.09" m="98.0003" cg="77."/>
<eng-data t="0.3" f="241.88" m="74.4906" cg="77."/>
<eng-data t="0.4" f="241.88" m="63.0481" cg="77."/>
<eng-data t="0.5" f="233.16" m="51.8119" cg="77."/>
<eng-data t="0.7" f="211.15" m="30.7933" cg="77."/>
<eng-data t="0.8" f="193.53" m="21.2213" cg="77."/>
<eng-data t="0.9" f="171.51" m="12.587" cg="77."/>
<eng-data t="1." f="118.76" m="5.72122" cg="77."/>
<eng-data t="1.1" f="61.56" m="1.45609" cg="77."/>
<eng-data t="1.2" f="0." m="0." cg="77."/>
</data>
</engine>
<engine mfg="Aerotech" code="H250G" Type="reloadable" dia="29." len="228.93"
initWt="256." propWt="116.3" delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="251.105" peakThrust="320.655" throatDia="0." exitDia="0."
Itot="231.017" burn-time="0.92" massFrac="0." Isp="0." tDiv="10" tStep="-1."
tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>By Tobin Yehle,
11/11/07.</comments>
<data>
<eng-data t="0." f="0." m="0." cg="0."/>
<eng-data t="0.00250627" f="88.6915" m="0." cg="0."/>
<eng-data t="0.0125313" f="177.383" m="0." cg="0."/>
<eng-data t="0.0300752" f="279.719" m="0." cg="0."/>
<eng-data t="0.0726817" f="311.103" m="0." cg="0."/>
<eng-data t="0.145363" f="320.654" m="0." cg="0."/>
<eng-data t="0.24812" f="311.103" m="0." cg="0."/>
<eng-data t="0.308271" f="297.458" m="0." cg="0."/>
<eng-data t="0.398496" f="282.448" m="0." cg="0."/>
<eng-data t="0.45614" f="270.168" m="0." cg="0."/>
<eng-data t="0.593985" f="238.785" m="0." cg="0."/>
<eng-data t="0.691729" f="221.047" m="0." cg="0."/>
<eng-data t="0.799499" f="218.318" m="0." cg="0."/>
<eng-data t="0.83208" f="210.131" m="0." cg="0."/>
<eng-data t="0.844612" f="189.663" m="0." cg="0."/>
<eng-data t="0.907268" f="13.6449" m="0." cg="0."/>
<eng-data t="0.92" f="0." m="0." cg="0."/>
</data>
</engine>
<engine mfg="Aerotech" code="H268R" Type="reloadable" dia="29." len="333." initWt="362."
propWt="184." delays="10,14,1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="262.483" peakThrust="332.45" throatDia="0." exitDia="0." Itot="309.73"
burn-time="1.18" massFrac="50.83" Isp="171.65" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="184." cg="166.5"/>
<eng-data t="0.02" f="268.1" m="182.407" cg="166.5"/>
<eng-data t="0.07" f="332.45" m="173.488" cg="166.5"/>
<eng-data t="0.12" f="312.43" m="163.911" cg="166.5"/>
<eng-data t="0.16" f="306.81" m="156.553" cg="166.5"/>
<eng-data t="0.21" f="305.76" m="147.456" cg="166.5"/>
<eng-data t="0.26" f="306.58" m="138.361" cg="166.5"/>
<eng-data t="0.31" f="312.55" m="129.166" cg="166.5"/>
<eng-data t="0.35" f="319.69" m="121.654" cg="166.5"/>
<eng-data t="0.4" f="321.23" m="112.136" cg="166.5"/>
<eng-data t="0.45" f="320.97" m="102.598" cg="166.5"/>
<eng-data t="0.5" f="321.21" m="93.0605" cg="166.5"/>
<eng-data t="0.54" f="321.79" m="85.4208" cg="166.5"/>
<eng-data t="0.59" f="323.32" m="75.8399" cg="166.5"/>
<eng-data t="0.64" f="322.85" m="66.2432" cg="166.5"/>
<eng-data t="0.69" f="307.04" m="56.8883" cg="166.5"/>
<eng-data t="0.73" f="291.59" m="49.7758" cg="166.5"/>
<eng-data t="0.78" f="277.71" m="41.3207" cg="166.5"/>
<eng-data t="0.83" f="267.13" m="33.229" cg="166.5"/>
<eng-data t="0.87" f="257.53" m="26.9953" cg="166.5"/>
<eng-data t="0.92" f="252.85" m="19.4153" cg="166.5"/>
<eng-data t="0.97" f="222.65" m="12.3534" cg="166.5"/>
<eng-data t="1.02" f="159.67" m="6.67528" cg="166.5"/>
<eng-data t="1.06" f="108.75" m="3.4861" cg="166.5"/>
<eng-data t="1.11" f="52.09" m="1.09736" cg="166.5"/>
<eng-data t="1.16" f="15.57" m="0.092496" cg="166.5"/>
<eng-data t="1.18" f="0." m="0." cg="166.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="H669N" Type="reloadable" dia="38." len="152." initWt="252."
propWt="96." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="667.931" peakThrust="1178." throatDia="0." exitDia="0." Itot="219.749"
burn-time="0.33" massFrac="38.1" Isp="233.42" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Greg Gardner - 09/15/06</comments>
<data>
<eng-data t="0." f="0." m="96." cg="76."/>
<eng-data t="0.003" f="141." m="95.9076" cg="76."/>
<eng-data t="0.006" f="523." m="95.4725" cg="76."/>
<eng-data t="0.009" f="934." m="94.5177" cg="76."/>
<eng-data t="0.012" f="1178." m="93.1338" cg="76."/>
<eng-data t="0.016" f="926." m="91.2954" cg="76."/>
<eng-data t="0.019" f="684." m="90.2404" cg="76."/>
<eng-data t="0.022" f="487." m="89.4731" cg="76."/>
<eng-data t="0.025" f="415." m="88.882" cg="76."/>
<eng-data t="0.028" f="622." m="88.2025" cg="76."/>
<eng-data t="0.031" f="801." m="87.27" cg="76."/>
<eng-data t="0.0325" f="906." m="86.7107" cg="76."/>
<eng-data t="0.034" f="866." m="86.1301" cg="76."/>
<eng-data t="0.037" f="755." m="85.0679" cg="76."/>
<eng-data t="0.04" f="737." m="84.0902" cg="76."/>
<eng-data t="0.043" f="666." m="83.1708" cg="76."/>
<eng-data t="0.047" f="737." m="81.945" cg="76."/>
<eng-data t="0.0485" f="802." m="81.4407" cg="76."/>
<eng-data t="0.05" f="755." m="80.9306" cg="76."/>
<eng-data t="0.053" f="791." m="79.9175" cg="76."/>
<eng-data t="0.056" f="765." m="78.8979" cg="76."/>
<eng-data t="0.059" f="755." m="77.9018" cg="76."/>
<eng-data t="0.062" f="747." m="76.9176" cg="76."/>
<eng-data t="0.069" f="737." m="74.6485" cg="76."/>
<eng-data t="0.075" f="761." m="72.6852" cg="76."/>
<eng-data t="0.082" f="755." m="70.3673" cg="76."/>
<eng-data t="0.088" f="729." m="68.4223" cg="76."/>
<eng-data t="0.093" f="741." m="66.8169" cg="76."/>
<eng-data t="0.1" f="751." m="64.5356" cg="76."/>
<eng-data t="0.2" f="703." m="32.7758" cg="76."/>
<eng-data t="0.25" f="640." m="18.1081" cg="76."/>
<eng-data t="0.3" f="586." m="4.71832" cg="76."/>
<eng-data t="0.306" f="584." m="3.18494" cg="76."/>
<eng-data t="0.309" f="576." m="2.4248" cg="76."/>
<eng-data t="0.312" f="506." m="1.71577" cg="76."/>
<eng-data t="0.318" f="292." m="0.669927" cg="76."/>
<eng-data t="0.325" f="93." m="0.0812563" cg="76."/>
<eng-data t="0.329" f="0." m="0." cg="76."/>
</data>
</engine>
<engine mfg="Aerotech" code="H999N" Type="reloadable" dia="38." len="203." initWt="331."
propWt="144." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="972.624" peakThrust="1710." throatDia="0." exitDia="0." Itot="319.993"
burn-time="0.33" massFrac="43.5" Isp="226.6" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Greg Gardner - 09/15/06</comments>
<data>
<eng-data t="0." f="0." m="144." cg="101.5"/>
<eng-data t="0.003" f="204." m="143.862" cg="101.5"/>
<eng-data t="0.006" f="757." m="143.214" cg="101.5"/>
<eng-data t="0.009" f="1357." m="141.787" cg="101.5"/>
<eng-data t="0.012" f="1710." m="139.716" cg="101.5"/>
<eng-data t="0.016" f="1345." m="136.967" cg="101.5"/>
<eng-data t="0.019" f="995." m="135.387" cg="101.5"/>
<eng-data t="0.022" f="710." m="134.236" cg="101.5"/>
<eng-data t="0.025" f="606." m="133.348" cg="101.5"/>
<eng-data t="0.028" f="905." m="132.328" cg="101.5"/>
<eng-data t="0.031" f="1165." m="130.931" cg="101.5"/>
<eng-data t="0.0325" f="1311." m="130.095" cg="101.5"/>
<eng-data t="0.034" f="1258." m="129.228" cg="101.5"/>
<eng-data t="0.037" f="1098." m="127.638" cg="101.5"/>
<eng-data t="0.04" f="1072." m="126.173" cg="101.5"/>
<eng-data t="0.043" f="969." m="124.795" cg="101.5"/>
<eng-data t="0.047" f="1072." m="122.958" cg="101.5"/>
<eng-data t="0.0485" f="1166." m="122.203" cg="101.5"/>
<eng-data t="0.05" f="1098." m="121.439" cg="101.5"/>
<eng-data t="0.053" f="1160." m="119.915" cg="101.5"/>
<eng-data t="0.056" f="1117." m="118.378" cg="101.5"/>
<eng-data t="0.059" f="1103." m="116.879" cg="101.5"/>
<eng-data t="0.062" f="1093." m="115.397" cg="101.5"/>
<eng-data t="0.069" f="1076." m="111.981" cg="101.5"/>
<eng-data t="0.075" f="1110." m="109.029" cg="101.5"/>
<eng-data t="0.082" f="1105." m="105.541" cg="101.5"/>
<eng-data t="0.088" f="1065." m="102.611" cg="101.5"/>
<eng-data t="0.093" f="1082." m="100.196" cg="101.5"/>
<eng-data t="0.1" f="1092." m="96.7716" cg="101.5"/>
<eng-data t="0.2" f="1022." m="49.2056" cg="101.5"/>
<eng-data t="0.25" f="931." m="27.2339" cg="101.5"/>
<eng-data t="0.3" f="853." m="7.16348" cg="101.5"/>
<eng-data t="0.306" f="850." m="4.86438" cg="101.5"/>
<eng-data t="0.309" f="838." m="3.72495" cg="101.5"/>
<eng-data t="0.312" f="735." m="2.66316" cg="101.5"/>
<eng-data t="0.318" f="435." m="1.08362" cg="101.5"/>
<eng-data t="0.325" f="161." m="0.144903" cg="101.5"/>
<eng-data t="0.329" f="0." m="0." cg="101.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="H115DM" Type="single-use" dia="29." len="203."
initWt="205." propWt="113." delays="14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="104.972" peakThrust="130.742" throatDia="0." exitDia="0."
Itot="177.718" burn-time="1.69" massFrac="55.12" Isp="160.37" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>AT H115 Dark Matter DMS</comments>
<data>
<eng-data t="0." f="0." m="113." cg="101.5"/>
<eng-data t="0.014" f="89.265" m="112.603" cg="101.5"/>
<eng-data t="0.024" f="130.742" m="111.903" cg="101.5"/>
<eng-data t="0.036" f="108.2" m="110.992" cg="101.5"/>
<eng-data t="0.048" f="101.588" m="110.191" cg="101.5"/>
<eng-data t="0.081" f="111.206" m="107.959" cg="101.5"/>
<eng-data t="0.202" f="121.124" m="99.0215" cg="101.5"/>
<eng-data t="0.405" f="123.228" m="83.2516" cg="101.5"/>
<eng-data t="0.598" f="123.829" m="68.0926" cg="101.5"/>
<eng-data t="0.8" f="123.528" m="52.2074" cg="101.5"/>
<eng-data t="1.002" f="122.326" m="36.4188" cg="101.5"/>
<eng-data t="1.2" f="114.211" m="21.5293" cg="101.5"/>
<eng-data t="1.269" f="111.807" m="16.5712" cg="101.5"/>
<eng-data t="1.293" f="111.506" m="14.8674" cg="101.5"/>
<eng-data t="1.35" f="119.32" m="10.6845" cg="101.5"/>
<eng-data t="1.367" f="117.818" m="9.40282" cg="101.5"/>
<eng-data t="1.393" f="111.807" m="7.50477" cg="101.5"/>
<eng-data t="1.429" f="88.964" m="5.20693" cg="101.5"/>
<eng-data t="1.467" f="67.024" m="3.32245" cg="101.5"/>
<eng-data t="1.524" f="44.182" m="1.30724" cg="101.5"/>
<eng-data t="1.562" f="22.842" m="0.49753" cg="101.5"/>
<eng-data t="1.583" f="13.224" m="0.256743" cg="101.5"/>
<eng-data t="1.6" f="6.913" m="0.14791" cg="101.5"/>
<eng-data t="1.626" f="3.306" m="0.0634407" cg="101.5"/>
<eng-data t="1.662" f="1.202" m="0.0118463" cg="101.5"/>
<eng-data t="1.693" f="0." m="0." cg="101.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="H169WS" Type="single-use" dia="29." len="221."
initWt="202." propWt="112." delays="13" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="153.306" peakThrust="233.462" throatDia="0." exitDia="0."
Itot="234.558" burn-time="1.53" massFrac="55.45" Isp="213.56" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="112." cg="110.5"/>
<eng-data t="0.021" f="3.91694" m="111.98" cg="110.5"/>
<eng-data t="0.034" f="138.475" m="111.538" cg="110.5"/>
<eng-data t="0.053" f="216.791" m="109.927" cg="110.5"/>
<eng-data t="0.08" f="231.308" m="107.038" cg="110.5"/>
<eng-data t="0.22" f="233.462" m="91.5036" cg="110.5"/>
<eng-data t="0.299" f="228.854" m="82.7839" cg="110.5"/>
<eng-data t="0.489" f="221.639" m="62.3487" cg="110.5"/>
<eng-data t="0.653" f="214." m="45.2915" cg="110.5"/>
<eng-data t="0.819" f="178.58" m="29.7328" cg="110.5"/>
<eng-data t="0.945" f="147.99" m="19.9089" cg="110.5"/>
<eng-data t="1.132" f="115.306" m="8.15393" cg="110.5"/>
<eng-data t="1.286" f="55.1945" m="1.88515" cg="110.5"/>
<eng-data t="1.35" f="30.5" m="0.575757" cg="110.5"/>
<eng-data t="1.366" f="12.3644" m="0.412018" cg="110.5"/>
<eng-data t="1.444" f="4.64227" m="0.095316" cg="110.5"/>
<eng-data t="1.53" f="0." m="0." cg="110.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="H178DM" Type="reloadable" dia="38." len="191."
initWt="324." propWt="177." delays="14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="164.647" peakThrust="215.719" throatDia="0." exitDia="0."
Itot="285.662" burn-time="1.74" massFrac="54.63" Isp="164.57" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>H178-14 Dark Matter</comments>
<data>
<eng-data t="0." f="0." m="177." cg="95.5"/>
<eng-data t="0.016" f="132.659" m="176.342" cg="95.5"/>
<eng-data t="0.099" f="165.726" m="168.67" cg="95.5"/>
<eng-data t="0.146" f="162.97" m="163.884" cg="95.5"/>
<eng-data t="0.201" f="163.364" m="158.323" cg="95.5"/>
<eng-data t="0.256" f="164.938" m="152.729" cg="95.5"/>
<eng-data t="0.301" f="168.481" m="148.081" cg="95.5"/>
<eng-data t="0.358" f="173.205" m="142.047" cg="95.5"/>
<eng-data t="0.401" f="176.354" m="137.39" cg="95.5"/>
<eng-data t="0.457" f="177.929" m="131.244" cg="95.5"/>
<eng-data t="0.498" f="183.046" m="126.659" cg="95.5"/>
<eng-data t="0.6" f="198.792" m="114.592" cg="95.5"/>
<eng-data t="0.635" f="204.303" m="110.221" cg="95.5"/>
<eng-data t="0.703" f="204.303" m="101.613" cg="95.5"/>
<eng-data t="0.799" f="215.719" m="89.1214" cg="95.5"/>
<eng-data t="0.901" f="210.602" m="75.6495" cg="95.5"/>
<eng-data t="0.999" f="211.783" m="62.8254" cg="95.5"/>
<eng-data t="1.049" f="205.09" m="56.3679" cg="95.5"/>
<eng-data t="1.098" f="206.271" m="50.1232" cg="95.5"/>
<eng-data t="1.202" f="196.824" m="37.1356" cg="95.5"/>
<eng-data t="1.297" f="178.322" m="26.0944" cg="95.5"/>
<eng-data t="1.351" f="172.811" m="20.2201" cg="95.5"/>
<eng-data t="1.404" f="178.322" m="14.4546" cg="95.5"/>
<eng-data t="1.434" f="186.195" m="11.0667" cg="95.5"/>
<eng-data t="1.499" f="125.574" m="4.78843" cg="95.5"/>
<eng-data t="1.539" f="71.25" m="2.34933" cg="95.5"/>
<eng-data t="1.566" f="44.876" m="1.37796" cg="95.5"/>
<eng-data t="1.582" f="31.492" m="0.99941" cg="95.5"/>
<eng-data t="1.601" f="27.949" m="0.64952" cg="95.5"/>
<eng-data t="1.606" f="16.533" m="0.580616" cg="95.5"/>
<eng-data t="1.617" f="18.895" m="0.459882" cg="95.5"/>
<eng-data t="1.644" f="8.66" m="0.22939" cg="95.5"/>
<eng-data t="1.684" f="4.33" m="0.0684147" cg="95.5"/>
<eng-data t="1.735" f="0." m="0." cg="95.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="H195NT" Type="single-use" dia="29." len="203.2"
initWt="197." propWt="115." delays="10" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="202.617" peakThrust="256.571" throatDia="0." exitDia="0."
Itot="236.859" burn-time="1.17" massFrac="58.38" Isp="210.03" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="115." cg="101.6"/>
<eng-data t="0.003" f="178.052" m="114.87" cg="101.6"/>
<eng-data t="0.005" f="224.131" m="114.675" cg="101.6"/>
<eng-data t="0.013" f="252.516" m="113.749" cg="101.6"/>
<eng-data t="0.019" f="256.571" m="113.008" cg="101.6"/>
<eng-data t="0.022" f="248.461" m="112.64" cg="101.6"/>
<eng-data t="0.058" f="239.614" m="108.375" cg="101.6"/>
<eng-data t="0.1" f="240.351" m="103.481" cg="101.6"/>
<eng-data t="0.199" f="235.559" m="92.0432" cg="101.6"/>
<eng-data t="0.255" f="228.555" m="85.7338" cg="101.6"/>
<eng-data t="0.285" f="227.449" m="82.4128" cg="101.6"/>
<eng-data t="0.301" f="230.767" m="80.633" cg="101.6"/>
<eng-data t="0.399" f="223.025" m="69.8371" cg="101.6"/>
<eng-data t="0.5" f="223.025" m="58.9004" cg="101.6"/>
<eng-data t="0.603" f="220.445" m="47.8118" cg="101.6"/>
<eng-data t="0.774" f="217.127" m="29.6473" cg="101.6"/>
<eng-data t="0.802" f="211.598" m="26.7331" cg="101.6"/>
<eng-data t="0.899" f="201.644" m="17.0022" cg="101.6"/>
<eng-data t="0.961" f="180.632" m="11.2485" cg="101.6"/>
<eng-data t="0.999" f="169.942" m="8.0145" cg="101.6"/>
<eng-data t="1.023" f="161.094" m="6.0858" cg="101.6"/>
<eng-data t="1.054" f="155.196" m="3.70554" cg="101.6"/>
<eng-data t="1.101" f="69.304" m="1.14405" cg="101.6"/>
<eng-data t="1.169" f="0." m="0." cg="101.6"/>
</data>
</engine>
<engine mfg="Aerotech" code="H550ST" Type="single-use" dia="38." len="206."
initWt="316." propWt="176." delays="14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="541.252" peakThrust="643.372" throatDia="0." exitDia="0."
Itot="313.385" burn-time="0.58" massFrac="55.7" Isp="181.57" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>AT H550 ST DMS</comments>
<data>
<eng-data t="0." f="0." m="176." cg="103."/>
<eng-data t="0.008" f="445.411" m="174.999" cg="103."/>
<eng-data t="0.009" f="533.786" m="174.724" cg="103."/>
<eng-data t="0.01" f="565.601" m="174.416" cg="103."/>
<eng-data t="0.013" f="586.812" m="173.445" cg="103."/>
<eng-data t="0.015" f="623.34" m="172.765" cg="103."/>
<eng-data t="0.021" f="639.837" m="170.637" cg="103."/>
<eng-data t="0.036" f="606.843" m="165.386" cg="103."/>
<eng-data t="0.045" f="629.232" m="162.262" cg="103."/>
<eng-data t="0.057" f="615.092" m="158.069" cg="103."/>
<eng-data t="0.061" f="635.123" m="156.665" cg="103."/>
<eng-data t="0.067" f="619.805" m="154.551" cg="103."/>
<eng-data t="0.101" f="637.48" m="142.547" cg="103."/>
<eng-data t="0.116" f="622.162" m="137.241" cg="103."/>
<eng-data t="0.157" f="643.372" m="122.671" cg="103."/>
<eng-data t="0.174" f="623.34" m="116.624" cg="103."/>
<eng-data t="0.196" f="623.34" m="108.923" cg="103."/>
<eng-data t="0.205" f="639.837" m="105.73" cg="103."/>
<eng-data t="0.231" f="631.588" m="96.4476" cg="103."/>
<eng-data t="0.234" f="618.627" m="95.3944" cg="103."/>
<eng-data t="0.255" f="611.557" m="88.1401" cg="103."/>
<eng-data t="0.268" f="628.053" m="83.615" cg="103."/>
<eng-data t="0.314" f="595.06" m="67.816" cg="103."/>
<eng-data t="0.334" f="600.952" m="61.0991" cg="103."/>
<eng-data t="0.362" f="571.493" m="51.8807" cg="103."/>
<eng-data t="0.386" f="565.601" m="44.2175" cg="103."/>
<eng-data t="0.401" f="556.175" m="39.4925" cg="103."/>
<eng-data t="0.426" f="518.468" m="31.9484" cg="103."/>
<eng-data t="0.445" f="503.15" m="26.4977" cg="103."/>
<eng-data t="0.493" f="447.768" m="13.6807" cg="103."/>
<eng-data t="0.505" f="447.768" m="10.663" cg="103."/>
<eng-data t="0.511" f="456.016" m="9.14029" cg="103."/>
<eng-data t="0.519" f="451.303" m="7.10206" cg="103."/>
<eng-data t="0.535" f="357.036" m="3.47029" cg="103."/>
<eng-data t="0.545" f="266.304" m="1.71993" cg="103."/>
<eng-data t="0.551" f="179.107" m="0.969485" cg="103."/>
<eng-data t="0.559" f="91.91" m="0.360662" cg="103."/>
<eng-data t="0.565" f="42.42" m="0.134339" cg="103."/>
<eng-data t="0.572" f="12.962" m="0.0254785" cg="103."/>
<eng-data t="0.579" f="0." m="0." cg="103."/>
</data>
</engine>
<engine mfg="Aerotech" code="I65W" Type="single-use" dia="54." len="218." initWt="752."
propWt="377." delays="10" auto-calc-mass="1" auto-calc-cg="1" avgThrust="77.709"
peakThrust="196.341" throatDia="0." exitDia="0." Itot="660.214" burn-time="8.5"
massFrac="50.13" Isp="178.58" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<comments>From AT DMS announcement May 2014.</comments>
<data>
<eng-data t="0." f="0." m="377." cg="109."/>
<eng-data t="0.023" f="148.274" m="376.026" cg="109."/>
<eng-data t="0.211" f="196.341" m="357.529" cg="109."/>
<eng-data t="0.398" f="167.827" m="338.085" cg="109."/>
<eng-data t="0.797" f="149.903" m="301.889" cg="109."/>
<eng-data t="1.395" f="135.239" m="253.205" cg="109."/>
<eng-data t="2.238" f="122.204" m="191.242" cg="109."/>
<eng-data t="3.199" f="99.392" m="130.441" cg="109."/>
<eng-data t="4.711" f="69.249" m="57.6389" cg="109."/>
<eng-data t="5.367" f="48.882" m="35.5133" cg="109."/>
<eng-data t="6.246" f="29.329" m="15.885" cg="109."/>
<eng-data t="6.926" f="15.479" m="7.18554" cg="109."/>
<eng-data t="7.395" f="11.406" m="3.58548" cg="109."/>
<eng-data t="8.496" f="0." m="0." cg="109."/>
</data>
</engine>
<engine mfg="Aerotech" code="I65W" Type="single-use" dia="54." len="235." initWt="776.1"
propWt="369.7" delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="76.332" peakThrust="150.07" throatDia="0." exitDia="0." Itot="630.5"
burn-time="8.26" massFrac="47.64" Isp="173.91" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>AEROTECH I65 RASP.ENG file made from NAR published data
File produced OCT 3, 2002
The total impulse, peak thrust, average thrust and burn time are
the same as the averaged static test data on the NAR web site in
the certification file. The curve drawn with these data points is as
close to the certification curve as can be with such a limited
number of points (32) allowed with wRASP up to v1.6.
</comments>
<data>
<eng-data t="0." f="0." m="369.7" cg="117.5"/>
<eng-data t="0.086" f="55.739" m="368.295" cg="117.5"/>
<eng-data t="0.099" f="90.267" m="367.738" cg="117.5"/>
<eng-data t="0.148" f="113.911" m="364.805" cg="117.5"/>
<eng-data t="0.296" f="113.911" m="354.92" cg="117.5"/>
<eng-data t="0.542" f="121.767" m="337.922" cg="117.5"/>
<eng-data t="0.579" f="123.588" m="335.26" cg="117.5"/>
<eng-data t="0.825" f="128.953" m="317.047" cg="117.5"/>
<eng-data t="0.973" f="132.593" m="305.698" cg="117.5"/>
<eng-data t="1.022" f="138.725" m="301.8" cg="117.5"/>
<eng-data t="1.071" f="132.593" m="297.903" cg="117.5"/>
<eng-data t="1.33" f="138.629" m="277.308" cg="117.5"/>
<eng-data t="1.502" f="139.875" m="263.264" cg="117.5"/>
<eng-data t="1.724" f="150.07" m="244.392" cg="117.5"/>
<eng-data t="2.019" f="141.886" m="219.142" cg="117.5"/>
<eng-data t="2.733" f="131.923" m="161.825" cg="117.5"/>
<eng-data t="3.14" f="119.181" m="131.862" cg="117.5"/>
<eng-data t="3.213" f="122.151" m="126.697" cg="117.5"/>
<eng-data t="3.275" f="114.295" m="122.399" cg="117.5"/>
<eng-data t="3.57" f="103.948" m="103.524" cg="117.5"/>
<eng-data t="3.977" f="88.791" m="80.5253" cg="117.5"/>
<eng-data t="4.051" f="93.036" m="76.5805" cg="117.5"/>
<eng-data t="4.1" f="84.547" m="74.0294" cg="117.5"/>
<eng-data t="4.432" f="74.229" m="58.5748" cg="117.5"/>
<eng-data t="4.912" f="58.44" m="39.9048" cg="117.5"/>
<eng-data t="5.725" f="34.758" m="17.6906" cg="117.5"/>
<eng-data t="6.119" f="24.43" m="10.8536" cg="117.5"/>
<eng-data t="6.611" f="13.489" m="5.38396" cg="117.5"/>
<eng-data t="7.166" f="6.787" m="2.08475" cg="117.5"/>
<eng-data t="7.596" f="3.729" m="0.75903" cg="117.5"/>
<eng-data t="7.978" f="1.886" m="0.13018" cg="117.5"/>
<eng-data t="8.114" f="0.665" m="0.0284648" cg="117.5"/>
<eng-data t="8.26" f="0." m="0." cg="117.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="I115W" Type="reloadable" dia="54." len="156." initWt="580."
propWt="229." delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="116.329" peakThrust="166.909" throatDia="0." exitDia="0."
Itot="408.779" burn-time="3.51" massFrac="39.48" Isp="182.03" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Aerotech I115W from TRA Cert Data</comments>
<data>
<eng-data t="0." f="0." m="229." cg="78."/>
<eng-data t="0.034" f="12.095" m="228.885" cg="78."/>
<eng-data t="0.177" f="105.225" m="224.186" cg="78."/>
<eng-data t="0.206" f="113.087" m="222.412" cg="78."/>
<eng-data t="1.017" f="163.281" m="159.632" cg="78."/>
<eng-data t="1.166" f="161.466" m="146.078" cg="78."/>
<eng-data t="1.257" f="162.676" m="137.816" cg="78."/>
<eng-data t="1.343" f="166.909" m="129.877" cg="78."/>
<eng-data t="1.417" f="160.862" m="123.083" cg="78."/>
<eng-data t="1.514" f="162.676" m="114.292" cg="78."/>
<eng-data t="1.617" f="163.885" m="104.871" cg="78."/>
<eng-data t="1.686" f="160.257" m="98.6063" cg="78."/>
<eng-data t="1.977" f="142.719" m="73.9108" cg="78."/>
<eng-data t="2.497" f="106.435" m="37.6208" cg="78."/>
<eng-data t="2.68" f="91.316" m="27.4843" cg="78."/>
<eng-data t="2.994" f="72.569" m="13.0703" cg="78."/>
<eng-data t="3.103" f="67.126" m="8.80523" cg="78."/>
<eng-data t="3.189" f="65.917" m="5.60038" cg="78."/>
<eng-data t="3.24" f="59.265" m="3.81213" cg="78."/>
<eng-data t="3.291" f="42.937" m="2.35215" cg="78."/>
<eng-data t="3.331" f="30.237" m="1.53231" cg="78."/>
<eng-data t="3.377" f="20.561" m="0.877789" cg="78."/>
<eng-data t="3.429" f="12.7" m="0.393332" cg="78."/>
<eng-data t="3.491" f="7.257" m="0.0467521" cg="78."/>
<eng-data t="3.514" f="0." m="0." cg="78."/>
</data>
</engine>
<engine mfg="Aerotech" code="I140W" Type="single-use" dia="38." len="202.7"
initWt="356." propWt="183." delays="14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="136.91" peakThrust="179.023" throatDia="0." exitDia="0."
Itot="339.263" burn-time="2.48" massFrac="51.4" Isp="189.04" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>AT I140W DMS</comments>
<data>
<eng-data t="0." f="0." m="183." cg="101.35"/>
<eng-data t="0.011" f="96.257" m="182.714" cg="101.35"/>
<eng-data t="0.024" f="80.214" m="182.096" cg="101.35"/>
<eng-data t="0.049" f="160.428" m="180.473" cg="101.35"/>
<eng-data t="0.062" f="144.02" m="179.406" cg="101.35"/>
<eng-data t="0.114" f="160.428" m="175.136" cg="101.35"/>
<eng-data t="0.159" f="164.074" m="171.198" cg="101.35"/>
<eng-data t="0.238" f="174.647" m="163.981" cg="101.35"/>
<eng-data t="0.314" f="173.918" m="156.836" cg="101.35"/>
<eng-data t="0.419" f="179.023" m="146.841" cg="101.35"/>
<eng-data t="0.627" f="178.293" m="126.796" cg="101.35"/>
<eng-data t="0.835" f="176.835" m="106.874" cg="101.35"/>
<eng-data t="0.943" f="177.2" m="96.5622" cg="101.35"/>
<eng-data t="1.146" f="164.803" m="77.8377" cg="101.35"/>
<eng-data t="1.349" f="148.76" m="60.6702" cg="101.35"/>
<eng-data t="1.459" f="141.103" m="52.0708" cg="101.35"/>
<eng-data t="1.562" f="131.259" m="44.5048" cg="101.35"/>
<eng-data t="1.773" f="113.393" m="30.5823" cg="101.35"/>
<eng-data t="2.192" f="83.86" m="8.29168" cg="101.35"/>
<eng-data t="2.295" f="67.088" m="4.09844" cg="101.35"/>
<eng-data t="2.395" f="37.555" m="1.2762" cg="101.35"/>
<eng-data t="2.435" f="31.356" m="0.532779" cg="101.35"/>
<eng-data t="2.47" f="20.418" m="0.0440542" cg="101.35"/>
<eng-data t="2.478" f="0." m="0." cg="101.35"/>
</data>
</engine>
<engine mfg="Aerotech" code="I154J" Type="reloadable" dia="38." len="250."
initWt="506.3" propWt="280." delays="6,10" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="107.035" peakThrust="199.49" throatDia="0." exitDia="0."
Itot="385.327" burn-time="3.6" massFrac="55.3" Isp="140.33" tDiv="10" tStep="-1."
tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="280." cg="125."/>
<eng-data t="0." f="199.49" m="280." cg="125."/>
<eng-data t="0.1" f="162.84" m="266.836" cg="125."/>
<eng-data t="0.3" f="153.9" m="243.819" cg="125."/>
<eng-data t="0.4" f="149.32" m="232.803" cg="125."/>
<eng-data t="0.6" f="149.32" m="211.102" cg="125."/>
<eng-data t="1." f="126.72" m="170.985" cg="125."/>
<eng-data t="1.6" f="117.65" m="117.713" cg="125."/>
<eng-data t="1.7" f="113.11" m="109.329" cg="125."/>
<eng-data t="2.1" f="113.11" m="76.4518" cg="125."/>
<eng-data t="2.6" f="95.05" m="38.6366" cg="125."/>
<eng-data t="3.1" f="67.88" m="9.03814" cg="125."/>
<eng-data t="3.3" f="22.6" m="2.46336" cg="125."/>
<eng-data t="3.6" f="0." m="0." cg="125."/>
</data>
</engine>
<engine mfg="Aerotech" code="I161W" Type="reloadable" dia="38." len="202."
initWt="384.8" propWt="187.5" delays="6,10,14" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="145.006" peakThrust="224.89" throatDia="0."
exitDia="0." Itot="333.514" burn-time="2.3" massFrac="48.73" Isp="181.38"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="187.5" cg="101."/>
<eng-data t="0." f="0.09" m="187.5" cg="101."/>
<eng-data t="0.1" f="224.89" m="181.176" cg="101."/>
<eng-data t="0.2" f="206.88" m="169.039" cg="101."/>
<eng-data t="0.5" f="202.43" m="134.522" cg="101."/>
<eng-data t="0.7" f="184.41" m="112.774" cg="101."/>
<eng-data t="1." f="179.92" m="82.0506" cg="101."/>
<eng-data t="1.3" f="166.4" m="52.8457" cg="101."/>
<eng-data t="1.6" f="134.91" m="27.4365" cg="101."/>
<eng-data t="1.8" f="112.44" m="13.5306" cg="101."/>
<eng-data t="2." f="62.98" m="3.6686" cg="101."/>
<eng-data t="2.1" f="22.51" m="1.2655" cg="101."/>
<eng-data t="2.3" f="0." m="0." cg="101."/>
</data>
</engine>
<engine mfg="Aerotech" code="I170G" Type="reloadable" dia="54." len="151." initWt="528."
propWt="227." delays="10" auto-calc-mass="1" auto-calc-cg="1" avgThrust="169.003"
peakThrust="207.3" throatDia="0." exitDia="0." Itot="405.608" burn-time="2.4"
massFrac="42.99" Isp="182.2" tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1."
FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Aerotech I170G from TRA Cert Data
Created by Mark Hairfield 12-29-10
</comments>
<data>
<eng-data t="0." f="0." m="227." cg="75.5"/>
<eng-data t="0.06" f="89." m="225.506" cg="75.5"/>
<eng-data t="0.16" f="169." m="218.286" cg="75.5"/>
<eng-data t="0.25" f="184.6" m="209.381" cg="75.5"/>
<eng-data t="0.5" f="202.4" m="182.308" cg="75.5"/>
<eng-data t="0.75" f="207.3" m="153.646" cg="75.5"/>
<eng-data t="1." f="202.4" m="124.985" cg="75.5"/>
<eng-data t="1.5" f="177.9" m="71.7759" cg="75.5"/>
<eng-data t="2.18" f="137.9" m="11.6847" cg="75.5"/>
<eng-data t="2.25" f="139.7" m="6.24714" cg="75.5"/>
<eng-data t="2.3" f="131.2" m="2.45688" cg="75.5"/>
<eng-data t="2.35" f="22.2" m="0.310608" cg="75.5"/>
<eng-data t="2.4" f="0." m="0." cg="75.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="I180W" Type="reloadable" dia="38." len="191." initWt="385."
propWt="180." delays="14" auto-calc-mass="1" auto-calc-cg="1" avgThrust="166.818"
peakThrust="361.192" throatDia="0." exitDia="0." Itot="326.296" burn-time="1.96"
massFrac="46.75" Isp="184.85" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<comments>38/360 Non hazmat I161W equivalalent</comments>
<data>
<eng-data t="0." f="0." m="180." cg="95.5"/>
<eng-data t="0.027" f="133.693" m="179.004" cg="95.5"/>
<eng-data t="0.029" f="224.545" m="178.807" cg="95.5"/>
<eng-data t="0.033" f="328.692" m="178.196" cg="95.5"/>
<eng-data t="0.042" f="338.295" m="176.541" cg="95.5"/>
<eng-data t="0.061" f="327.215" m="173.053" cg="95.5"/>
<eng-data t="0.082" f="337.556" m="169.202" cg="95.5"/>
<eng-data t="0.088" f="347.158" m="168.069" cg="95.5"/>
<eng-data t="0.117" f="361.192" m="162.403" cg="95.5"/>
<eng-data t="0.203" f="360.454" m="145.285" cg="95.5"/>
<eng-data t="0.243" f="350.851" m="137.437" cg="95.5"/>
<eng-data t="0.289" f="350.851" m="128.534" cg="95.5"/>
<eng-data t="0.358" f="313.181" m="115.897" cg="95.5"/>
<eng-data t="0.368" f="303.579" m="114.196" cg="95.5"/>
<eng-data t="0.387" f="312.442" m="110.967" cg="95.5"/>
<eng-data t="0.446" f="278.465" m="101.351" cg="95.5"/>
<eng-data t="0.502" f="259.999" m="93.0339" cg="95.5"/>
<eng-data t="0.634" f="223.068" m="75.4461" cg="95.5"/>
<eng-data t="0.762" f="195.738" m="60.66" cg="95.5"/>
<eng-data t="0.998" f="151.42" m="38.0621" cg="95.5"/>
<eng-data t="1.5" f="68.693" m="7.58454" cg="95.5"/>
<eng-data t="1.736" f="26.591" m="1.38211" cg="95.5"/>
<eng-data t="1.845" f="9.602" m="0.293978" cg="95.5"/>
<eng-data t="1.956" f="0." m="0." cg="95.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="I195J" Type="reloadable" dia="38." len="297."
initWt="582.4" propWt="312.5" delays="6,10,14" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="160.848" peakThrust="244.78" throatDia="0."
exitDia="0." Itot="455.2" burn-time="2.83" massFrac="53.66" Isp="148.54"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="312.5" cg="148.5"/>
<eng-data t="0." f="244.78" m="312.5" cg="148.5"/>
<eng-data t="0.1" f="236.61" m="295.976" cg="148.5"/>
<eng-data t="0.2" f="216.19" m="280.433" cg="148.5"/>
<eng-data t="0.3" f="212.11" m="265.732" cg="148.5"/>
<eng-data t="1.4" f="212.11" m="105.554" cg="148.5"/>
<eng-data t="1.5" f="203.94" m="91.2728" cg="148.5"/>
<eng-data t="1.6" f="188.46" m="77.8035" cg="148.5"/>
<eng-data t="1.7" f="179.49" m="65.1734" cg="148.5"/>
<eng-data t="1.8" f="156.65" m="53.6352" cg="148.5"/>
<eng-data t="1.9" f="142.78" m="43.357" cg="148.5"/>
<eng-data t="2." f="130.53" m="33.9755" cg="148.5"/>
<eng-data t="2.1" f="118.28" m="25.435" cg="148.5"/>
<eng-data t="2.2" f="106.08" m="17.7337" cg="148.5"/>
<eng-data t="2.3" f="89.74" m="11.012" cg="148.5"/>
<eng-data t="2.4" f="63.63" m="5.74751" cg="148.5"/>
<eng-data t="2.5" f="32.62" m="2.44367" cg="148.5"/>
<eng-data t="2.6" f="8.97" m="1.01607" cg="148.5"/>
<eng-data t="2.7" f="8.97" m="0.400271" cg="148.5"/>
<eng-data t="2.83" f="0." m="0." cg="148.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="I200W" Type="reloadable" dia="29." len="333."
initWt="357.504" propWt="181.888" delays="6,10,14" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="181.245" peakThrust="303.951" throatDia="0."
exitDia="0." Itot="326.785" burn-time="1.8" massFrac="50.88" Isp="183.2"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="181.888" cg="166.5"/>
<eng-data t="0.033" f="303.951" m="179.097" cg="166.5"/>
<eng-data t="0.103" f="273.452" m="167.848" cg="166.5"/>
<eng-data t="0.174" f="276.061" m="156.99" cg="166.5"/>
<eng-data t="0.245" f="271.625" m="146.168" cg="166.5"/>
<eng-data t="0.316" f="268.233" m="135.501" cg="166.5"/>
<eng-data t="0.386" f="258.449" m="125.241" cg="166.5"/>
<eng-data t="0.457" f="252.48" m="115.145" cg="166.5"/>
<eng-data t="0.528" f="246.642" m="105.283" cg="166.5"/>
<eng-data t="0.599" f="242.304" m="95.6219" cg="166.5"/>
<eng-data t="0.67" f="237.737" m="86.1366" cg="166.5"/>
<eng-data t="0.741" f="234.769" m="76.8003" cg="166.5"/>
<eng-data t="0.811" f="233.171" m="67.6843" cg="166.5"/>
<eng-data t="0.882" f="230.66" m="58.5194" cg="166.5"/>
<eng-data t="0.953" f="224.985" m="49.5162" cg="166.5"/>
<eng-data t="1.024" f="221.658" m="40.6909" cg="166.5"/>
<eng-data t="1.095" f="214.548" m="32.0718" cg="166.5"/>
<eng-data t="1.166" f="177.365" m="24.3279" cg="166.5"/>
<eng-data t="1.236" f="154.208" m="17.8685" cg="166.5"/>
<eng-data t="1.307" f="119.146" m="12.4672" cg="166.5"/>
<eng-data t="1.378" f="91.586" m="8.30333" cg="166.5"/>
<eng-data t="1.449" f="65.33" m="5.20279" cg="166.5"/>
<eng-data t="1.52" f="32.877" m="3.26229" cg="166.5"/>
<eng-data t="1.591" f="28.702" m="2.04553" cg="166.5"/>
<eng-data t="1.661" f="22.211" m="1.0537" cg="166.5"/>
<eng-data t="1.732" f="15.558" m="0.307414" cg="166.5"/>
<eng-data t="1.803" f="0." m="0." cg="166.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="I205W" Type="single-use" dia="29." len="304.8"
initWt="315." propWt="188." delays="14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="183.103" peakThrust="377.299" throatDia="0." exitDia="0."
Itot="346.431" burn-time="1.89" massFrac="59.68" Isp="187.9" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>From AT DMS announcement May 2014.</comments>
<data>
<eng-data t="0." f="0." m="188." cg="152.4"/>
<eng-data t="0.008" f="377.299" m="187.181" cg="152.4"/>
<eng-data t="0.028" f="241.932" m="183.821" cg="152.4"/>
<eng-data t="0.36" f="256.333" m="138.935" cg="152.4"/>
<eng-data t="0.711" f="246.252" m="91.0686" cg="152.4"/>
<eng-data t="0.861" f="233.292" m="71.5508" cg="152.4"/>
<eng-data t="1.121" f="230.411" m="38.8375" cg="152.4"/>
<eng-data t="1.146" f="214.571" m="35.819" cg="152.4"/>
<eng-data t="1.242" f="211.69" m="24.7155" cg="152.4"/>
<eng-data t="1.349" f="141.127" m="14.4721" cg="152.4"/>
<eng-data t="1.404" f="125.286" m="10.4963" cg="152.4"/>
<eng-data t="1.489" f="72.004" m="5.94604" cg="152.4"/>
<eng-data t="1.602" f="41.762" m="2.45783" cg="152.4"/>
<eng-data t="1.712" f="11.521" m="0.867484" cg="152.4"/>
<eng-data t="1.787" f="12.961" m="0.369266" cg="152.4"/>
<eng-data t="1.892" f="0." m="0." cg="152.4"/>
</data>
</engine>
<engine mfg="Aerotech" code="I211W" Type="reloadable" dia="38." len="250."
initWt="476.3" propWt="250." delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="200.21" peakThrust="386." throatDia="0." exitDia="0." Itot="440.462"
burn-time="2.2" massFrac="52.49" Isp="179.66" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="250." cg="125."/>
<eng-data t="0." f="386." m="250." cg="125."/>
<eng-data t="0.1" f="289.39" m="230.833" cg="125."/>
<eng-data t="0.2" f="276.22" m="214.781" cg="125."/>
<eng-data t="0.3" f="276.22" m="199.103" cg="125."/>
<eng-data t="0.4" f="293.79" m="182.927" cg="125."/>
<eng-data t="0.5" f="271.86" m="166.874" cg="125."/>
<eng-data t="0.6" f="271.86" m="151.444" cg="125."/>
<eng-data t="1.3" f="206.08" m="56.4989" cg="125."/>
<eng-data t="1.8" f="131.57" m="8.58756" cg="125."/>
<eng-data t="1.9" f="52.62" m="3.36039" cg="125."/>
<eng-data t="2." f="21.93" m="1.24471" cg="125."/>
<eng-data t="2.2" f="0." m="0." cg="125."/>
</data>
</engine>
<engine mfg="Aerotech" code="I215R" Type="reloadable" dia="54." len="156." initWt="527."
propWt="208." delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="213.475" peakThrust="259.145" throatDia="0." exitDia="0."
Itot="396.85" burn-time="1.86" massFrac="39.47" Isp="194.56" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Aerotech I215R from TRA Cert Data</comments>
<data>
<eng-data t="0." f="0." m="208." cg="78."/>
<eng-data t="0.049" f="88.39" m="206.865" cg="78."/>
<eng-data t="0.089" f="154.683" m="204.317" cg="78."/>
<eng-data t="0.094" f="206.914" m="203.843" cg="78."/>
<eng-data t="0.178" f="245.083" m="193.893" cg="78."/>
<eng-data t="0.251" f="255.127" m="184.324" cg="78."/>
<eng-data t="0.325" f="259.145" m="174.351" cg="78."/>
<eng-data t="0.404" f="249.1" m="163.828" cg="78."/>
<eng-data t="0.582" f="257.136" m="140.214" cg="78."/>
<eng-data t="0.631" f="253.118" m="133.662" cg="78."/>
<eng-data t="0.7" f="253.118" m="124.508" cg="78."/>
<eng-data t="0.774" f="245.083" m="114.846" cg="78."/>
<eng-data t="1.001" f="239.056" m="86.0456" cg="78."/>
<eng-data t="1.509" f="192.852" m="28.5464" cg="78."/>
<eng-data t="1.681" f="178.79" m="11.7947" cg="78."/>
<eng-data t="1.716" f="180.799" m="8.49643" cg="78."/>
<eng-data t="1.746" f="190.843" m="5.57461" cg="78."/>
<eng-data t="1.775" f="178.79" m="2.76546" cg="78."/>
<eng-data t="1.8" f="90.399" m="1.00184" cg="78."/>
<eng-data t="1.82" f="34.151" m="0.34904" cg="78."/>
<eng-data t="1.859" f="0." m="0." cg="78."/>
</data>
</engine>
<engine mfg="Aerotech" code="I218R" Type="reloadable" dia="38." len="191." initWt="375."
propWt="192." delays="6,14,1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="211.934" peakThrust="284.37" throatDia="0." exitDia="0."
Itot="317.901" burn-time="1.5" massFrac="51.2" Isp="168.84" tDiv="10" tStep="-1."
tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="192." cg="95.5"/>
<eng-data t="0.03" f="136.08" m="190.767" cg="95.5"/>
<eng-data t="0.09" f="275.03" m="183.318" cg="95.5"/>
<eng-data t="0.15" f="281." m="173.244" cg="95.5"/>
<eng-data t="0.21" f="284.37" m="163." cg="95.5"/>
<eng-data t="0.27" f="284.04" m="152.701" cg="95.5"/>
<eng-data t="0.33" f="279.31" m="142.494" cg="95.5"/>
<eng-data t="0.39" f="277.79" m="132.4" cg="95.5"/>
<eng-data t="0.45" f="276.31" m="122.36" cg="95.5"/>
<eng-data t="0.51" f="269.38" m="112.473" cg="95.5"/>
<eng-data t="0.57" f="266.04" m="102.772" cg="95.5"/>
<eng-data t="0.63" f="261.91" m="93.2058" cg="95.5"/>
<eng-data t="0.69" f="256.37" m="83.8152" cg="95.5"/>
<eng-data t="0.75" f="250.57" m="74.63" cg="95.5"/>
<eng-data t="0.81" f="242.21" m="65.7014" cg="95.5"/>
<eng-data t="0.87" f="234.61" m="57.062" cg="95.5"/>
<eng-data t="0.93" f="225.49" m="48.7255" cg="95.5"/>
<eng-data t="0.99" f="216.17" m="40.7232" cg="95.5"/>
<eng-data t="1.05" f="205.41" m="33.0846" cg="95.5"/>
<eng-data t="1.11" f="193.24" m="25.8616" cg="95.5"/>
<eng-data t="1.17" f="177.21" m="19.1494" cg="95.5"/>
<eng-data t="1.23" f="161.3" m="13.016" cg="95.5"/>
<eng-data t="1.29" f="139.12" m="7.57277" cg="95.5"/>
<eng-data t="1.35" f="96.08" m="3.31122" cg="95.5"/>
<eng-data t="1.41" f="38.85" m="0.866443" cg="95.5"/>
<eng-data t="1.47" f="5.98" m="0.0541753" cg="95.5"/>
<eng-data t="1.5" f="0." m="0." cg="95.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="I229T" Type="reloadable" dia="54." len="156." initWt="520."
propWt="206." delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="239.122" peakThrust="273.66" throatDia="0." exitDia="0."
Itot="413.681" burn-time="1.73" massFrac="39.62" Isp="204.78" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="206." cg="78."/>
<eng-data t="0.01" f="44.73" m="205.889" cg="78."/>
<eng-data t="0.02" f="216.65" m="205.238" cg="78."/>
<eng-data t="0.19" f="244.72" m="185.709" cg="78."/>
<eng-data t="0.4" f="266.64" m="158.972" cg="78."/>
<eng-data t="0.49" f="266.64" m="147.022" cg="78."/>
<eng-data t="0.52" f="273.66" m="142.986" cg="78."/>
<eng-data t="0.59" f="271.9" m="133.478" cg="78."/>
<eng-data t="0.75" f="272.78" m="111.779" cg="78."/>
<eng-data t="0.84" f="268.4" m="99.652" cg="78."/>
<eng-data t="0.88" f="271.9" m="94.271" cg="78."/>
<eng-data t="0.97" f="262.26" m="82.3012" cg="78."/>
<eng-data t="1." f="265.76" m="78.3572" cg="78."/>
<eng-data t="1.07" f="255.24" m="69.2767" cg="78."/>
<eng-data t="1.21" f="249.1" m="51.6966" cg="78."/>
<eng-data t="1.51" f="219.28" m="16.7109" cg="78."/>
<eng-data t="1.6" f="230.68" m="6.6279" cg="78."/>
<eng-data t="1.63" f="191.21" m="3.47659" cg="78."/>
<eng-data t="1.64" f="132.44" m="2.67075" cg="78."/>
<eng-data t="1.66" f="86.83" m="1.57886" cg="78."/>
<eng-data t="1.7" f="44.73" m="0.268604" cg="78."/>
<eng-data t="1.71" f="21.05" m="0.104822" cg="78."/>
<eng-data t="1.73" f="0." m="0." cg="78."/>
</data>
</engine>
<engine mfg="Aerotech" code="I245G" Type="reloadable" dia="38." len="192.53"
initWt="365." propWt="181.3" delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="239.565" peakThrust="411.99" throatDia="0." exitDia="0."
Itot="350.544" burn-time="1.46" massFrac="49.67" Isp="197.16" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>From Aerotech pre-cert data.
Created 11/11/07 by Jim Yehle.</comments>
<data>
<eng-data t="0." f="0." m="181.3" cg="96.266"/>
<eng-data t="0.0244989" f="234.061" m="179.817" cg="96.266"/>
<eng-data t="0.0550162" f="257.888" m="175.935" cg="96.266"/>
<eng-data t="0.0868597" f="368.567" m="170.776" cg="96.266"/>
<eng-data t="0.106904" f="382.335" m="166.884" cg="96.266"/>
<eng-data t="0.13363" f="390.808" m="161.54" cg="96.266"/>
<eng-data t="0.200445" f="405.635" m="147.779" cg="96.266"/>
<eng-data t="0.262806" f="410.931" m="134.611" cg="96.266"/>
<eng-data t="0.302895" f="411.99" m="126.08" cg="96.266"/>
<eng-data t="0.363029" f="408.813" m="113.316" cg="96.266"/>
<eng-data t="0.401294" f="398.43" m="105.328" cg="96.266"/>
<eng-data t="0.501114" f="363.271" m="85.6662" cg="96.266"/>
<eng-data t="0.594655" f="320.907" m="69.1163" cg="96.266"/>
<eng-data t="0.68932" f="278.355" m="54.4461" cg="96.266"/>
<eng-data t="0.797327" f="212.879" m="40.7258" cg="96.266"/>
<eng-data t="0.893204" f="181.477" m="30.9483" cg="96.266"/>
<eng-data t="1.00647" f="154.187" m="21.1164" cg="96.266"/>
<eng-data t="1.09061" f="133.72" m="14.8518" cg="96.266"/>
<eng-data t="1.16036" f="120.737" m="10.2627" cg="96.266"/>
<eng-data t="1.1804" f="122.856" m="9.00003" cg="96.266"/>
<eng-data t="1.23625" f="106.43" m="5.68882" cg="96.266"/>
<eng-data t="1.30421" f="75.0467" m="2.49944" cg="96.266"/>
<eng-data t="1.3608" f="36.0094" m="0.874102" cg="96.266"/>
<eng-data t="1.40312" f="19.0638" m="0.271441" cg="96.266"/>
<eng-data t="1.43875" f="5.2955" m="0.0469685" cg="96.266"/>
<eng-data t="1.46325" f="0." m="0." cg="96.266"/>
</data>
</engine>
<engine mfg="Aerotech" code="I284W" Type="reloadable" dia="38." len="297."
initWt="567.8" propWt="312.5" delays="6,10,14" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="307.909" peakThrust="487.77" throatDia="0."
exitDia="0." Itot="554.236" burn-time="1.8" massFrac="55.04" Isp="180.85"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="312.5" cg="148.5"/>
<eng-data t="0." f="487.77" m="312.5" cg="148.5"/>
<eng-data t="0.1" f="408.77" m="287.225" cg="148.5"/>
<eng-data t="0.2" f="408.77" m="264.177" cg="148.5"/>
<eng-data t="0.4" f="430.74" m="216.842" cg="148.5"/>
<eng-data t="0.6" f="413.18" m="169.258" cg="148.5"/>
<eng-data t="1.1" f="307.67" m="67.6475" cg="148.5"/>
<eng-data t="1.3" f="250.51" m="36.1751" cg="148.5"/>
<eng-data t="1.5" f="193.35" m="11.1485" cg="148.5"/>
<eng-data t="1.6" f="79.08" m="3.46818" cg="148.5"/>
<eng-data t="1.7" f="21.97" m="0.619377" cg="148.5"/>
<eng-data t="1.8" f="0." m="0." cg="148.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="I285R" Type="reloadable" dia="38." len="250." initWt="498."
propWt="254." delays="10,14,1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="276.644" peakThrust="373.97" throatDia="0." exitDia="0."
Itot="414.966" burn-time="1.5" massFrac="51." Isp="166.59" tDiv="10" tStep="-1."
tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="254." cg="125."/>
<eng-data t="0.03" f="171.41" m="252.426" cg="125."/>
<eng-data t="0.09" f="325.57" m="243.3" cg="125."/>
<eng-data t="0.15" f="341.7" m="231.047" cg="125."/>
<eng-data t="0.21" f="358.92" m="218.182" cg="125."/>
<eng-data t="0.27" f="373.71" m="204.728" cg="125."/>
<eng-data t="0.33" f="373.97" m="190.999" cg="125."/>
<eng-data t="0.39" f="368.44" m="177.366" cg="125."/>
<eng-data t="0.45" f="367.5" m="163.852" cg="125."/>
<eng-data t="0.51" f="361.9" m="150.458" cg="125."/>
<eng-data t="0.57" f="351.93" m="137.35" cg="125."/>
<eng-data t="0.63" f="346.11" m="124.532" cg="125."/>
<eng-data t="0.69" f="340.99" m="111.915" cg="125."/>
<eng-data t="0.75" f="329.38" m="99.6047" cg="125."/>
<eng-data t="0.81" f="321.63" m="87.6502" cg="125."/>
<eng-data t="0.87" f="310.86" m="76.0358" cg="125."/>
<eng-data t="0.93" f="295.95" m="64.893" cg="125."/>
<eng-data t="0.99" f="283.7" m="54.2489" cg="125."/>
<eng-data t="1.05" f="269.65" m="44.0877" cg="125."/>
<eng-data t="1.11" f="253.42" m="34.4826" cg="125."/>
<eng-data t="1.17" f="240.22" m="25.4179" cg="125."/>
<eng-data t="1.23" f="224.12" m="16.8913" cg="125."/>
<eng-data t="1.29" f="204.12" m="9.02751" cg="125."/>
<eng-data t="1.35" f="118.73" m="3.09903" cg="125."/>
<eng-data t="1.41" f="23.48" m="0.487628" cg="125."/>
<eng-data t="1.47" f="2.05" m="0.018822" cg="125."/>
<eng-data t="1.5" f="0." m="0." cg="125."/>
</data>
</engine>
<engine mfg="Aerotech" code="I300T" Type="reloadable" dia="38." len="250."
initWt="440.5" propWt="221.6" delays="6,10,14" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="272.993" peakThrust="473.17" throatDia="0."
exitDia="0." Itot="436.789" burn-time="1.6" massFrac="50.31" Isp="200.99"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="221.6" cg="125."/>
<eng-data t="0." f="473.17" m="221.6" cg="125."/>
<eng-data t="0.1" f="395.68" m="199.56" cg="125."/>
<eng-data t="0.2" f="375.31" m="180.002" cg="125."/>
<eng-data t="0.3" f="367.14" m="161.169" cg="125."/>
<eng-data t="0.4" f="358.97" m="142.749" cg="125."/>
<eng-data t="0.5" f="346.72" m="124.848" cg="125."/>
<eng-data t="0.6" f="338.56" m="107.465" cg="125."/>
<eng-data t="0.7" f="318.19" m="90.8051" cg="125."/>
<eng-data t="0.8" f="305.94" m="74.9729" cg="125."/>
<eng-data t="0.9" f="295.35" m="59.72" cg="125."/>
<eng-data t="1.07" f="269.23" m="35.3732" cg="125."/>
<eng-data t="1.1" f="258.01" m="31.3609" cg="125."/>
<eng-data t="1.2" f="246.79" m="18.5556" cg="125."/>
<eng-data t="1.3" f="179.49" m="7.74224" cg="125."/>
<eng-data t="1.4" f="48.95" m="1.94742" cg="125."/>
<eng-data t="1.5" f="13.91" m="0.352854" cg="125."/>
<eng-data t="1.6" f="0." m="0." cg="125."/>
</data>
</engine>
<engine mfg="Aerotech" code="I350R" Type="single-use" dia="38." len="356." initWt="616."
propWt="348." delays="10" auto-calc-mass="1" auto-calc-cg="1" avgThrust="401.007"
peakThrust="486.027" throatDia="0." exitDia="0." Itot="643.616" burn-time="1.6"
massFrac="56.49" Isp="188.59" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<comments>Aerotech I350-10R single use motor file created using Aerotech instruction
sheet data and thrust tracer utility.
</comments>
<data>
<eng-data t="0." f="0." m="348." cg="178."/>
<eng-data t="0.004" f="2.809" m="347.997" cg="178."/>
<eng-data t="0.008" f="207.896" m="347.769" cg="178."/>
<eng-data t="0.031" f="272.512" m="344.782" cg="178."/>
<eng-data t="0.035" f="359.603" m="344.098" cg="178."/>
<eng-data t="0.046" f="407.363" m="341.818" cg="178."/>
<eng-data t="0.081" f="432.648" m="333.869" cg="178."/>
<eng-data t="0.104" f="435.457" m="328.471" cg="178."/>
<eng-data t="0.127" f="427.029" m="323.108" cg="178."/>
<eng-data t="0.184" f="435.457" m="309.818" cg="178."/>
<eng-data t="0.223" f="443.886" m="300.546" cg="178."/>
<eng-data t="0.299" f="469.17" m="281.786" cg="178."/>
<eng-data t="0.399" f="480.408" m="256.115" cg="178."/>
<eng-data t="0.503" f="486.027" m="228.942" cg="178."/>
<eng-data t="0.603" f="474.789" m="202.967" cg="178."/>
<eng-data t="0.702" f="469.17" m="177.702" cg="178."/>
<eng-data t="0.802" f="457.933" m="152.638" cg="178."/>
<eng-data t="0.906" f="443.886" m="127.283" cg="178."/>
<eng-data t="1.002" f="432.648" m="104.534" cg="178."/>
<eng-data t="1.098" f="415.792" m="82.5137" cg="178."/>
<eng-data t="1.205" f="390.507" m="59.1898" cg="178."/>
<eng-data t="1.298" f="368.032" m="40.1183" cg="178."/>
<eng-data t="1.401" f="345.556" m="20.2479" cg="178."/>
<eng-data t="1.443" f="325.891" m="12.6239" cg="178."/>
<eng-data t="1.497" f="216.324" m="4.70823" cg="178."/>
<eng-data t="1.532" f="101.138" m="1.70435" cg="178."/>
<eng-data t="1.57" f="33.713" m="0.318998" cg="178."/>
<eng-data t="1.605" f="0." m="0." cg="178."/>
</data>
</engine>
<engine mfg="Aerotech" code="I357T" Type="reloadable" dia="38." len="202."
initWt="363.5" propWt="166.2" delays="6,10,14" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="310." peakThrust="465.53" throatDia="0." exitDia="0."
Itot="341." burn-time="1.1" massFrac="45.72" Isp="209.22" tDiv="10" tStep="-1."
tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="166.2" cg="101."/>
<eng-data t="0." f="465.53" m="166.2" cg="101."/>
<eng-data t="0.1" f="407.97" m="144.913" cg="101."/>
<eng-data t="0.4" f="394.67" m="86.2334" cg="101."/>
<eng-data t="0.6" f="363.62" m="49.2751" cg="101."/>
<eng-data t="0.7" f="319.23" m="32.6344" cg="101."/>
<eng-data t="0.8" f="257.18" m="18.5876" cg="101."/>
<eng-data t="0.9" f="190.69" m="7.67322" cg="101."/>
<eng-data t="1." f="62.09" m="1.5131" cg="101."/>
<eng-data t="1.1" f="0." m="0." cg="101."/>
</data>
</engine>
<engine mfg="Aerotech" code="I366R" Type="reloadable" dia="38." len="298." initWt="562."
propWt="318." delays="10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="358.043" peakThrust="485.39" throatDia="0." exitDia="0."
Itot="537.064" burn-time="1.5" massFrac="56.58" Isp="172.22" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="318." cg="149."/>
<eng-data t="0.03" f="323.26" m="315.129" cg="149."/>
<eng-data t="0.09" f="485.39" m="300.765" cg="149."/>
<eng-data t="0.15" f="483.74" m="283.55" cg="149."/>
<eng-data t="0.21" f="479.93" m="266.432" cg="149."/>
<eng-data t="0.27" f="473.37" m="249.498" cg="149."/>
<eng-data t="0.33" f="466.19" m="232.809" cg="149."/>
<eng-data t="0.39" f="457.44" m="216.402" cg="149."/>
<eng-data t="0.45" f="448.75" m="200.305" cg="149."/>
<eng-data t="0.51" f="441.48" m="184.492" cg="149."/>
<eng-data t="0.57" f="430.24" m="169.007" cg="149."/>
<eng-data t="0.63" f="421.52" m="153.877" cg="149."/>
<eng-data t="0.69" f="411.76" m="139.075" cg="149."/>
<eng-data t="0.75" f="398.88" m="124.676" cg="149."/>
<eng-data t="0.81" f="387.5" m="110.707" cg="149."/>
<eng-data t="0.87" f="375.43" m="97.155" cg="149."/>
<eng-data t="0.93" f="361.32" m="84.068" cg="149."/>
<eng-data t="0.99" f="345.06" m="71.5204" cg="149."/>
<eng-data t="1.05" f="330.39" m="59.5222" cg="149."/>
<eng-data t="1.11" f="312.64" m="48.0999" cg="149."/>
<eng-data t="1.17" f="293.51" m="37.3327" cg="149."/>
<eng-data t="1.23" f="275.08" m="27.2327" cg="149."/>
<eng-data t="1.29" f="262.41" m="17.6852" cg="149."/>
<eng-data t="1.35" f="230.88" m="8.92274" cg="149."/>
<eng-data t="1.41" f="118.01" m="2.72532" cg="149."/>
<eng-data t="1.47" f="23.61" m="0.209695" cg="149."/>
<eng-data t="1.5" f="0." m="0." cg="149."/>
</data>
</engine>
<engine mfg="Aerotech" code="I435T" Type="reloadable" dia="38." len="297."
initWt="526.9" propWt="277." delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="397.436" peakThrust="780.77" throatDia="0." exitDia="0." Itot="556.41"
burn-time="1.4" massFrac="52.57" Isp="204.83" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="277." cg="148.5"/>
<eng-data t="0." f="780.77" m="277." cg="148.5"/>
<eng-data t="0.1" f="628.21" m="241.928" cg="148.5"/>
<eng-data t="0.2" f="583.33" m="211.771" cg="148.5"/>
<eng-data t="0.3" f="551.92" m="183.513" cg="148.5"/>
<eng-data t="0.4" f="538.46" m="156.371" cg="148.5"/>
<eng-data t="0.5" f="529.49" m="129.788" cg="148.5"/>
<eng-data t="0.6" f="507.05" m="103.987" cg="148.5"/>
<eng-data t="0.7" f="448.72" m="80.1961" cg="148.5"/>
<eng-data t="0.8" f="403.85" m="58.9741" cg="148.5"/>
<eng-data t="0.9" f="358.97" m="39.9863" cg="148.5"/>
<eng-data t="1." f="314.1" m="23.2324" cg="148.5"/>
<eng-data t="1.1" f="197.44" m="10.4993" cg="148.5"/>
<eng-data t="1.2" f="89.74" m="3.35092" cg="148.5"/>
<eng-data t="1.3" f="22.44" m="0.55857" cg="148.5"/>
<eng-data t="1.4" f="0." m="0." cg="148.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="I49WN" Type="reloadable" dia="38." len="184." initWt="398."
propWt="205." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="48.372" peakThrust="63.438" throatDia="0." exitDia="0." Itot="384.119"
burn-time="7.94" massFrac="51.51" Isp="191.07" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Aerotech I49N-P</comments>
<data>
<eng-data t="0." f="0." m="205." cg="92."/>
<eng-data t="0.008" f="1.406" m="204.997" cg="92."/>
<eng-data t="0.025" f="48.594" m="204.77" cg="92."/>
<eng-data t="0.093" f="52.031" m="202.944" cg="92."/>
<eng-data t="0.429" f="57.344" m="193.138" cg="92."/>
<eng-data t="0.665" f="60.313" m="185.728" cg="92."/>
<eng-data t="0.841" f="60.625" m="180.048" cg="92."/>
<eng-data t="1.06" f="62.344" m="172.862" cg="92."/>
<eng-data t="1.295" f="63.438" m="164.975" cg="92."/>
<eng-data t="1.556" f="62.344" m="156.214" cg="92."/>
<eng-data t="1.825" f="62.344" m="147.264" cg="92."/>
<eng-data t="1.994" f="60.625" m="141.719" cg="92."/>
<eng-data t="2.212" f="60.156" m="134.693" cg="92."/>
<eng-data t="3.003" f="56.719" m="110.023" cg="92."/>
<eng-data t="3.785" f="52.344" m="87.2648" cg="92."/>
<eng-data t="4.349" f="49.375" m="71.9561" cg="92."/>
<eng-data t="4.997" f="46.563" m="55.367" cg="92."/>
<eng-data t="5.998" f="43.438" m="31.3267" cg="92."/>
<eng-data t="6.393" f="42.031" m="22.3179" cg="92."/>
<eng-data t="6.831" f="41.563" m="12.5476" cg="92."/>
<eng-data t="6.999" f="36.875" m="9.03125" cg="92."/>
<eng-data t="7.083" f="33.125" m="7.46221" cg="92."/>
<eng-data t="7.184" f="31.406" m="5.72301" cg="92."/>
<eng-data t="7.369" f="23.125" m="3.03102" cg="92."/>
<eng-data t="7.495" f="16.406" m="1.70189" cg="92."/>
<eng-data t="7.764" f="4.219" m="0.221405" cg="92."/>
<eng-data t="7.882" f="1.875" m="0.0295197" cg="92."/>
<eng-data t="7.941" f="0." m="0." cg="92."/>
</data>
</engine>
<engine mfg="Aerotech" code="I500T" Type="single-use" dia="38." len="355." initWt="580."
propWt="248." delays="14" auto-calc-mass="1" auto-calc-cg="1" avgThrust="466.415"
peakThrust="581.557" throatDia="0." exitDia="0." Itot="622.663" burn-time="1.33"
massFrac="42.76" Isp="256.02" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<comments>At DMS I500T</comments>
<data>
<eng-data t="0." f="0." m="248." cg="177.5"/>
<eng-data t="0.008" f="447.072" m="247.288" cg="177.5"/>
<eng-data t="0.014" f="534.306" m="246.115" cg="177.5"/>
<eng-data t="0.028" f="581.557" m="243.004" cg="177.5"/>
<eng-data t="0.052" f="504.016" m="237.816" cg="177.5"/>
<eng-data t="0.09" f="514.92" m="230.105" cg="177.5"/>
<eng-data t="0.11" f="533.094" m="225.931" cg="177.5"/>
<eng-data t="0.131" f="524.613" m="221.507" cg="177.5"/>
<eng-data t="0.177" f="551.268" m="211.652" cg="177.5"/>
<eng-data t="0.202" f="540.364" m="206.217" cg="177.5"/>
<eng-data t="0.23" f="552.479" m="200.123" cg="177.5"/>
<eng-data t="0.29" f="543.998" m="187.022" cg="177.5"/>
<eng-data t="0.399" f="552.479" m="163.221" cg="177.5"/>
<eng-data t="0.481" f="553.691" m="145.157" cg="177.5"/>
<eng-data t="0.526" f="563.384" m="135.146" cg="177.5"/>
<eng-data t="0.565" f="554.902" m="126.461" cg="177.5"/>
<eng-data t="0.6" f="564.595" m="118.658" cg="177.5"/>
<eng-data t="0.638" f="558.537" m="110.159" cg="177.5"/>
<eng-data t="0.728" f="567.018" m="89.9855" cg="177.5"/>
<eng-data t="0.8" f="560.96" m="73.8121" cg="177.5"/>
<eng-data t="0.922" f="537.94" m="47.1136" cg="177.5"/>
<eng-data t="0.979" f="535.517" m="34.9285" cg="177.5"/>
<eng-data t="0.999" f="546.421" m="30.6193" cg="177.5"/>
<eng-data t="1.02" f="550.056" m="26.0338" cg="177.5"/>
<eng-data t="1.043" f="535.517" m="21.0615" cg="177.5"/>
<eng-data t="1.064" f="444.649" m="16.9624" cg="177.5"/>
<eng-data t="1.091" f="322.28" m="12.8387" cg="177.5"/>
<eng-data t="1.11" f="267.759" m="10.6062" cg="177.5"/>
<eng-data t="1.141" f="225.353" m="7.56194" cg="177.5"/>
<eng-data t="1.152" f="181.737" m="6.67017" cg="177.5"/>
<eng-data t="1.16" f="238.681" m="6.00038" cg="177.5"/>
<eng-data t="1.163" f="149.024" m="5.76875" cg="177.5"/>
<eng-data t="1.174" f="118.735" m="5.1822" cg="177.5"/>
<eng-data t="1.2" f="118.735" m="3.95264" cg="177.5"/>
<eng-data t="1.255" f="86.022" m="1.70995" cg="177.5"/>
<eng-data t="1.312" f="46.04" m="0.210878" cg="177.5"/>
<eng-data t="1.335" f="0." m="0." cg="177.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="I599N" Type="reloadable" dia="54." len="156."
initWt="520.051" propWt="195." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="649.618" peakThrust="797.44" throatDia="0." exitDia="0."
Itot="404.712" burn-time="0.62" massFrac="37.5" Isp="211.64" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Aerotech I599N from TRA Cert Data</comments>
<data>
<eng-data t="0." f="0." m="195." cg="78."/>
<eng-data t="0.007" f="179.424" m="194.697" cg="78."/>
<eng-data t="0.01" f="495.908" m="194.209" cg="78."/>
<eng-data t="0.012" f="578.144" m="193.692" cg="78."/>
<eng-data t="0.014" f="647.92" m="193.101" cg="78."/>
<eng-data t="0.017" f="797.44" m="192.056" cg="78."/>
<eng-data t="0.024" f="593.096" m="189.711" cg="78."/>
<eng-data t="0.032" f="647.92" m="187.32" cg="78."/>
<eng-data t="0.045" f="677.824" m="183.168" cg="78."/>
<eng-data t="0.051" f="702.744" m="181.172" cg="78."/>
<eng-data t="0.055" f="677.824" m="179.842" cg="78."/>
<eng-data t="0.062" f="720.188" m="177.484" cg="78."/>
<eng-data t="0.076" f="707.728" m="172.668" cg="78."/>
<eng-data t="0.12" f="752.584" m="157.189" cg="78."/>
<eng-data t="0.202" f="757.568" m="127.356" cg="78."/>
<eng-data t="0.225" f="755.076" m="118.974" cg="78."/>
<eng-data t="0.241" f="735.14" m="113.23" cg="78."/>
<eng-data t="0.25" f="720.188" m="110.075" cg="78."/>
<eng-data t="0.263" f="730.156" m="105.532" cg="78."/>
<eng-data t="0.329" f="722.68" m="82.432" cg="78."/>
<eng-data t="0.399" f="697.76" m="58.478" cg="78."/>
<eng-data t="0.45" f="667.856" m="41.6993" cg="78."/>
<eng-data t="0.501" f="618.016" m="25.9004" cg="78."/>
<eng-data t="0.536" f="585.62" m="15.7515" cg="78."/>
<eng-data t="0.55" f="580.636" m="11.8179" cg="78."/>
<eng-data t="0.564" f="585.62" m="7.88443" cg="78."/>
<eng-data t="0.578" f="632.968" m="3.77442" cg="78."/>
<eng-data t="0.581" f="555.716" m="2.91531" cg="78."/>
<eng-data t="0.584" f="426.132" m="2.2057" cg="78."/>
<eng-data t="0.589" f="299.04" m="1.33218" cg="78."/>
<eng-data t="0.595" f="176.932" m="0.644179" cg="78."/>
<eng-data t="0.598" f="112.14" m="0.435256" cg="78."/>
<eng-data t="0.604" f="57.316" m="0.190312" cg="78."/>
<eng-data t="0.608" f="24.92" m="0.111065" cg="78."/>
<eng-data t="0.619" f="12.46" m="0.0120071" cg="78."/>
<eng-data t="0.623" f="0." m="0." cg="78."/>
</data>
</engine>
<engine mfg="Aerotech" code="I59WN" Type="reloadable" dia="38." len="232." initWt="487."
propWt="272." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="56.567" peakThrust="171.786" throatDia="0." exitDia="0."
Itot="486.706" burn-time="8.6" massFrac="55.85" Isp="182.46" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Aerotech I59WN-P</comments>
<data>
<eng-data t="0." f="0." m="272." cg="116."/>
<eng-data t="0.009" f="0.357" m="271.999" cg="116."/>
<eng-data t="0.046" f="138.571" m="270.563" cg="116."/>
<eng-data t="0.12" f="150." m="264.596" cg="116."/>
<eng-data t="0.193" f="147.857" m="258.52" cg="116."/>
<eng-data t="0.368" f="157.857" m="243.57" cg="116."/>
<eng-data t="0.506" f="167.857" m="231.01" cg="116."/>
<eng-data t="0.699" f="171.071" m="212.732" cg="116."/>
<eng-data t="0.791" f="171.786" m="203.918" cg="116."/>
<eng-data t="0.893" f="168.571" m="194.217" cg="116."/>
<eng-data t="1.058" f="158.214" m="179.151" cg="116."/>
<eng-data t="1.233" f="146.429" m="164.253" cg="116."/>
<eng-data t="1.417" f="132.143" m="149.931" cg="116."/>
<eng-data t="1.509" f="125.714" m="143.302" cg="116."/>
<eng-data t="1.61" f="100.357" m="136.922" cg="116."/>
<eng-data t="1.675" f="80.357" m="133.639" cg="116."/>
<eng-data t="1.785" f="60.357" m="129.314" cg="116."/>
<eng-data t="1.96" f="53.571" m="123.743" cg="116."/>
<eng-data t="2.209" f="48.571" m="116.636" cg="116."/>
<eng-data t="2.531" f="45.357" m="108.185" cg="116."/>
<eng-data t="2.669" f="43.214" m="104.769" cg="116."/>
<eng-data t="3.009" f="40.714" m="96.7958" cg="116."/>
<eng-data t="3.387" f="40.714" m="88.195" cg="116."/>
<eng-data t="4.021" f="38.929" m="74.0856" cg="116."/>
<eng-data t="4.261" f="37.5" m="68.96" cg="116."/>
<eng-data t="4.997" f="36.429" m="53.7557" cg="116."/>
<eng-data t="6." f="33.929" m="34.0366" cg="116."/>
<eng-data t="6.883" f="31.429" m="17.9104" cg="116."/>
<eng-data t="7.003" f="33.571" m="15.7309" cg="116."/>
<eng-data t="7.187" f="30.714" m="12.4257" cg="116."/>
<eng-data t="7.334" f="27.5" m="10.0345" cg="116."/>
<eng-data t="7.574" f="22.5" m="6.6813" cg="116."/>
<eng-data t="7.96" f="17.5" m="2.3669" cg="116."/>
<eng-data t="8.117" f="9.643" m="1.17613" cg="116."/>
<eng-data t="8.319" f="4.643" m="0.369757" cg="116."/>
<eng-data t="8.604" f="0." m="0." cg="116."/>
</data>
</engine>
<engine mfg="Aerotech" code="I600R" Type="reloadable" dia="38." len="344.68"
initWt="617." propWt="323.7" delays="10" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="542.493" peakThrust="817.754" throatDia="0." exitDia="0."
Itot="640.142" burn-time="1.18" massFrac="52.46" Isp="201.66" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>I600R Data Entered by Tim Van Milligan
For RockSim: www.RockSim.com
Based on Aerotech's Reload Kit Instruction Sheet.
Not Officially Approved by TRA or Aerotech
</comments>
<data>
<eng-data t="0." f="0." m="323.7" cg="172.34"/>
<eng-data t="0.005" f="40.438" m="323.649" cg="172.34"/>
<eng-data t="0.046" f="817.754" m="314.753" cg="172.34"/>
<eng-data t="0.059" f="813.261" m="309.392" cg="172.34"/>
<eng-data t="0.1" f="772.822" m="292.95" cg="172.34"/>
<eng-data t="0.2" f="736.877" m="254.78" cg="172.34"/>
<eng-data t="0.4" f="696.439" m="182.301" cg="172.34"/>
<eng-data t="0.5" f="669.48" m="147.766" cg="172.34"/>
<eng-data t="0.6" f="620.055" m="115.162" cg="172.34"/>
<eng-data t="0.796" f="539.178" m="57.7157" cg="172.34"/>
<eng-data t="0.894" f="485.261" m="32.3324" cg="172.34"/>
<eng-data t="0.951" f="453.809" m="18.7989" cg="172.34"/>
<eng-data t="0.964" f="435.836" m="15.8748" cg="172.34"/>
<eng-data t="1." f="274.082" m="9.4131" cg="172.34"/>
<eng-data t="1.052" f="152.767" m="3.80114" cg="172.34"/>
<eng-data t="1.106" f="62.904" m="0.856571" cg="172.34"/>
<eng-data t="1.144" f="13.48" m="0.122696" cg="172.34"/>
<eng-data t="1.18" f="0." m="0." cg="172.34"/>
</data>
</engine>
<engine mfg="Aerotech" code="I117FJ" Type="reloadable" dia="54." len="156."
initWt="580." propWt="253." delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="130.267" peakThrust="164.749" throatDia="0." exitDia="0."
Itot="365.528" burn-time="2.81" massFrac="43.62" Isp="147.33" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Aerotech I117FJ from TRA Cert Data</comments>
<data>
<eng-data t="0." f="0." m="253." cg="78."/>
<eng-data t="0.014" f="65.9" m="252.681" cg="78."/>
<eng-data t="0.021" f="94.456" m="252.292" cg="78."/>
<eng-data t="0.055" f="120.816" m="249.759" cg="78."/>
<eng-data t="0.089" f="107.636" m="247.071" cg="78."/>
<eng-data t="0.179" f="107.636" m="240.366" cg="78."/>
<eng-data t="0.344" f="124.111" m="227.133" cg="78."/>
<eng-data t="0.385" f="133.996" m="223.471" cg="78."/>
<eng-data t="0.447" f="123.013" m="217.956" cg="78."/>
<eng-data t="0.509" f="138.389" m="212.347" cg="78."/>
<eng-data t="0.564" f="131.799" m="207.204" cg="78."/>
<eng-data t="0.646" f="146.077" m="199.319" cg="78."/>
<eng-data t="0.708" f="144.979" m="193.074" cg="78."/>
<eng-data t="0.736" f="127.406" m="190.434" cg="78."/>
<eng-data t="0.75" f="149.372" m="189.093" cg="78."/>
<eng-data t="0.798" f="141.684" m="184.258" cg="78."/>
<eng-data t="0.825" f="164.749" m="181.395" cg="78."/>
<eng-data t="0.866" f="152.667" m="176.891" cg="78."/>
<eng-data t="1.004" f="158.159" m="162.047" cg="78."/>
<eng-data t="1.141" f="155.962" m="147.154" cg="78."/>
<eng-data t="1.224" f="154.864" m="138.225" cg="78."/>
<eng-data t="1.492" f="155.962" m="109.397" cg="78."/>
<eng-data t="2.304" f="121.914" m="31.3102" cg="78."/>
<eng-data t="2.407" f="118.619" m="22.7362" cg="78."/>
<eng-data t="2.482" f="117.521" m="16.607" cg="78."/>
<eng-data t="2.544" f="128.504" m="11.3282" cg="78."/>
<eng-data t="2.599" f="112.029" m="6.74984" cg="78."/>
<eng-data t="2.654" f="75.784" m="3.17499" cg="78."/>
<eng-data t="2.695" f="45.031" m="1.46074" cg="78."/>
<eng-data t="2.75" f="16.475" m="0.290027" cg="78."/>
<eng-data t="2.771" f="8.787" m="0.106434" cg="78."/>
<eng-data t="2.806" f="0." m="0." cg="78."/>
</data>
</engine>
<engine mfg="Aerotech" code="I1299N" Type="reloadable" dia="38." len="249."
initWt="422." propWt="192." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1248.44" peakThrust="1491." throatDia="0." exitDia="0." Itot="424.469"
burn-time="0.34" massFrac="45.5" Isp="225.44" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Entered by Jim Yehle
from TRA cert document
</comments>
<data>
<eng-data t="0." f="0." m="192." cg="124.5"/>
<eng-data t="0." f="15.7171" m="192." cg="124.5"/>
<eng-data t="0.00361" f="222.5" m="191.806" cg="124.5"/>
<eng-data t="0.0115" f="1112." m="189.424" cg="124.5"/>
<eng-data t="0.0134228" f="1237.11" m="188.403" cg="124.5"/>
<eng-data t="0.02" f="1287." m="184.648" cg="124.5"/>
<eng-data t="0.04" f="1359." m="172.679" cg="124.5"/>
<eng-data t="0.1" f="1451." m="134.548" cg="124.5"/>
<eng-data t="0.12" f="1470." m="121.335" cg="124.5"/>
<eng-data t="0.18" f="1491." m="81.1548" cg="124.5"/>
<eng-data t="0.2" f="1483." m="67.7025" cg="124.5"/>
<eng-data t="0.22" f="1462." m="54.3814" cg="124.5"/>
<eng-data t="0.24" f="1399." m="41.4402" cg="124.5"/>
<eng-data t="0.28" f="1208." m="17.8557" cg="124.5"/>
<eng-data t="0.294743" f="1131.63" m="10.0547" cg="124.5"/>
<eng-data t="0.3" f="1065." m="7.4429" cg="124.5"/>
<eng-data t="0.304251" f="974.46" m="5.48231" cg="124.5"/>
<eng-data t="0.32" f="305." m="0.92491" cg="124.5"/>
<eng-data t="0.330537" f="55.0098" m="0.0669778" cg="124.5"/>
<eng-data t="0.333893" f="11.7878" m="0.0162822" cg="124.5"/>
<eng-data t="0.34" f="0." m="0." cg="124.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="I225FJ" Type="reloadable" dia="38." len="250."
initWt="486." propWt="264." delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="206.264" peakThrust="275.9" throatDia="0." exitDia="0." Itot="371.275"
burn-time="1.8" massFrac="54.32" Isp="143.41" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Converted from RASP file by Chris Kobel mfr data
Curvefit to instruction sheet on Aerotech website (12/27/06)</comments>
<data>
<eng-data t="0." f="0." m="264." cg="120."/>
<eng-data t="0.04" f="213.6" m="260.962" cg="120."/>
<eng-data t="0.1" f="213.6" m="251.849" cg="120."/>
<eng-data t="0.2" f="213.6" m="236.661" cg="120."/>
<eng-data t="0.28" f="218.1" m="224.382" cg="120."/>
<eng-data t="0.3" f="235.9" m="221.154" cg="120."/>
<eng-data t="0.4" f="249.2" m="203.907" cg="120."/>
<eng-data t="0.5" f="262.6" m="185.711" cg="120."/>
<eng-data t="0.6" f="267." m="166.882" cg="120."/>
<eng-data t="0.7" f="271.5" m="147.737" cg="120."/>
<eng-data t="0.8" f="275.9" m="128.275" cg="120."/>
<eng-data t="0.87" f="275.9" m="114.542" cg="120."/>
<eng-data t="0.9" f="271.5" m="108.704" cg="120."/>
<eng-data t="1." f="258.1" m="89.8748" cg="120."/>
<eng-data t="1.1" f="240.3" m="72.1551" cg="120."/>
<eng-data t="1.2" f="218.1" m="55.8576" cg="120."/>
<eng-data t="1.3" f="200.3" m="40.9821" cg="120."/>
<eng-data t="1.4" f="178." m="27.5324" cg="120."/>
<eng-data t="1.5" f="160.2" m="15.5083" cg="120."/>
<eng-data t="1.6" f="97.9" m="6.33202" cg="120."/>
<eng-data t="1.7" f="40.1" m="1.42568" cg="120."/>
<eng-data t="1.8" f="0." m="0." cg="120."/>
</data>
</engine>
<engine mfg="Aerotech" code="I280DM" Type="single-use" dia="38." len="356.4"
initWt="616." propWt="355." delays="14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="282.802" peakThrust="342.389" throatDia="0." exitDia="0."
Itot="557.402" burn-time="1.97" massFrac="57.63" Isp="160.11" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>I280DM DMS</comments>
<data>
<eng-data t="0." f="0." m="355." cg="178.2"/>
<eng-data t="0.016" f="342.389" m="353.256" cg="178.2"/>
<eng-data t="0.048" f="297.021" m="346.74" cg="178.2"/>
<eng-data t="0.111" f="316.16" m="334.438" cg="178.2"/>
<eng-data t="0.173" f="328.211" m="321.716" cg="178.2"/>
<eng-data t="0.202" f="327.502" m="315.661" cg="178.2"/>
<eng-data t="0.261" f="322.54" m="303.448" cg="178.2"/>
<eng-data t="0.334" f="311.907" m="288.699" cg="178.2"/>
<eng-data t="0.498" f="310.489" m="256.195" cg="178.2"/>
<eng-data t="0.602" f="308.363" m="235.7" cg="178.2"/>
<eng-data t="0.705" f="307.654" m="215.495" cg="178.2"/>
<eng-data t="0.802" f="310.489" m="196.401" cg="178.2"/>
<eng-data t="0.902" f="310.489" m="176.627" cg="178.2"/>
<eng-data t="1." f="306.236" m="157.38" cg="178.2"/>
<eng-data t="1.025" f="316.869" m="152.42" cg="178.2"/>
<eng-data t="1.057" f="309.072" m="146.041" cg="178.2"/>
<eng-data t="1.1" f="308.363" m="137.587" cg="178.2"/>
<eng-data t="1.139" f="317.578" m="129.813" cg="178.2"/>
<eng-data t="1.205" f="307.654" m="116.673" cg="178.2"/>
<eng-data t="1.298" f="304.109" m="98.5551" cg="178.2"/>
<eng-data t="1.336" f="316.16" m="91.0494" cg="178.2"/>
<eng-data t="1.4" f="299.856" m="78.4948" cg="178.2"/>
<eng-data t="1.5" f="296.312" m="59.5103" cg="178.2"/>
<eng-data t="1.55" f="298.438" m="50.0407" cg="178.2"/>
<eng-data t="1.595" f="306.945" m="41.3656" cg="178.2"/>
<eng-data t="1.634" f="295.603" m="33.8824" cg="178.2"/>
<eng-data t="1.652" f="280.716" m="30.579" cg="178.2"/>
<eng-data t="1.716" f="253.07" m="19.7003" cg="178.2"/>
<eng-data t="1.743" f="224.006" m="15.5984" cg="178.2"/>
<eng-data t="1.8" f="153.827" m="8.7403" cg="178.2"/>
<eng-data t="1.9" f="62.381" m="1.85533" cg="178.2"/>
<eng-data t="1.97" f="20.558" m="0.00654652" cg="178.2"/>
<eng-data t="1.971" f="0." m="0." cg="178.2"/>
</data>
</engine>
<engine mfg="Aerotech" code="I305FJ" Type="reloadable" dia="38." len="298."
initWt="581." propWt="302." delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="277.44" peakThrust="405.662" throatDia="0." exitDia="0."
Itot="443.903" burn-time="1.6" massFrac="51.98" Isp="149.89" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>I305FJ based on Aerotech instruction sheet by C. Kobel 3/30/07</comments>
<data>
<eng-data t="0." f="0." m="302." cg="149."/>
<eng-data t="0.02" f="341.398" m="299.677" cg="149."/>
<eng-data t="0.1" f="365.497" m="280.441" cg="149."/>
<eng-data t="0.2" f="383.571" m="254.96" cg="149."/>
<eng-data t="0.3" f="403.653" m="228.181" cg="149."/>
<eng-data t="0.4" f="405.662" m="200.651" cg="149."/>
<eng-data t="0.5" f="405.662" m="173.053" cg="149."/>
<eng-data t="0.6" f="404.657" m="145.489" cg="149."/>
<eng-data t="0.7" f="374.534" m="118.984" cg="149."/>
<eng-data t="0.8" f="342.402" m="94.596" cg="149."/>
<eng-data t="0.9" f="309.267" m="72.4285" cg="149."/>
<eng-data t="1." f="272.115" m="52.652" cg="149."/>
<eng-data t="1.1" f="238.979" m="35.2664" cg="149."/>
<eng-data t="1.15" f="224.921" m="27.3763" cg="149."/>
<eng-data t="1.2" f="194.798" m="20.2376" cg="149."/>
<eng-data t="1.3" f="119.489" m="9.54671" cg="149."/>
<eng-data t="1.4" f="62.255" m="3.36443" cg="149."/>
<eng-data t="1.45" f="33.136" m="1.742" cg="149."/>
<eng-data t="1.5" f="23.095" m="0.785609" cg="149."/>
<eng-data t="1.6" f="0." m="0." cg="149."/>
</data>
</engine>
<engine mfg="Aerotech" code="I327DM" Type="reloadable" dia="38." len="337."
initWt="628." propWt="354." delays="14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="315.022" peakThrust="432.602" throatDia="0." exitDia="0."
Itot="542.784" burn-time="1.72" massFrac="56.37" Isp="156.35" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>I327-14 Dark Matter</comments>
<data>
<eng-data t="0." f="0." m="354." cg="168.5"/>
<eng-data t="0.009" f="393.741" m="352.844" cg="168.5"/>
<eng-data t="0.026" f="432.602" m="348.263" cg="168.5"/>
<eng-data t="0.161" f="387.142" m="312.176" cg="168.5"/>
<eng-data t="0.245" f="382.742" m="291.087" cg="168.5"/>
<eng-data t="0.303" f="371.011" m="276.831" cg="168.5"/>
<eng-data t="0.601" f="372.477" m="204.581" cg="168.5"/>
<eng-data t="0.702" f="371.011" m="180.094" cg="168.5"/>
<eng-data t="0.798" f="375.41" m="156.727" cg="168.5"/>
<eng-data t="0.983" f="371.744" m="111.653" cg="168.5"/>
<eng-data t="1.04" f="370.278" m="97.8602" cg="168.5"/>
<eng-data t="1.104" f="371.744" m="82.3741" cg="168.5"/>
<eng-data t="1.199" f="343.148" m="60.2273" cg="168.5"/>
<eng-data t="1.3" f="335.816" m="37.8651" cg="168.5"/>
<eng-data t="1.335" f="357.813" m="29.9485" cg="168.5"/>
<eng-data t="1.365" f="327.751" m="23.2417" cg="168.5"/>
<eng-data t="1.399" f="265.427" m="16.6649" cg="168.5"/>
<eng-data t="1.428" f="185.505" m="12.4006" cg="168.5"/>
<eng-data t="1.451" f="156.91" m="9.83237" cg="168.5"/>
<eng-data t="1.493" f="112.183" m="6.14685" cg="168.5"/>
<eng-data t="1.553" f="68.19" m="2.61771" cg="168.5"/>
<eng-data t="1.601" f="32.262" m="1.04537" cg="168.5"/>
<eng-data t="1.656" f="11.732" m="0.256326" cg="168.5"/>
<eng-data t="1.723" f="0." m="0." cg="168.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="I364FJ" Type="reloadable" dia="38." len="345."
initWt="678." propWt="362.5" delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="324.236" peakThrust="413.9" throatDia="0." exitDia="0." Itot="551.202"
burn-time="1.7" massFrac="53.47" Isp="155.05" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>AeroTech I364FJ
Curvefit to instruction sheet on Aerotech website (12/27/06)
by Chris Kobel
burn time: 1.7 seconds
total impulse: 551.2 newton-seconds
average thrust: 72.9 pounds
</comments>
<data>
<eng-data t="0." f="0." m="362.5" cg="172.5"/>
<eng-data t="0.02" f="356." m="360.159" cg="172.5"/>
<eng-data t="0.1" f="373.8" m="340.961" cg="172.5"/>
<eng-data t="0.2" f="387.2" m="315.937" cg="172.5"/>
<eng-data t="0.3" f="400.5" m="290.035" cg="172.5"/>
<eng-data t="0.4" f="400.5" m="263.696" cg="172.5"/>
<eng-data t="0.5" f="409.4" m="237.064" cg="172.5"/>
<eng-data t="0.6" f="413.9" m="209.992" cg="172.5"/>
<eng-data t="0.7" f="409.4" m="182.92" cg="172.5"/>
<eng-data t="0.8" f="382.7" m="156.873" cg="172.5"/>
<eng-data t="0.9" f="373.8" m="131.998" cg="172.5"/>
<eng-data t="1." f="351.6" m="108.145" cg="172.5"/>
<eng-data t="1.1" f="333.8" m="85.6068" cg="172.5"/>
<eng-data t="1.2" f="320.4" m="64.0949" cg="172.5"/>
<eng-data t="1.3" f="311.5" m="43.3164" cg="172.5"/>
<eng-data t="1.4" f="244.8" m="25.0237" cg="172.5"/>
<eng-data t="1.5" f="178." m="11.1209" cg="172.5"/>
<eng-data t="1.6" f="80.1" m="2.6339" cg="172.5"/>
<eng-data t="1.7" f="0." m="0." cg="172.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="J90W" Type="reloadable" dia="54." len="241." initWt="834.1"
propWt="391.4" delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="98.895" peakThrust="173.83" throatDia="0." exitDia="0." Itot="741.715"
burn-time="7.5" massFrac="46.92" Isp="193.24" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="391.4" cg="120.5"/>
<eng-data t="0." f="120.9" m="391.4" cg="120.5"/>
<eng-data t="1." f="155.5" m="318.472" cg="120.5"/>
<eng-data t="2." f="173.83" m="231.579" cg="120.5"/>
<eng-data t="2.5" f="173.34" m="185.779" cg="120.5"/>
<eng-data t="3." f="163.73" m="141.312" cg="120.5"/>
<eng-data t="3.5" f="142.69" m="100.888" cg="120.5"/>
<eng-data t="4." f="107.51" m="67.8802" cg="120.5"/>
<eng-data t="5." f="54.44" m="25.15" cg="120.5"/>
<eng-data t="5.5" f="34.74" m="13.385" cg="120.5"/>
<eng-data t="6." f="19.66" m="6.20834" cg="120.5"/>
<eng-data t="6.5" f="10.05" m="2.28888" cg="120.5"/>
<eng-data t="7." f="3.65" m="0.481523" cg="120.5"/>
<eng-data t="7.5" f="0." m="0." cg="120.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="J135W" Type="reloadable" dia="54." len="368."
initWt="1125.7" propWt="587.1" delays="6,10,14" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="157.619" peakThrust="270.44" throatDia="0."
exitDia="0." Itot="1103.33" burn-time="7." massFrac="52.15" Isp="191.63"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="587.1" cg="184."/>
<eng-data t="0." f="152.12" m="587.1" cg="184."/>
<eng-data t="1.5" f="239.75" m="430.71" cg="184."/>
<eng-data t="2." f="260.21" m="364.2" cg="184."/>
<eng-data t="2.5" f="270.44" m="293.609" cg="184."/>
<eng-data t="3." f="265.55" m="222.306" cg="184."/>
<eng-data t="3.5" f="233.52" m="155.915" cg="184."/>
<eng-data t="4." f="176.14" m="101.419" cg="184."/>
<eng-data t="4.5" f="127.66" m="61.0045" cg="184."/>
<eng-data t="5." f="85.4" m="32.6613" cg="184."/>
<eng-data t="5.5" f="48.48" m="14.8514" cg="184."/>
<eng-data t="6." f="23.57" m="5.26662" cg="184."/>
<eng-data t="6.5" f="8.01" m="1.06556" cg="184."/>
<eng-data t="7." f="0." m="0." cg="184."/>
</data>
</engine>
<engine mfg="Aerotech" code="J180T" Type="reloadable" dia="54." len="230."
initWt="840.9" propWt="398.2" delays="6,10,14" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="183.505" peakThrust="360.56" throatDia="0."
exitDia="0." Itot="825.773" burn-time="4.5" massFrac="47.35" Isp="211.47"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="398.2" cg="115."/>
<eng-data t="0." f="0.04" m="398.2" cg="115."/>
<eng-data t="0.1" f="360.56" m="389.506" cg="115."/>
<eng-data t="0.2" f="341.61" m="372.576" cg="115."/>
<eng-data t="0.5" f="351.08" m="322.472" cg="115."/>
<eng-data t="1." f="327.37" m="240.682" cg="115."/>
<eng-data t="1.7" f="265.68" m="140.59" cg="115."/>
<eng-data t="2.6" f="142.34" m="52.0514" cg="115."/>
<eng-data t="3.5" f="52.17" m="9.84345" cg="115."/>
<eng-data t="3.7" f="33.23" m="5.72533" cg="115."/>
<eng-data t="4.3" f="4.76" m="0.229534" cg="115."/>
<eng-data t="4.5" f="0." m="0." cg="115."/>
</data>
</engine>
<engine mfg="Aerotech" code="J270W" Type="single-use" dia="38." len="356.4"
initWt="642." propWt="381." delays="14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="273.691" peakThrust="367.585" throatDia="0." exitDia="0."
Itot="701.47" burn-time="2.56" massFrac="59.35" Isp="187.74" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>J270W DMS</comments>
<data>
<eng-data t="0." f="0." m="381." cg="178.2"/>
<eng-data t="0.007" f="367.585" m="380.301" cg="178.2"/>
<eng-data t="0.02" f="325.124" m="377.856" cg="178.2"/>
<eng-data t="0.074" f="353.027" m="367.911" cg="178.2"/>
<eng-data t="0.136" f="329.977" m="356.411" cg="178.2"/>
<eng-data t="0.176" f="343.928" m="349.09" cg="178.2"/>
<eng-data t="0.273" f="324.518" m="331.481" cg="178.2"/>
<eng-data t="0.33" f="342.715" m="321.153" cg="178.2"/>
<eng-data t="0.357" f="326.338" m="316.247" cg="178.2"/>
<eng-data t="0.399" f="330.584" m="308.754" cg="178.2"/>
<eng-data t="0.473" f="310.567" m="295.869" cg="178.2"/>
<eng-data t="0.553" f="325.731" m="282.045" cg="178.2"/>
<eng-data t="0.734" f="340.895" m="249.278" cg="178.2"/>
<eng-data t="0.744" f="357.273" m="247.382" cg="178.2"/>
<eng-data t="0.761" f="315.419" m="244.276" cg="178.2"/>
<eng-data t="0.788" f="337.256" m="239.49" cg="178.2"/>
<eng-data t="0.897" f="340.895" m="219.416" cg="178.2"/>
<eng-data t="1.009" f="333.617" m="198.9" cg="178.2"/>
<eng-data t="1.053" f="354.24" m="190.681" cg="178.2"/>
<eng-data t="1.105" f="320.878" m="181.147" cg="178.2"/>
<eng-data t="1.18" f="345.748" m="167.569" cg="178.2"/>
<eng-data t="1.214" f="321.485" m="161.408" cg="178.2"/>
<eng-data t="1.249" f="345.748" m="155.066" cg="178.2"/>
<eng-data t="1.274" f="314.206" m="150.585" cg="178.2"/>
<eng-data t="1.5" f="316.026" m="111.905" cg="178.2"/>
<eng-data t="1.601" f="309.96" m="94.7347" cg="178.2"/>
<eng-data t="1.916" f="303.894" m="42.2224" cg="178.2"/>
<eng-data t="1.956" f="265.073" m="36.0417" cg="178.2"/>
<eng-data t="2." f="214.121" m="30.3158" cg="178.2"/>
<eng-data t="2.052" f="179.546" m="24.7565" cg="178.2"/>
<eng-data t="2.102" f="158.923" m="20.1605" cg="178.2"/>
<eng-data t="2.201" f="117.676" m="12.724" cg="178.2"/>
<eng-data t="2.268" f="106.151" m="8.65139" cg="178.2"/>
<eng-data t="2.303" f="87.953" m="6.80642" cg="178.2"/>
<eng-data t="2.369" f="55.805" m="4.22973" cg="178.2"/>
<eng-data t="2.407" f="49.739" m="3.14055" cg="178.2"/>
<eng-data t="2.486" f="39.427" m="1.22756" cg="178.2"/>
<eng-data t="2.558" f="21.837" m="0.0296516" cg="178.2"/>
<eng-data t="2.563" f="0." m="0." cg="178.2"/>
</data>
</engine>
<engine mfg="Aerotech" code="J275W" Type="reloadable" dia="54." len="241."
initWt="882.9" propWt="440.2" delays="6,10,14,18" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="255.842" peakThrust="350.5" throatDia="0."
exitDia="0." Itot="818.693" burn-time="3.2" massFrac="49.86" Isp="189.65"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="440.2" cg="120.5"/>
<eng-data t="0." f="0.45" m="440.2" cg="120.5"/>
<eng-data t="0.1" f="331.55" m="431.274" cg="120.5"/>
<eng-data t="0.2" f="293.61" m="414.467" cg="120.5"/>
<eng-data t="0.7" f="326.8" m="331.071" cg="120.5"/>
<eng-data t="1.3" f="350.5" m="221.818" cg="120.5"/>
<eng-data t="1.6" f="350.5" m="165.281" cg="120.5"/>
<eng-data t="2.1" f="307.85" m="76.7843" cg="120.5"/>
<eng-data t="2.3" f="269.99" m="45.7146" cg="120.5"/>
<eng-data t="2.4" f="227.34" m="32.3442" cg="120.5"/>
<eng-data t="2.7" f="85.27" m="7.13133" cg="120.5"/>
<eng-data t="2.8" f="47.37" m="3.5654" cg="120.5"/>
<eng-data t="3." f="9.47" m="0.509189" cg="120.5"/>
<eng-data t="3.2" f="0." m="0." cg="120.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="J315R" Type="reloadable" dia="54." len="230." initWt="863."
propWt="429." delays="14,1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="291.179" peakThrust="376.06" throatDia="0." exitDia="0."
Itot="757.065" burn-time="2.6" massFrac="49.71" Isp="179.95" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="429." cg="115."/>
<eng-data t="0.05" f="189.72" m="426.312" cg="115."/>
<eng-data t="0.15" f="337.53" m="411.374" cg="115."/>
<eng-data t="0.26" f="354.53" m="389.805" cg="115."/>
<eng-data t="0.36" f="364.11" m="369.443" cg="115."/>
<eng-data t="0.47" f="371.48" m="346.518" cg="115."/>
<eng-data t="0.57" f="373.22" m="325.418" cg="115."/>
<eng-data t="0.68" f="376.06" m="302.066" cg="115."/>
<eng-data t="0.78" f="372.96" m="280.844" cg="115."/>
<eng-data t="0.88" f="368.99" m="259.822" cg="115."/>
<eng-data t="0.99" f="366.98" m="236.884" cg="115."/>
<eng-data t="1.09" f="358.75" m="216.322" cg="115."/>
<eng-data t="1.2" f="351.3" m="194.192" cg="115."/>
<eng-data t="1.3" f="339.34" m="174.624" cg="115."/>
<eng-data t="1.41" f="325.2" m="153.913" cg="115."/>
<eng-data t="1.51" f="311.32" m="135.879" cg="115."/>
<eng-data t="1.61" f="300.5" m="118.544" cg="115."/>
<eng-data t="1.72" f="288.6" m="100.184" cg="115."/>
<eng-data t="1.82" f="278.28" m="84.1221" cg="115."/>
<eng-data t="1.93" f="270.54" m="67.0174" cg="115."/>
<eng-data t="2.03" f="262.13" m="51.9252" cg="115."/>
<eng-data t="2.14" f="245.03" m="36.1188" cg="115."/>
<eng-data t="2.24" f="236.24" m="22.483" cg="115."/>
<eng-data t="2.34" f="188.31" m="10.4541" cg="115."/>
<eng-data t="2.45" f="63.67" m="2.60084" cg="115."/>
<eng-data t="2.55" f="18.75" m="0.265623" cg="115."/>
<eng-data t="2.6" f="0." m="0." cg="115."/>
</data>
</engine>
<engine mfg="Aerotech" code="J340M" Type="reloadable" dia="38." len="337."
initWt="577.3" propWt="365." delays="14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="298.067" peakThrust="606.518" throatDia="0." exitDia="0."
Itot="652.767" burn-time="2.19" massFrac="63.23" Isp="182.37" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>AT J340 Metalstorm for 38-720</comments>
<data>
<eng-data t="0." f="0." m="365." cg="168.5"/>
<eng-data t="0.005" f="361.55" m="364.495" cg="168.5"/>
<eng-data t="0.008" f="501.742" m="363.771" cg="168.5"/>
<eng-data t="0.026" f="606.518" m="358.193" cg="168.5"/>
<eng-data t="0.096" f="491.412" m="336.706" cg="168.5"/>
<eng-data t="0.214" f="453.044" m="305.548" cg="168.5"/>
<eng-data t="0.485" f="439.762" m="237.904" cg="168.5"/>
<eng-data t="0.772" f="435.335" m="167.687" cg="168.5"/>
<eng-data t="0.826" f="426.481" m="154.676" cg="168.5"/>
<eng-data t="0.891" f="423.53" m="139.229" cg="168.5"/>
<eng-data t="1.048" f="383.685" m="103.797" cg="168.5"/>
<eng-data t="1.389" f="311.375" m="37.5323" cg="168.5"/>
<eng-data t="1.425" f="308.424" m="31.2941" cg="168.5"/>
<eng-data t="1.459" f="309.9" m="25.4165" cg="168.5"/>
<eng-data t="1.554" f="182.988" m="12.3254" cg="168.5"/>
<eng-data t="1.611" f="103.3" m="7.76309" cg="168.5"/>
<eng-data t="1.699" f="57.553" m="3.80562" cg="168.5"/>
<eng-data t="1.841" f="11.806" m="1.05205" cg="168.5"/>
<eng-data t="1.898" f="8.854" m="0.722815" cg="168.5"/>
<eng-data t="2.19" f="0." m="0." cg="168.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="J350W" Type="reloadable" dia="38." len="340." initWt="665."
propWt="375." delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="368.581" peakThrust="705.97" throatDia="0." exitDia="0."
Itot="700.304" burn-time="1.9" massFrac="56.39" Isp="190.43" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="375." cg="170."/>
<eng-data t="0." f="705.97" m="375." cg="170."/>
<eng-data t="0.1" f="598.37" m="340.077" cg="170."/>
<eng-data t="0.2" f="571.28" m="308.761" cg="170."/>
<eng-data t="0.3" f="562.33" m="278.41" cg="170."/>
<eng-data t="0.4" f="545.92" m="248.737" cg="170."/>
<eng-data t="0.5" f="517.35" m="220.269" cg="170."/>
<eng-data t="0.6" f="506.91" m="192.846" cg="170."/>
<eng-data t="0.7" f="460.65" m="166.94" cg="170."/>
<eng-data t="0.8" f="448.72" m="142.592" cg="170."/>
<eng-data t="1." f="400.75" m="97.1049" cg="170."/>
<eng-data t="1.2" f="345.32" m="57.1541" cg="170."/>
<eng-data t="1.4" f="269.23" m="24.2461" cg="170."/>
<eng-data t="1.5" f="155.39" m="12.8773" cg="170."/>
<eng-data t="1.7" f="44.76" m="2.1596" cg="170."/>
<eng-data t="1.8" f="17.95" m="0.480595" cg="170."/>
<eng-data t="1.9" f="0." m="0." cg="170."/>
</data>
</engine>
<engine mfg="Aerotech" code="J415W" Type="reloadable" dia="54." len="326."
initWt="1198.9" propWt="660.3" delays="6,10,14" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="343.236" peakThrust="552." throatDia="0."
exitDia="0." Itot="1201.33" burn-time="3.5" massFrac="55.08" Isp="185.52"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="660.3" cg="163."/>
<eng-data t="0." f="552." m="660.3" cg="163."/>
<eng-data t="0.1" f="441.51" m="632.996" cg="163."/>
<eng-data t="0.3" f="463.57" m="583.249" cg="163."/>
<eng-data t="0.5" f="441.51" m="533.502" cg="163."/>
<eng-data t="1.2" f="441.51" m="363.631" cg="163."/>
<eng-data t="1.4" f="450.27" m="314.615" cg="163."/>
<eng-data t="1.7" f="432.66" m="241.821" cg="163."/>
<eng-data t="2.2" f="353.22" m="133.833" cg="163."/>
<eng-data t="2.7" f="264.88" m="48.8992" cg="163."/>
<eng-data t="2.8" f="220.75" m="35.5531" cg="163."/>
<eng-data t="3." f="136.91" m="15.8946" cg="163."/>
<eng-data t="3.1" f="88.29" m="9.70559" cg="163."/>
<eng-data t="3.5" f="0." m="0." cg="163."/>
</data>
</engine>
<engine mfg="Aerotech" code="J420R" Type="reloadable" dia="38." len="337." initWt="659."
propWt="381." delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="404.335" peakThrust="563.47" throatDia="0." exitDia="0."
Itot="650.979" burn-time="1.61" massFrac="57.81" Isp="174.23" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="381." cg="168.5"/>
<eng-data t="0.03" f="61.08" m="380.464" cg="168.5"/>
<eng-data t="0.1" f="563.47" m="367.67" cg="168.5"/>
<eng-data t="0.16" f="525.28" m="348.554" cg="168.5"/>
<eng-data t="0.22" f="521.24" m="330.179" cg="168.5"/>
<eng-data t="0.29" f="527.37" m="308.698" cg="168.5"/>
<eng-data t="0.35" f="537.09" m="290.008" cg="168.5"/>
<eng-data t="0.42" f="535.14" m="268.044" cg="168.5"/>
<eng-data t="0.48" f="534.62" m="249.261" cg="168.5"/>
<eng-data t="0.55" f="530.25" m="227.448" cg="168.5"/>
<eng-data t="0.61" f="526.45" m="208.894" cg="168.5"/>
<eng-data t="0.67" f="517.2" m="190.57" cg="168.5"/>
<eng-data t="0.74" f="510.28" m="169.522" cg="168.5"/>
<eng-data t="0.8" f="500.89" m="151.768" cg="168.5"/>
<eng-data t="0.87" f="479.45" m="131.686" cg="168.5"/>
<eng-data t="0.93" f="460.68" m="115.179" cg="168.5"/>
<eng-data t="1." f="438.59" m="96.7578" cg="168.5"/>
<eng-data t="1.06" f="409.65" m="81.8643" cg="168.5"/>
<eng-data t="1.12" f="383.45" m="67.9389" cg="168.5"/>
<eng-data t="1.19" f="361.02" m="52.6887" cg="168.5"/>
<eng-data t="1.25" f="339.74" m="40.3847" cg="168.5"/>
<eng-data t="1.32" f="319.19" m="26.8868" cg="168.5"/>
<eng-data t="1.38" f="296.71" m="16.0727" cg="168.5"/>
<eng-data t="1.45" f="195.19" m="5.99635" cg="168.5"/>
<eng-data t="1.51" f="61.98" m="1.48092" cg="168.5"/>
<eng-data t="1.58" f="7.22" m="0.063385" cg="168.5"/>
<eng-data t="1.61" f="0." m="0." cg="168.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="J425R" Type="single-use" dia="38." len="356.4"
initWt="631." propWt="364." delays="14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="410.7" peakThrust="452.851" throatDia="0." exitDia="0." Itot="676.833"
burn-time="1.65" massFrac="57.69" Isp="189.61" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>From AT DMS announcement May 2014.</comments>
<data>
<eng-data t="0." f="0." m="364." cg="178.2"/>
<eng-data t="0.018" f="267.857" m="362.704" cg="178.2"/>
<eng-data t="0.062" f="368.062" m="355.18" cg="178.2"/>
<eng-data t="0.242" f="420.092" m="317.031" cg="178.2"/>
<eng-data t="0.524" f="443.216" m="251.567" cg="178.2"/>
<eng-data t="0.902" f="452.851" m="160.487" cg="178.2"/>
<eng-data t="1.225" f="448.997" m="82.1578" cg="178.2"/>
<eng-data t="1.389" f="433.581" m="43.2366" cg="178.2"/>
<eng-data t="1.502" f="452.851" m="16.3018" cg="178.2"/>
<eng-data t="1.53" f="420.092" m="9.72927" cg="178.2"/>
<eng-data t="1.542" f="356.5" m="7.22337" cg="178.2"/>
<eng-data t="1.599" f="67.446" m="0.725442" cg="178.2"/>
<eng-data t="1.618" f="28.905" m="0.233176" cg="178.2"/>
<eng-data t="1.648" f="0." m="0." cg="178.2"/>
</data>
</engine>
<engine mfg="Aerotech" code="J460T" Type="reloadable" dia="54." len="241."
initWt="832.9" propWt="390.2" delays="6,10,14" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="427.721" peakThrust="582.91" throatDia="0."
exitDia="0." Itot="812.671" burn-time="1.9" massFrac="46.85" Isp="212.38"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="390.2" cg="120.5"/>
<eng-data t="0." f="582.91" m="390.2" cg="120.5"/>
<eng-data t="0.1" f="515.43" m="363.832" cg="120.5"/>
<eng-data t="0.2" f="510.85" m="339.194" cg="120.5"/>
<eng-data t="0.6" f="506.36" m="241.512" cg="120.5"/>
<eng-data t="0.9" f="492.93" m="169.541" cg="120.5"/>
<eng-data t="1.3" f="448.09" m="79.176" cg="120.5"/>
<eng-data t="1.5" f="412.24" m="37.8676" cg="120.5"/>
<eng-data t="1.6" f="336.05" m="19.9032" cg="120.5"/>
<eng-data t="1.7" f="179.25" m="7.53228" cg="120.5"/>
<eng-data t="1.8" f="67.25" m="1.61449" cg="120.5"/>
<eng-data t="1.9" f="0." m="0." cg="120.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="J500G" Type="reloadable" dia="38." len="335.41"
initWt="654." propWt="362.6" delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="498.389" peakThrust="787.971" throatDia="0." exitDia="0."
Itot="722.664" burn-time="1.45" massFrac="55.44" Isp="203.23" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Taken from Aerotech curves, not cert docs.
Jim Yehle 15 Nov 07</comments>
<data>
<eng-data t="0." f="0." m="362.6" cg="167.703"/>
<eng-data t="0.0134378" f="40.2458" m="362.464" cg="167.703"/>
<eng-data t="0.0335946" f="724.425" m="358.597" cg="167.703"/>
<eng-data t="0.0403135" f="781.616" m="356.059" cg="167.703"/>
<eng-data t="0.0604703" f="787.971" m="348.122" cg="167.703"/>
<eng-data t="0.0895857" f="711.716" m="337.167" cg="167.703"/>
<eng-data t="0.134378" f="686.297" m="321.457" cg="167.703"/>
<eng-data t="0.394177" f="637.578" m="235.17" cg="167.703"/>
<eng-data t="0.575588" f="588.86" m="179.353" cg="167.703"/>
<eng-data t="0.606943" f="622.751" m="169.822" cg="167.703"/>
<eng-data t="0.633819" f="620.633" m="161.438" cg="167.703"/>
<eng-data t="1.20045" f="360.094" m="22.0236" cg="167.703"/>
<eng-data t="1.24076" f="345.267" m="14.8898" cg="167.703"/>
<eng-data t="1.31019" f="182.165" m="5.70288" cg="167.703"/>
<eng-data t="1.38186" f="65.6642" m="1.24691" cg="167.703"/>
<eng-data t="1.43337" f="23.3002" m="0.0972067" cg="167.703"/>
<eng-data t="1.45" f="0." m="0." cg="167.703"/>
</data>
</engine>
<engine mfg="Aerotech" code="J520W" Type="reloadable" dia="38." len="502.1"
initWt="757.4" propWt="381." delays="13" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="464.687" peakThrust="892.23" throatDia="0." exitDia="0."
Itot="686.808" burn-time="1.48" massFrac="50.3" Isp="183.82" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Certified 8/26/2018 TMT</comments>
<data>
<eng-data t="0." f="0." m="381." cg="251.05"/>
<eng-data t="0.024" f="15.517" m="380.897" cg="251.05"/>
<eng-data t="0.034" f="131.895" m="380.488" cg="251.05"/>
<eng-data t="0.039" f="318.099" m="379.864" cg="251.05"/>
<eng-data t="0.046" f="659.474" m="377.966" cg="251.05"/>
<eng-data t="0.049" f="752.577" m="376.791" cg="251.05"/>
<eng-data t="0.051" f="799.128" m="375.93" cg="251.05"/>
<eng-data t="0.066" f="756.456" m="369.458" cg="251.05"/>
<eng-data t="0.071" f="791.369" m="367.311" cg="251.05"/>
<eng-data t="0.098" f="892.23" m="354.703" cg="251.05"/>
<eng-data t="0.137" f="861.196" m="335.735" cg="251.05"/>
<eng-data t="0.168" f="837.921" m="321.125" cg="251.05"/>
<eng-data t="0.195" f="810.766" m="308.778" cg="251.05"/>
<eng-data t="0.234" f="783.611" m="291.531" cg="251.05"/>
<eng-data t="0.4" f="706.026" m="222.943" cg="251.05"/>
<eng-data t="0.598" f="593.527" m="151.573" cg="251.05"/>
<eng-data t="0.798" f="477.149" m="92.178" cg="251.05"/>
<eng-data t="0.998" f="376.288" m="44.8344" cg="251.05"/>
<eng-data t="1.056" f="333.617" m="33.4139" cg="251.05"/>
<eng-data t="1.102" f="298.703" m="25.3461" cg="251.05"/>
<eng-data t="1.198" f="170.688" m="12.8474" cg="251.05"/>
<eng-data t="1.302" f="100.861" m="5.01412" cg="251.05"/>
<eng-data t="1.4" f="46.551" m="1.00712" cg="251.05"/>
<eng-data t="1.478" f="0." m="0." cg="251.05"/>
</data>
</engine>
<engine mfg="Aerotech" code="J540R" Type="reloadable" dia="54." len="314."
initWt="1100." propWt="621." delays="6,10,14,1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="510.979" peakThrust="666.92" throatDia="0."
exitDia="0." Itot="1149.7" burn-time="2.25" massFrac="56.45" Isp="188.79"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="621." cg="157."/>
<eng-data t="0.04" f="498.76" m="615.612" cg="157."/>
<eng-data t="0.13" f="639.62" m="587.942" cg="157."/>
<eng-data t="0.22" f="649.32" m="556.613" cg="157."/>
<eng-data t="0.31" f="657.97" m="524.838" cg="157."/>
<eng-data t="0.4" f="664.02" m="492.705" cg="157."/>
<eng-data t="0.49" f="666.92" m="460.355" cg="157."/>
<eng-data t="0.58" f="663.7" m="428.012" cg="157."/>
<eng-data t="0.68" f="658.4" m="392.306" cg="157."/>
<eng-data t="0.77" f="651.23" m="360.474" cg="157."/>
<eng-data t="0.85" f="638.51" m="332.609" cg="157."/>
<eng-data t="0.94" f="626.4" m="301.863" cg="157."/>
<eng-data t="1.03" f="612.56" m="271.749" cg="157."/>
<eng-data t="1.13" f="590.09" m="239.269" cg="157."/>
<eng-data t="1.22" f="562.39" m="211.257" cg="157."/>
<eng-data t="1.31" f="536.88" m="184.537" cg="157."/>
<eng-data t="1.4" f="511.61" m="159.053" cg="157."/>
<eng-data t="1.49" f="490.35" m="134.699" cg="157."/>
<eng-data t="1.58" f="468.98" m="111.381" cg="157."/>
<eng-data t="1.67" f="451.34" m="89.0114" cg="157."/>
<eng-data t="1.76" f="430.18" m="67.5849" cg="157."/>
<eng-data t="1.85" f="414.55" m="47.0527" cg="157."/>
<eng-data t="1.94" f="398.12" m="27.2997" cg="157."/>
<eng-data t="2.03" f="305.88" m="10.1881" cg="157."/>
<eng-data t="2.12" f="55.54" m="1.40334" cg="157."/>
<eng-data t="2.21" f="1.52" m="0.0164202" cg="157."/>
<eng-data t="2.25" f="0." m="0." cg="157."/>
</data>
</engine>
<engine mfg="Aerotech" code="J570W" Type="reloadable" dia="38." len="479."
initWt="886.144" propWt="547.904" delays="6,10,14" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="503.817" peakThrust="1149.8" throatDia="0."
exitDia="0." Itot="1033.83" burn-time="2.05" massFrac="61.83" Isp="192.41"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="547.904" cg="239.5"/>
<eng-data t="0.039" f="1149.8" m="536.021" cg="239.5"/>
<eng-data t="0.119" f="1042.85" m="489.54" cg="239.5"/>
<eng-data t="0.199" f="960.891" m="447.062" cg="239.5"/>
<eng-data t="0.279" f="900.02" m="407.613" cg="239.5"/>
<eng-data t="0.36" f="837.772" m="370.313" cg="239.5"/>
<eng-data t="0.441" f="792.834" m="335.314" cg="239.5"/>
<eng-data t="0.521" f="735.51" m="302.915" cg="239.5"/>
<eng-data t="0.602" f="685.857" m="272.407" cg="239.5"/>
<eng-data t="0.682" f="649.599" m="244.096" cg="239.5"/>
<eng-data t="0.762" f="608.757" m="217.421" cg="239.5"/>
<eng-data t="0.844" f="597.35" m="191.213" cg="239.5"/>
<eng-data t="0.924" f="568.934" m="166.489" cg="239.5"/>
<eng-data t="1.004" f="548.552" m="142.8" cg="239.5"/>
<eng-data t="1.084" f="505.08" m="120.464" cg="239.5"/>
<eng-data t="1.165" f="484.626" m="99.2209" cg="239.5"/>
<eng-data t="1.246" f="452.328" m="79.1102" cg="239.5"/>
<eng-data t="1.326" f="362.439" m="61.8381" cg="239.5"/>
<eng-data t="1.406" f="297.973" m="47.838" cg="239.5"/>
<eng-data t="1.487" f="262.381" m="35.8106" cg="239.5"/>
<eng-data t="1.568" f="195.696" m="25.9785" cg="239.5"/>
<eng-data t="1.648" f="156.733" m="18.5074" cg="239.5"/>
<eng-data t="1.729" f="124.649" m="12.4678" cg="239.5"/>
<eng-data t="1.809" f="113.749" m="7.41405" cg="239.5"/>
<eng-data t="1.89" f="69.812" m="3.47411" cg="239.5"/>
<eng-data t="1.971" f="46.023" m="0.987834" cg="239.5"/>
<eng-data t="2.052" f="0." m="0." cg="239.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="J800T" Type="reloadable" dia="54." len="326."
initWt="1133.9" propWt="595.3" delays="6,10,14,18" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="790.502" peakThrust="1255.67" throatDia="0."
exitDia="0." Itot="1264.8" burn-time="1.6" massFrac="52.5" Isp="216.65" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="595.3" cg="163."/>
<eng-data t="0." f="1255.67" m="595.3" cg="163."/>
<eng-data t="0.1" f="1102.7" m="539.8" cg="163."/>
<eng-data t="0.2" f="1067.83" m="488.72" cg="163."/>
<eng-data t="0.3" f="1045.99" m="438.975" cg="163."/>
<eng-data t="0.6" f="1002.4" m="294.359" cg="163."/>
<eng-data t="0.7" f="971.89" m="247.897" cg="163."/>
<eng-data t="0.8" f="937.02" m="202.974" cg="163."/>
<eng-data t="0.9" f="841.12" m="161.128" cg="163."/>
<eng-data t="1.3" f="588.38" m="26.5649" cg="163."/>
<eng-data t="1.4" f="217.91" m="7.5902" cg="163."/>
<eng-data t="1.5" f="52.31" m="1.23103" cg="163."/>
<eng-data t="1.6" f="0." m="0." cg="163."/>
</data>
</engine>
<engine mfg="Aerotech" code="J825R" Type="reloadable" dia="38." len="479." initWt="880."
propWt="530." delays="10" auto-calc-mass="1" auto-calc-cg="1" avgThrust="786.654"
peakThrust="1069.87" throatDia="0." exitDia="0." Itot="928.251" burn-time="1.18"
massFrac="60.23" Isp="178.59" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<comments>Aerotech J825R</comments>
<data>
<eng-data t="0." f="0." m="530." cg="239.5"/>
<eng-data t="0." f="11.504" m="530." cg="239.5"/>
<eng-data t="0.048913" f="1069.87" m="514.9" cg="239.5"/>
<eng-data t="0.100155" f="977.842" m="484.944" cg="239.5"/>
<eng-data t="0.118789" f="1035.36" m="474.235" cg="239.5"/>
<eng-data t="0.652174" f="897.314" m="179.942" cg="239.5"/>
<eng-data t="0.801242" f="839.794" m="106.017" cg="239.5"/>
<eng-data t="0.899068" f="782.274" m="60.7164" cg="239.5"/>
<eng-data t="0.999224" f="586.705" m="21.5734" cg="239.5"/>
<eng-data t="1.09938" f="103.536" m="1.83748" cg="239.5"/>
<eng-data t="1.14363" f="23.008" m="0.238892" cg="239.5"/>
<eng-data t="1.18" f="0." m="0." cg="239.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="J1299N" Type="reloadable" dia="54." len="230."
initWt="834." propWt="371.6" delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1253.93" peakThrust="1452." throatDia="0." exitDia="0." Itot="850.164"
burn-time="0.68" massFrac="44.56" Isp="233.3" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>AT 54-852
Greg Gardner - 09/15/06
</comments>
<data>
<eng-data t="0." f="0." m="371.6" cg="115."/>
<eng-data t="0.01" f="548." m="370.402" cg="115."/>
<eng-data t="0.02" f="1152." m="366.687" cg="115."/>
<eng-data t="0.03" f="1232." m="361.477" cg="115."/>
<eng-data t="0.04" f="1277." m="355.994" cg="115."/>
<eng-data t="0.05" f="1272." m="350.423" cg="115."/>
<eng-data t="0.06" f="1288." m="344.828" cg="115."/>
<eng-data t="0.07" f="1333." m="339.1" cg="115."/>
<eng-data t="0.08" f="1347." m="333.243" cg="115."/>
<eng-data t="0.09" f="1378." m="327.288" cg="115."/>
<eng-data t="0.1" f="1383." m="321.254" cg="115."/>
<eng-data t="0.12" f="1405." m="309.067" cg="115."/>
<eng-data t="0.14" f="1410." m="296.763" cg="115."/>
<eng-data t="0.16" f="1440." m="284.306" cg="115."/>
<eng-data t="0.18" f="1444." m="271.7" cg="115."/>
<eng-data t="0.2" f="1446." m="259.068" cg="115."/>
<eng-data t="0.25" f="1449." m="227.434" cg="115."/>
<eng-data t="0.3" f="1452." m="195.734" cg="115."/>
<eng-data t="0.35" f="1448." m="164.045" cg="115."/>
<eng-data t="0.4" f="1440." m="132.487" cg="115."/>
<eng-data t="0.45" f="1405." m="101.398" cg="115."/>
<eng-data t="0.5" f="1320." m="71.6215" cg="115."/>
<eng-data t="0.55" f="1248." m="43.5602" cg="115."/>
<eng-data t="0.57" f="1224." m="32.7552" cg="115."/>
<eng-data t="0.59" f="1210." m="22.1164" cg="115."/>
<eng-data t="0.6" f="1180." m="16.8932" cg="115."/>
<eng-data t="0.61" f="1188." m="11.718" cg="115."/>
<eng-data t="0.605" f="1195." m="14.322" cg="115."/>
<eng-data t="0.62" f="1188." m="6.51005" cg="115."/>
<eng-data t="0.63" f="510." m="2.79914" cg="115."/>
<eng-data t="0.64" f="220." m="1.20375" cg="115."/>
<eng-data t="0.65" f="96." m="0.513146" cg="115."/>
<eng-data t="0.66" f="46." m="0.202811" cg="115."/>
<eng-data t="0.67" f="26." m="0.0454576" cg="115."/>
<eng-data t="0.678" f="0." m="0." cg="115."/>
</data>
</engine>
<engine mfg="Aerotech" code="J1799N" Type="reloadable" dia="54." len="368."
initWt="1111." propWt="591." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1649.9" peakThrust="2114.01" throatDia="0." exitDia="0."
Itot="1075.74" burn-time="0.65" massFrac="53.2" Isp="185.61" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>This is the J1799N. It was a replacement for the J1999N.</comments>
<data>
<eng-data t="0." f="0." m="591." cg="184."/>
<eng-data t="0.004" f="665.031" m="590.269" cg="184."/>
<eng-data t="0.007" f="1338.87" m="588.618" cg="184."/>
<eng-data t="0.009" f="1625.14" m="586.989" cg="184."/>
<eng-data t="0.014" f="1497.42" m="582.701" cg="184."/>
<eng-data t="0.02" f="2021.52" m="576.901" cg="184."/>
<eng-data t="0.026" f="1572.29" m="570.978" cg="184."/>
<eng-data t="0.042" f="1796.9" m="556.17" cg="184."/>
<eng-data t="0.051" f="1730.84" m="547.448" cg="184."/>
<eng-data t="0.062" f="1849.76" m="536.629" cg="184."/>
<eng-data t="0.075" f="1788.1" m="523.638" cg="184."/>
<eng-data t="0.083" f="1898.2" m="515.537" cg="184."/>
<eng-data t="0.096" f="1832.14" m="502.216" cg="184."/>
<eng-data t="0.104" f="1911.41" m="493.989" cg="184."/>
<eng-data t="0.138" f="1955.45" m="457.874" cg="184."/>
<eng-data t="0.144" f="2114.01" m="451.167" cg="184."/>
<eng-data t="0.154" f="2008.31" m="439.843" cg="184."/>
<eng-data t="0.176" f="2008.31" m="415.569" cg="184."/>
<eng-data t="0.18" f="1964.26" m="411.204" cg="184."/>
<eng-data t="0.207" f="1973.07" m="382.002" cg="184."/>
<eng-data t="0.258" f="2025.92" m="325.978" cg="184."/>
<eng-data t="0.325" f="1977.48" m="252.297" cg="184."/>
<eng-data t="0.362" f="1937.84" m="212.503" cg="184."/>
<eng-data t="0.399" f="1951.05" m="172.977" cg="184."/>
<eng-data t="0.428" f="1933.43" m="142.033" cg="184."/>
<eng-data t="0.44" f="1858.56" m="129.533" cg="184."/>
<eng-data t="0.499" f="1695.61" m="71.9304" cg="184."/>
<eng-data t="0.527" f="1633.95" m="46.3212" cg="184."/>
<eng-data t="0.553" f="1523.85" m="23.7679" cg="184."/>
<eng-data t="0.564" f="1431.36" m="14.8383" cg="184."/>
<eng-data t="0.572" f="1114.26" m="9.24415" cg="184."/>
<eng-data t="0.581" f="665.031" m="4.84529" cg="184."/>
<eng-data t="0.587" f="409.589" m="3.07413" cg="184."/>
<eng-data t="0.595" f="220.209" m="1.69011" cg="184."/>
<eng-data t="0.604" f="96.892" m="0.90615" cg="184."/>
<eng-data t="0.615" f="26.425" m="0.533529" cg="184."/>
<eng-data t="0.633" f="39.638" m="0.206879" cg="184."/>
<eng-data t="0.652" f="0." m="0." cg="184."/>
</data>
</engine>
<engine mfg="Aerotech" code="J250FJ" Type="reloadable" dia="54." len="241."
initWt="920." propWt="511." delays="6,10,14,18" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="252.927" peakThrust="306.038" throatDia="0."
exitDia="0." Itot="707.183" burn-time="2.8" massFrac="55.54" Isp="141.12"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Aerotech J250FJ from TRA Cert Data</comments>
<data>
<eng-data t="0." f="0." m="511." cg="120.5"/>
<eng-data t="0.011" f="132.176" m="510.475" cg="120.5"/>
<eng-data t="0.021" f="263.335" m="509.046" cg="120.5"/>
<eng-data t="0.084" f="236.899" m="497.66" cg="120.5"/>
<eng-data t="0.168" f="252.151" m="482.818" cg="120.5"/>
<eng-data t="0.294" f="238.933" m="460.462" cg="120.5"/>
<eng-data t="0.494" f="261.301" m="424.316" cg="120.5"/>
<eng-data t="0.715" f="285.703" m="380.64" cg="120.5"/>
<eng-data t="0.993" f="295.87" m="322.227" cg="120.5"/>
<eng-data t="1.177" f="306.038" m="282.214" cg="120.5"/>
<eng-data t="1.267" f="305.021" m="262.344" cg="120.5"/>
<eng-data t="1.498" f="301.971" m="211.686" cg="120.5"/>
<eng-data t="1.64" f="292.82" m="181.171" cg="120.5"/>
<eng-data t="2.002" f="253.167" m="109.762" cg="120.5"/>
<eng-data t="2.344" f="224.699" m="50.716" cg="120.5"/>
<eng-data t="2.391" f="225.715" m="43.0676" cg="120.5"/>
<eng-data t="2.502" f="233.849" m="24.6375" cg="120.5"/>
<eng-data t="2.57" f="185.046" m="14.3461" cg="120.5"/>
<eng-data t="2.659" f="116.925" m="4.63621" cg="120.5"/>
<eng-data t="2.685" f="76.255" m="2.82155" cg="120.5"/>
<eng-data t="2.738" f="32.536" m="0.738367" cg="120.5"/>
<eng-data t="2.77" f="17.285" m="0.162369" cg="120.5"/>
<eng-data t="2.796" f="0." m="0." cg="120.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="J401FJ" Type="reloadable" dia="54." len="325."
initWt="912." propWt="511." delays="6,10,14,18" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="397.97" peakThrust="488.102" throatDia="0."
exitDia="0." Itot="1107.55" burn-time="2.78" massFrac="56.03" Isp="221.02"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Input by Tim Van Milligan using ThrustCurve Tracer by John Coker. Data from
Tripoli certification paperwork dated 25 November 2007.
</comments>
<data>
<eng-data t="0." f="0." m="511." cg="162.5"/>
<eng-data t="0.011" f="440.414" m="509.882" cg="162.5"/>
<eng-data t="0.022" f="488.102" m="507.526" cg="162.5"/>
<eng-data t="0.075" f="427.791" m="496.328" cg="162.5"/>
<eng-data t="0.116" f="422.18" m="488.289" cg="162.5"/>
<eng-data t="0.191" f="446.024" m="473.267" cg="162.5"/>
<eng-data t="0.277" f="453.037" m="455.431" cg="162.5"/>
<eng-data t="0.382" f="462.855" m="433.246" cg="162.5"/>
<eng-data t="0.513" f="468.466" m="405.101" cg="162.5"/>
<eng-data t="0.712" f="472.673" m="361.896" cg="162.5"/>
<eng-data t="0.775" f="471.271" m="348.177" cg="162.5"/>
<eng-data t="0.948" f="471.271" m="310.561" cg="162.5"/>
<eng-data t="1.06" f="472.673" m="286.172" cg="162.5"/>
<eng-data t="1.281" f="469.868" m="238.119" cg="162.5"/>
<eng-data t="1.431" f="462.855" m="205.844" cg="162.5"/>
<eng-data t="1.607" f="453.037" m="168.658" cg="162.5"/>
<eng-data t="1.858" f="426.388" m="117.736" cg="162.5"/>
<eng-data t="2.034" f="403.946" m="84.0237" cg="162.5"/>
<eng-data t="2.135" f="384.31" m="65.6577" cg="162.5"/>
<eng-data t="2.202" f="378.7" m="53.8645" cg="162.5"/>
<eng-data t="2.258" f="374.492" m="44.1343" cg="162.5"/>
<eng-data t="2.277" f="374.492" m="40.8514" cg="162.5"/>
<eng-data t="2.3" f="380.102" m="36.8477" cg="162.5"/>
<eng-data t="2.322" f="380.102" m="32.9895" cg="162.5"/>
<eng-data t="2.345" f="370.284" m="29.0081" cg="162.5"/>
<eng-data t="2.367" f="359.064" m="25.3065" cg="162.5"/>
<eng-data t="2.408" f="314.181" m="18.9388" cg="162.5"/>
<eng-data t="2.461" f="244.051" m="12.1136" cg="162.5"/>
<eng-data t="2.502" f="186.545" m="8.04087" cg="162.5"/>
<eng-data t="2.566" f="103.792" m="3.75431" cg="162.5"/>
<eng-data t="2.607" f="64.519" m="2.16238" cg="162.5"/>
<eng-data t="2.652" f="42.078" m="1.0558" cg="162.5"/>
<eng-data t="2.704" f="18.234" m="0.332304" cg="162.5"/>
<eng-data t="2.783" f="0." m="0." cg="162.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="J435WS" Type="single-use" dia="38." len="365.9"
initWt="624." propWt="352." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="433.528" peakThrust="694.661" throatDia="0." exitDia="0."
Itot="772.113" burn-time="1.78" massFrac="43.59" Isp="289.46" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>38mm DMS Certified 5-19-18</comments>
<data>
<eng-data t="0." f="0." m="272." cg="182.95"/>
<eng-data t="0.029" f="11.077" m="271.943" cg="182.95"/>
<eng-data t="0.03" f="41.142" m="271.934" cg="182.95"/>
<eng-data t="0.031" f="212.038" m="271.89" cg="182.95"/>
<eng-data t="0.036" f="528.512" m="271.237" cg="182.95"/>
<eng-data t="0.038" f="378.187" m="270.918" cg="182.95"/>
<eng-data t="0.048" f="694.661" m="269.028" cg="182.95"/>
<eng-data t="0.067" f="625.036" m="264.612" cg="182.95"/>
<eng-data t="0.071" f="688.331" m="263.686" cg="182.95"/>
<eng-data t="0.083" f="631.366" m="260.897" cg="182.95"/>
<eng-data t="0.095" f="651.937" m="258.184" cg="182.95"/>
<eng-data t="0.105" f="610.795" m="255.96" cg="182.95"/>
<eng-data t="0.116" f="629.784" m="253.557" cg="182.95"/>
<eng-data t="0.135" f="610.795" m="249.405" cg="182.95"/>
<eng-data t="0.145" f="621.872" m="247.234" cg="182.95"/>
<eng-data t="0.166" f="655.101" m="242.51" cg="182.95"/>
<eng-data t="0.171" f="625.036" m="241.383" cg="182.95"/>
<eng-data t="0.304" f="601.301" m="212.654" cg="182.95"/>
<eng-data t="0.399" f="564.906" m="193.139" cg="182.95"/>
<eng-data t="0.456" f="558.577" m="181.86" cg="182.95"/>
<eng-data t="0.504" f="547.5" m="172.508" cg="182.95"/>
<eng-data t="0.549" f="549.083" m="163.816" cg="182.95"/>
<eng-data t="0.613" f="538.006" m="151.561" cg="182.95"/>
<eng-data t="0.672" f="531.677" m="140.445" cg="182.95"/>
<eng-data t="0.701" f="525.347" m="135.046" cg="182.95"/>
<eng-data t="0.762" f="525.347" m="123.756" cg="182.95"/>
<eng-data t="0.803" f="515.853" m="116.237" cg="182.95"/>
<eng-data t="0.848" f="506.359" m="108.135" cg="182.95"/>
<eng-data t="0.903" f="501.612" m="98.3699" cg="182.95"/>
<eng-data t="0.983" f="492.117" m="84.367" cg="182.95"/>
<eng-data t="1.017" f="485.788" m="78.5106" cg="182.95"/>
<eng-data t="1.059" f="479.458" m="71.3698" cg="182.95"/>
<eng-data t="1.152" f="469.964" m="55.8173" cg="182.95"/>
<eng-data t="1.261" f="449.393" m="38.1663" cg="182.95"/>
<eng-data t="1.276" f="454.14" m="35.7791" cg="182.95"/>
<eng-data t="1.316" f="441.481" m="29.4689" cg="182.95"/>
<eng-data t="1.366" f="425.658" m="21.832" cg="182.95"/>
<eng-data t="1.387" f="401.922" m="18.7709" cg="182.95"/>
<eng-data t="1.409" f="343.374" m="15.8828" cg="182.95"/>
<eng-data t="1.42" f="375.022" m="14.4909" cg="182.95"/>
<eng-data t="1.428" f="340.21" m="13.483" cg="182.95"/>
<eng-data t="1.435" f="229.444" m="12.7806" cg="182.95"/>
<eng-data t="1.451" f="242.103" m="11.4517" cg="182.95"/>
<eng-data t="1.499" f="212.038" m="7.61208" cg="182.95"/>
<eng-data t="1.508" f="188.302" m="6.97743" cg="182.95"/>
<eng-data t="1.527" f="215.202" m="5.62704" cg="182.95"/>
<eng-data t="1.532" f="118.678" m="5.333" cg="182.95"/>
<eng-data t="1.544" f="63.295" m="4.94836" cg="182.95"/>
<eng-data t="1.558" f="132.919" m="4.46451" cg="182.95"/>
<eng-data t="1.575" f="87.03" m="3.8059" cg="182.95"/>
<eng-data t="1.587" f="125.007" m="3.35772" cg="182.95"/>
<eng-data t="1.601" f="83.866" m="2.84265" cg="182.95"/>
<eng-data t="1.618" f="115.513" m="2.24563" cg="182.95"/>
<eng-data t="1.632" f="72.789" m="1.78128" cg="182.95"/>
<eng-data t="1.648" f="87.03" m="1.33087" cg="182.95"/>
<eng-data t="1.667" f="47.471" m="0.880746" cg="182.95"/>
<eng-data t="1.686" f="45.889" m="0.568302" cg="182.95"/>
<eng-data t="1.717" f="18.988" m="0.214051" cg="182.95"/>
<eng-data t="1.781" f="0." m="0." cg="182.95"/>
</data>
</engine>
<engine mfg="Aerotech" code="J510WL" Type="reloadable" dia="38." len="584."
initWt="1080." propWt="662." delays="14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="472.2" peakThrust="1055.9" throatDia="0." exitDia="0." Itot="1180.5"
burn-time="2.5" massFrac="61.3" Isp="181.84" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="662." cg="292."/>
<eng-data t="0.032" f="1055.9" m="652.526" cg="292."/>
<eng-data t="0.11" f="865.54" m="610.503" cg="292."/>
<eng-data t="0.161" f="829.933" m="586.258" cg="292."/>
<eng-data t="0.267" f="794.325" m="537.983" cg="292."/>
<eng-data t="0.351" f="780.63" m="500.889" cg="292."/>
<eng-data t="0.512" f="705.306" m="433.809" cg="292."/>
<eng-data t="0.682" f="654.633" m="368.986" cg="292."/>
<eng-data t="1.318" f="624.504" m="140.88" cg="292."/>
<eng-data t="1.461" f="475.225" m="96.786" cg="292."/>
<eng-data t="1.623" f="345.121" m="59.5233" cg="292."/>
<eng-data t="1.934" f="153.387" m="16.0528" cg="292."/>
<eng-data t="2.039" f="115.04" m="8.15004" cg="292."/>
<eng-data t="2.177" f="41.086" m="2.10893" cg="292."/>
<eng-data t="2.317" f="5.478" m="0.281083" cg="292."/>
<eng-data t="2.5" f="0." m="0." cg="292."/>
</data>
</engine>
<engine mfg="Aerotech" code="J575FJ" Type="reloadable" dia="38." len="478.79"
initWt="914.24" propWt="576." delays="6,10,14" auto-calc-mass="1"
auto-calc-cg="0" avgThrust="597.435" peakThrust="884.242" throatDia="0."
exitDia="0." Itot="800.563" burn-time="1.34" massFrac="63." Isp="141.73"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="576." cg="239.4"/>
<eng-data t="0.0156556" f="656.682" m="572.302" cg="239.4"/>
<eng-data t="0.0195695" f="840.689" m="570.193" cg="239.4"/>
<eng-data t="0.0550206" f="878.839" m="548.263" cg="239.4"/>
<eng-data t="0.090784" f="880.64" m="525.626" cg="239.4"/>
<eng-data t="0.154058" f="882.441" m="485.494" cg="239.4"/>
<eng-data t="0.209078" f="884.242" m="450.525" cg="239.4"/>
<eng-data t="0.261348" f="880.64" m="417.339" cg="239.4"/>
<eng-data t="0.341128" f="878.839" m="366.841" cg="239.4"/>
<eng-data t="0.390646" f="873.436" m="335.625" cg="239.4"/>
<eng-data t="0.451169" f="862.631" m="297.826" cg="239.4"/>
<eng-data t="0.525447" f="821.21" m="252.832" cg="239.4"/>
<eng-data t="0.599725" f="783.391" m="209.955" cg="239.4"/>
<eng-data t="0.797799" f="669.935" m="106.396" cg="239.4"/>
<eng-data t="0.836314" f="639.319" m="88.2555" cg="239.4"/>
<eng-data t="1.00138" f="340.37" m="30.0811" cg="239.4"/>
<eng-data t="1.0729" f="205.303" m="16.0401" cg="239.4"/>
<eng-data t="1.14993" f="108.054" m="7.35668" cg="239.4"/>
<eng-data t="1.21045" f="72.036" m="3.43561" cg="239.4"/>
<eng-data t="1.28473" f="32.4162" m="0.644517" cg="239.4"/>
<eng-data t="1.34" f="0." m="0." cg="239.4"/>
</data>
</engine>
<engine mfg="Aerotech" code="K185W" Type="reloadable" dia="54." len="437."
initWt="1434.05" propWt="827.008" delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="178.688" peakThrust="339.677" throatDia="0."
exitDia="0." Itot="1378.58" burn-time="7.71" massFrac="57.67" Isp="169.98"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>AeroTech K185W
Copyright Tripoli Motor Testing 1998 (www.tripoli.org)
provided by ThrustCurve.org (www.thrustcurve.org)
</comments>
<data>
<eng-data t="0." f="0." m="827.008" cg="218.5"/>
<eng-data t="0.15" f="279.128" m="814.449" cg="218.5"/>
<eng-data t="0.452" f="308.22" m="761.245" cg="218.5"/>
<eng-data t="0.754" f="328.435" m="703.573" cg="218.5"/>
<eng-data t="1.056" f="338.929" m="643.12" cg="218.5"/>
<eng-data t="1.359" f="339.677" m="581.445" cg="218.5"/>
<eng-data t="1.663" f="333.166" m="520.093" cg="218.5"/>
<eng-data t="1.965" f="321.891" m="460.754" cg="218.5"/>
<eng-data t="2.267" f="309.687" m="403.543" cg="218.5"/>
<eng-data t="2.57" f="293.26" m="348.744" cg="218.5"/>
<eng-data t="2.873" f="271.536" m="297.413" cg="218.5"/>
<eng-data t="3.175" f="247.174" m="250.426" cg="218.5"/>
<eng-data t="3.477" f="216.883" m="208.389" cg="218.5"/>
<eng-data t="3.78" f="186.951" m="171.687" cg="218.5"/>
<eng-data t="4.083" f="161.096" m="140.055" cg="218.5"/>
<eng-data t="4.385" f="138.113" m="112.951" cg="218.5"/>
<eng-data t="4.688" f="117.749" m="89.6972" cg="218.5"/>
<eng-data t="4.991" f="99.372" m="69.9643" cg="218.5"/>
<eng-data t="5.294" f="82.759" m="53.4113" cg="218.5"/>
<eng-data t="5.596" f="68.426" m="39.7163" cg="218.5"/>
<eng-data t="5.898" f="55.126" m="28.5244" cg="218.5"/>
<eng-data t="6.201" f="44.162" m="19.5006" cg="218.5"/>
<eng-data t="6.504" f="34.209" m="12.3779" cg="218.5"/>
<eng-data t="6.806" f="25.064" m="7.00866" cg="218.5"/>
<eng-data t="7.108" f="16.88" m="3.20917" cg="218.5"/>
<eng-data t="7.411" f="9.2" m="0.838899" cg="218.5"/>
<eng-data t="7.715" f="0." m="0." cg="218.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="K250W" Type="single-use" dia="54." len="673."
initWt="2211.33" propWt="1529.02" delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="249.904" peakThrust="418.669" throatDia="0."
exitDia="0." Itot="2553.02" burn-time="10.22" massFrac="69.14" Isp="170.26"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>AeroTech K250W
Copyright Tripoli Motor Testing 1998 (www.tripoli.org)
provided by ThrustCurve.org (www.thrustcurve.org)
</comments>
<data>
<eng-data t="0." f="0." m="1529.02" cg="336.5"/>
<eng-data t="0.199" f="365.33" m="1507.25" cg="336.5"/>
<eng-data t="0.599" f="403.324" m="1415.18" cg="336.5"/>
<eng-data t="0.999" f="418.669" m="1316.72" cg="336.5"/>
<eng-data t="1.4" f="409.813" m="1217.23" cg="336.5"/>
<eng-data t="1.801" f="408.949" m="1118.92" cg="336.5"/>
<eng-data t="2.201" f="412.146" m="1020.57" cg="336.5"/>
<eng-data t="2.602" f="411.952" m="921.607" cg="336.5"/>
<eng-data t="3.003" f="409.488" m="822.968" cg="336.5"/>
<eng-data t="3.403" f="393.214" m="726.819" cg="336.5"/>
<eng-data t="3.804" f="373.599" m="634.739" cg="336.5"/>
<eng-data t="4.205" f="348.913" m="547.98" cg="336.5"/>
<eng-data t="4.605" f="328.463" m="466.842" cg="336.5"/>
<eng-data t="5.006" f="307.163" m="390.516" cg="336.5"/>
<eng-data t="5.407" f="281.467" m="319.833" cg="336.5"/>
<eng-data t="5.807" f="249.011" m="256.291" cg="336.5"/>
<eng-data t="6.208" f="217.159" m="200.313" cg="336.5"/>
<eng-data t="6.609" f="185.908" m="151.913" cg="336.5"/>
<eng-data t="7.009" f="149.19" m="111.774" cg="336.5"/>
<eng-data t="7.41" f="119.808" m="79.4727" cg="336.5"/>
<eng-data t="7.811" f="92.096" m="54.0271" cg="336.5"/>
<eng-data t="8.211" f="69.726" m="34.6438" cg="336.5"/>
<eng-data t="8.613" f="52.613" m="19.9166" cg="336.5"/>
<eng-data t="9.014" f="35.876" m="9.29075" cg="336.5"/>
<eng-data t="9.414" f="16.727" m="2.98989" cg="336.5"/>
<eng-data t="9.815" f="4.086" m="0.49065" cg="336.5"/>
<eng-data t="10.216" f="0." m="0." cg="336.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="K270W" Type="reloadable" dia="54." len="579."
initWt="2100." propWt="1188." delays="6,10,14,18" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="247.914" peakThrust="425.727" throatDia="0."
exitDia="0." Itot="2154.87" burn-time="8.69" massFrac="56.57" Isp="184.96"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>AeroTech K270W-P Moon Burner from TRA Certification Data
K270W 54 P 1.188 2.1 AT
Converted from Mark Koelsch submitted RASP file dated Mar 23, 2008.</comments>
<data>
<eng-data t="0." f="0." m="1188." cg="28.95"/>
<eng-data t="0.046" f="177.061" m="1185.75" cg="28.95"/>
<eng-data t="0.062" f="177.061" m="1184.19" cg="28.95"/>
<eng-data t="0.092" f="292.932" m="1180.31" cg="28.95"/>
<eng-data t="0.154" f="425.727" m="1168.02" cg="28.95"/>
<eng-data t="0.277" f="414.01" m="1139.55" cg="28.95"/>
<eng-data t="0.446" f="389.273" m="1102.13" cg="28.95"/>
<eng-data t="0.585" f="377.556" m="1072.75" cg="28.95"/>
<eng-data t="0.738" f="381.462" m="1040.74" cg="28.95"/>
<eng-data t="1." f="372.349" m="986.296" cg="28.95"/>
<eng-data t="1.154" f="377.556" m="954.462" cg="28.95"/>
<eng-data t="1.231" f="376.254" m="938.462" cg="28.95"/>
<eng-data t="1.308" f="378.858" m="922.434" cg="28.95"/>
<eng-data t="1.4" f="395.783" m="902.789" cg="28.95"/>
<eng-data t="1.569" f="380.16" m="866.642" cg="28.95"/>
<eng-data t="1.615" f="399.689" m="856.753" cg="28.95"/>
<eng-data t="1.846" f="381.462" m="807.012" cg="28.95"/>
<eng-data t="2.369" f="381.462" m="697.023" cg="28.95"/>
<eng-data t="2.415" f="368.443" m="687.515" cg="28.95"/>
<eng-data t="2.554" f="381.462" m="658.781" cg="28.95"/>
<eng-data t="3.015" f="360.631" m="564.478" cg="28.95"/>
<eng-data t="3.354" f="350.216" m="498.052" cg="28.95"/>
<eng-data t="3.723" f="328.083" m="429.058" cg="28.95"/>
<eng-data t="4." f="300.743" m="381.043" cg="28.95"/>
<eng-data t="4.6" f="273.403" m="286.083" cg="28.95"/>
<eng-data t="5.262" f="225.232" m="195.091" cg="28.95"/>
<eng-data t="5.677" f="175.759" m="149.219" cg="28.95"/>
<eng-data t="6." f="144.513" m="120.703" cg="28.95"/>
<eng-data t="6.538" f="124.984" m="80.7357" cg="28.95"/>
<eng-data t="7.015" f="89.832" m="52.4901" cg="28.95"/>
<eng-data t="8." f="66.398" m="10.0706" cg="28.95"/>
<eng-data t="8.323" f="22.133" m="2.18808" cg="28.95"/>
<eng-data t="8.508" f="10.415" m="0.528254" cg="28.95"/>
<eng-data t="8.692" f="0." m="0." cg="28.95"/>
<eng-data t="8.692" f="5.208" m="0." cg="28.95"/>
</data>
</engine>
<engine mfg="Aerotech" code="K458W" Type="reloadable" dia="98." len="275."
initWt="3106.2" propWt="1330." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="400.002" peakThrust="596.79" throatDia="0." exitDia="0."
Itot="2560.01" burn-time="6.4" massFrac="42.82" Isp="196.28" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="1330." cg="137.5"/>
<eng-data t="0." f="417.98" m="1330." cg="137.5"/>
<eng-data t="0.2" f="358.91" m="1289.64" cg="137.5"/>
<eng-data t="0.4" f="379.77" m="1251.26" cg="137.5"/>
<eng-data t="0.7" f="404.81" m="1190.12" cg="137.5"/>
<eng-data t="1.2" f="467.44" m="1076.83" cg="137.5"/>
<eng-data t="1.9" f="538.39" m="893.935" cg="137.5"/>
<eng-data t="2.6" f="596.79" m="687.52" cg="137.5"/>
<eng-data t="3.6" f="538.39" m="392.641" cg="137.5"/>
<eng-data t="3.7" f="500.8" m="365.646" cg="137.5"/>
<eng-data t="4.6" f="313.01" m="175.387" cg="137.5"/>
<eng-data t="4.8" f="287.96" m="144.165" cg="137.5"/>
<eng-data t="5.8" f="166.89" m="26.0112" cg="137.5"/>
<eng-data t="6.4" f="0." m="0." cg="137.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="K480W" Type="reloadable" dia="54." len="568."
initWt="2059." propWt="1232." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="478.075" peakThrust="915.996" throatDia="0." exitDia="0."
Itot="2294.76" burn-time="4.8" massFrac="59.83" Isp="189.94" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>From AT Instruction Sheet by C. Kobel 3/12/10</comments>
<data>
<eng-data t="0." f="0." m="1232." cg="284."/>
<eng-data t="0.03" f="535.684" m="1227.69" cg="284."/>
<eng-data t="0.045" f="860.341" m="1222.06" cg="284."/>
<eng-data t="0.057" f="915.996" m="1216.34" cg="284."/>
<eng-data t="0.098" f="830.194" m="1197.12" cg="284."/>
<eng-data t="0.159" f="832.513" m="1169.9" cg="284."/>
<eng-data t="0.246" f="795.409" m="1131.88" cg="284."/>
<eng-data t="0.307" f="811.642" m="1105.56" cg="284."/>
<eng-data t="0.398" f="793.09" m="1066.36" cg="284."/>
<eng-data t="0.492" f="809.323" m="1025.93" cg="284."/>
<eng-data t="0.557" f="823.237" m="997.445" cg="284."/>
<eng-data t="0.621" f="811.642" m="969.358" cg="284."/>
<eng-data t="0.689" f="779.176" m="940.319" cg="284."/>
<eng-data t="0.735" f="795.409" m="920.876" cg="284."/>
<eng-data t="0.845" f="767.581" m="874.724" cg="284."/>
<eng-data t="0.989" f="718.883" m="817.265" cg="284."/>
<eng-data t="1.091" f="707.288" m="778.215" cg="284."/>
<eng-data t="1.25" f="684.098" m="718.829" cg="284."/>
<eng-data t="1.307" f="667.865" m="698.142" cg="284."/>
<eng-data t="1.5" f="653.952" m="629.661" cg="284."/>
<eng-data t="1.606" f="656.271" m="592.379" cg="284."/>
<eng-data t="1.742" f="651.633" m="544.631" cg="284."/>
<eng-data t="1.909" f="628.443" m="487.246" cg="284."/>
<eng-data t="2." f="605.253" m="457.11" cg="284."/>
<eng-data t="2.25" f="586.701" m="377.119" cg="284."/>
<eng-data t="2.5" f="565.83" m="299.773" cg="284."/>
<eng-data t="2.75" f="547.279" m="225.073" cg="284."/>
<eng-data t="2.886" f="544.96" m="185.198" cg="284."/>
<eng-data t="3." f="524.089" m="152.483" cg="284."/>
<eng-data t="3.064" f="491.623" m="135.033" cg="284."/>
<eng-data t="3.144" f="417.416" m="115.511" cg="284."/>
<eng-data t="3.25" f="394.226" m="92.4166" cg="284."/>
<eng-data t="3.292" f="338.571" m="84.1547" cg="284."/>
<eng-data t="3.451" f="271.32" m="58.1236" cg="284."/>
<eng-data t="3.5" f="231.898" m="51.5046" cg="284."/>
<eng-data t="3.625" f="178.561" m="37.7318" cg="284."/>
<eng-data t="3.7" f="143.777" m="31.2422" cg="284."/>
<eng-data t="3.871" f="132.182" m="18.5749" cg="284."/>
<eng-data t="4." f="88.121" m="10.9461" cg="284."/>
<eng-data t="4.133" f="41.742" m="6.30973" cg="284."/>
<eng-data t="4.246" f="23.19" m="4.34012" cg="284."/>
<eng-data t="4.5" f="18.552" m="1.49402" cg="284."/>
<eng-data t="4.8" f="0." m="0." cg="284."/>
</data>
</engine>
<engine mfg="Aerotech" code="K535W" Type="single-use" dia="54." len="358.1"
initWt="1264." propWt="745." delays="14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="483.947" peakThrust="642.221" throatDia="0." exitDia="0."
Itot="1428.61" burn-time="2.95" massFrac="58.94" Isp="195.54" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>revised per AT post on TRF 5/19/14</comments>
<data>
<eng-data t="0." f="0." m="745." cg="179.05"/>
<eng-data t="0.015" f="467.288" m="743.172" cg="179.05"/>
<eng-data t="0.063" f="642.221" m="729.286" cg="179.05"/>
<eng-data t="0.104" f="613.465" m="715.862" cg="179.05"/>
<eng-data t="0.23" f="627.843" m="675.081" cg="179.05"/>
<eng-data t="0.419" f="620.654" m="613.554" cg="179.05"/>
<eng-data t="0.883" f="623.05" m="463.085" cg="179.05"/>
<eng-data t="1.335" f="599.087" m="319.049" cg="179.05"/>
<eng-data t="1.646" f="555.953" m="225.386" cg="179.05"/>
<eng-data t="1.843" f="500.837" m="171.102" cg="179.05"/>
<eng-data t="2.017" f="450.513" m="127.94" cg="179.05"/>
<eng-data t="2.258" f="404.983" m="74.1818" cg="179.05"/>
<eng-data t="2.488" f="366.641" m="27.9068" cg="179.05"/>
<eng-data t="2.6" f="230.049" m="10.4815" cg="179.05"/>
<eng-data t="2.611" f="172.537" m="9.32684" cg="179.05"/>
<eng-data t="2.648" f="124.61" m="6.46012" cg="179.05"/>
<eng-data t="2.696" f="81.476" m="3.88081" cg="179.05"/>
<eng-data t="2.789" f="40.738" m="0.917236" cg="179.05"/>
<eng-data t="2.837" f="9.585" m="0.28741" cg="179.05"/>
<eng-data t="2.952" f="0." m="0." cg="179.05"/>
</data>
</engine>
<engine mfg="Aerotech" code="K540M" Type="reloadable" dia="54." len="401."
initWt="1275." propWt="876.7" delays="14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="484.267" peakThrust="855.514" throatDia="0." exitDia="0."
Itot="1592.75" burn-time="3.29" massFrac="68.76" Isp="185.26" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>AT K540 Metalstorm 54-1706</comments>
<data>
<eng-data t="0." f="0." m="876.7" cg="200.5"/>
<eng-data t="0.013" f="625.709" m="874.461" cg="200.5"/>
<eng-data t="0.014" f="791.806" m="874.071" cg="200.5"/>
<eng-data t="0.03" f="855.514" m="866.817" cg="200.5"/>
<eng-data t="0.073" f="764.502" m="847.646" cg="200.5"/>
<eng-data t="0.146" f="718.996" m="817.841" cg="200.5"/>
<eng-data t="0.33" f="712.17" m="745.367" cg="200.5"/>
<eng-data t="0.394" f="734.923" m="719.879" cg="200.5"/>
<eng-data t="0.622" f="705.344" m="629.503" cg="200.5"/>
<eng-data t="0.866" f="678.041" m="536.605" cg="200.5"/>
<eng-data t="1.059" f="655.288" m="465.784" cg="200.5"/>
<eng-data t="1.406" f="648.462" m="341.276" cg="200.5"/>
<eng-data t="1.445" f="596.13" m="327.917" cg="200.5"/>
<eng-data t="1.544" f="605.231" m="295.184" cg="200.5"/>
<eng-data t="1.668" f="582.478" m="254.652" cg="200.5"/>
<eng-data t="1.689" f="625.709" m="247.669" cg="200.5"/>
<eng-data t="1.741" f="566.551" m="230.606" cg="200.5"/>
<eng-data t="2.032" f="498.292" m="145.326" cg="200.5"/>
<eng-data t="2.088" f="480.089" m="130.247" cg="200.5"/>
<eng-data t="2.118" f="511.943" m="122.056" cg="200.5"/>
<eng-data t="2.174" f="436.858" m="107.433" cg="200.5"/>
<eng-data t="2.324" f="395.903" m="73.0549" cg="200.5"/>
<eng-data t="2.435" f="357.223" m="50.0477" cg="200.5"/>
<eng-data t="2.525" f="304.891" m="33.6475" cg="200.5"/>
<eng-data t="2.542" f="329.919" m="30.6775" cg="200.5"/>
<eng-data t="2.65" f="175.198" m="15.6638" cg="200.5"/>
<eng-data t="2.774" f="88.737" m="6.65652" cg="200.5"/>
<eng-data t="2.89" f="36.405" m="2.66137" cg="200.5"/>
<eng-data t="3.006" f="13.652" m="1.0633" cg="200.5"/>
<eng-data t="3.289" f="0." m="0." cg="200.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="K550W" Type="reloadable" dia="54." len="410."
initWt="1515.1" propWt="880.4" delays="6,10,14,18" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="455.561" peakThrust="853.13" throatDia="0."
exitDia="0." Itot="1594.46" burn-time="3.5" massFrac="58.11" Isp="184.68"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="880.4" cg="205."/>
<eng-data t="0." f="628.15" m="880.4" cg="205."/>
<eng-data t="0.1" f="853.13" m="839.505" cg="205."/>
<eng-data t="0.2" f="695.98" m="796.737" cg="205."/>
<eng-data t="0.3" f="628.64" m="760.167" cg="205."/>
<eng-data t="0.7" f="606.17" m="623.804" cg="205."/>
<eng-data t="1.2" f="606.17" m="456.452" cg="205."/>
<eng-data t="1.6" f="588.2" m="324.555" cg="205."/>
<eng-data t="1.8" f="543.32" m="262.077" cg="205."/>
<eng-data t="2.5" f="435.55" m="72.9046" cg="205."/>
<eng-data t="2.9" f="89.85" m="14.8835" cg="205."/>
<eng-data t="3.5" f="0." m="0." cg="205."/>
</data>
</engine>
<engine mfg="Aerotech" code="K560W" Type="reloadable" dia="75." len="396."
initWt="2713.54" propWt="1408.06" delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="496.918" peakThrust="789.305" throatDia="0."
exitDia="0." Itot="2467.2" burn-time="4.96" massFrac="51.89" Isp="178.67"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="1408.06" cg="198."/>
<eng-data t="0.096" f="552.123" m="1392.94" cg="198."/>
<eng-data t="0.29" f="645.403" m="1326.64" cg="198."/>
<eng-data t="0.484" f="681.109" m="1253.21" cg="198."/>
<eng-data t="0.679" f="716.167" m="1175.46" cg="198."/>
<eng-data t="0.874" f="742.678" m="1094.28" cg="198."/>
<eng-data t="1.069" f="764.778" m="1010.4" cg="198."/>
<eng-data t="1.264" f="775.71" m="924.678" cg="198."/>
<eng-data t="1.458" f="785.859" m="838.231" cg="198."/>
<eng-data t="1.653" f="789.305" m="750.582" cg="198."/>
<eng-data t="1.848" f="789.077" m="662.754" cg="198."/>
<eng-data t="2.043" f="744.622" m="577.412" cg="198."/>
<eng-data t="2.237" f="676.886" m="498.718" cg="198."/>
<eng-data t="2.432" f="614.711" m="426.848" cg="198."/>
<eng-data t="2.627" f="557.908" m="361.598" cg="198."/>
<eng-data t="2.822" f="503.641" m="302.529" cg="198."/>
<eng-data t="3.017" f="455.504" m="249.158" cg="198."/>
<eng-data t="3.211" f="412.045" m="201.131" cg="198."/>
<eng-data t="3.406" f="372.963" m="157.45" cg="198."/>
<eng-data t="3.601" f="335.987" m="118.001" cg="198."/>
<eng-data t="3.796" f="307.346" m="82.2028" cg="198."/>
<eng-data t="3.991" f="279.856" m="49.5283" cg="198."/>
<eng-data t="4.185" f="223.491" m="21.6634" cg="198."/>
<eng-data t="4.38" f="70.441" m="5.30776" cg="198."/>
<eng-data t="4.575" f="10.028" m="0.830104" cg="198."/>
<eng-data t="4.77" f="2.445" m="0.136051" cg="198."/>
<eng-data t="4.965" f="0." m="0." cg="198."/>
</data>
</engine>
<engine mfg="Aerotech" code="K650T" Type="reloadable" dia="98." len="289."
initWt="2935.3" propWt="1270.08" delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="581.268" peakThrust="747.557" throatDia="0."
exitDia="0." Itot="2387.85" burn-time="4.11" massFrac="43.27" Isp="191.71"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>AeroTech K650T
Copyright Tripoli Motor Testing 1998 (www.tripoli.org)
provided by ThrustCurve.org (www.thrustcurve.org)
</comments>
<data>
<eng-data t="0." f="0." m="1270.08" cg="144.5"/>
<eng-data t="0.079" f="514.338" m="1259.27" cg="144.5"/>
<eng-data t="0.24" f="594.264" m="1211.81" cg="144.5"/>
<eng-data t="0.401" f="618.849" m="1159.86" cg="144.5"/>
<eng-data t="0.563" f="641.658" m="1105.56" cg="144.5"/>
<eng-data t="0.723" f="665.057" m="1049.95" cg="144.5"/>
<eng-data t="0.884" f="686.488" m="992.085" cg="144.5"/>
<eng-data t="1.046" f="704.685" m="932.149" cg="144.5"/>
<eng-data t="1.206" f="720.215" m="871.517" cg="144.5"/>
<eng-data t="1.368" f="730.072" m="809.034" cg="144.5"/>
<eng-data t="1.529" f="736.891" m="746.222" cg="144.5"/>
<eng-data t="1.69" f="743.109" m="682.853" cg="144.5"/>
<eng-data t="1.851" f="747.503" m="619.029" cg="144.5"/>
<eng-data t="2.013" f="747.557" m="554.617" cg="144.5"/>
<eng-data t="2.174" f="744.081" m="490.748" cg="144.5"/>
<eng-data t="2.335" f="732.294" m="427.534" cg="144.5"/>
<eng-data t="2.496" f="710.412" m="365.761" cg="144.5"/>
<eng-data t="2.657" f="682.67" m="306.113" cg="144.5"/>
<eng-data t="2.819" f="653.246" m="248.557" cg="144.5"/>
<eng-data t="2.979" f="627.02" m="194.08" cg="144.5"/>
<eng-data t="3.141" f="595.456" m="141.412" cg="144.5"/>
<eng-data t="3.302" f="563.844" m="91.7736" cg="144.5"/>
<eng-data t="3.463" f="551.08" m="44.0355" cg="144.5"/>
<eng-data t="3.624" f="236.059" m="10.3322" cg="144.5"/>
<eng-data t="3.785" f="1.383" m="0.165586" cg="144.5"/>
<eng-data t="3.947" f="1.234" m="0.0528366" cg="144.5"/>
<eng-data t="4.108" f="0." m="0." cg="144.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="K680R" Type="reloadable" dia="98." len="289."
initWt="3035." propWt="1316." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="675.742" peakThrust="819.178" throatDia="0." exitDia="0."
Itot="2358.34" burn-time="3.49" massFrac="43.36" Isp="182.74" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Aerotech K680R RASP engine file
Data Entered by Tim Van Milligan
Source: TRA Certification paperwork, and
Aerotech's instruction sheet: RMS 98/2560-10240 REDLINE.
</comments>
<data>
<eng-data t="0." f="0." m="1316." cg="144.5"/>
<eng-data t="0.085" f="629.798" m="1301.06" cg="144.5"/>
<eng-data t="0.494" f="717.881" m="1147.27" cg="144.5"/>
<eng-data t="0.996" f="797.157" m="935.073" cg="144.5"/>
<eng-data t="1.29" f="819.178" m="802.487" cg="144.5"/>
<eng-data t="1.506" f="819.178" m="703.749" cg="144.5"/>
<eng-data t="2.001" f="775.136" m="483.559" cg="144.5"/>
<eng-data t="2.519" f="673.84" m="274.142" cg="144.5"/>
<eng-data t="2.99" f="563.735" m="111.508" cg="144.5"/>
<eng-data t="3.137" f="541.714" m="66.1689" cg="144.5"/>
<eng-data t="3.176" f="532.906" m="54.4756" cg="144.5"/>
<eng-data t="3.238" f="563.735" m="35.5052" cg="144.5"/>
<eng-data t="3.276" f="563.735" m="23.5513" cg="144.5"/>
<eng-data t="3.408" f="52.85" m="0.842942" cg="144.5"/>
<eng-data t="3.431" f="22.02" m="0.362484" cg="144.5"/>
<eng-data t="3.49" f="0." m="0." cg="144.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="K695R" Type="reloadable" dia="54." len="410."
initWt="1506." propWt="931." delays="10,14,1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="665.099" peakThrust="900.13" throatDia="0."
exitDia="0." Itot="1496.47" burn-time="2.25" massFrac="61.82" Isp="163.91"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="931." cg="205."/>
<eng-data t="0.04" f="618.61" m="923.303" cg="205."/>
<eng-data t="0.13" f="727.84" m="885.608" cg="205."/>
<eng-data t="0.22" f="752." m="844.179" cg="205."/>
<eng-data t="0.31" f="812.48" m="800.38" cg="205."/>
<eng-data t="0.4" f="900.13" m="752.434" cg="205."/>
<eng-data t="0.5" f="884.76" m="696.912" cg="205."/>
<eng-data t="0.58" f="873.46" m="653.158" cg="205."/>
<eng-data t="0.68" f="864.56" m="599.095" cg="205."/>
<eng-data t="0.77" f="849.67" m="551.104" cg="205."/>
<eng-data t="0.86" f="838.89" m="503.831" cg="205."/>
<eng-data t="0.95" f="822.55" m="457.318" cg="205."/>
<eng-data t="1.04" f="806.24" m="411.718" cg="205."/>
<eng-data t="1.13" f="781.34" m="367.273" cg="205."/>
<eng-data t="1.22" f="753.97" m="324.29" cg="205."/>
<eng-data t="1.31" f="728.47" m="282.788" cg="205."/>
<eng-data t="1.4" f="697.63" m="242.863" cg="205."/>
<eng-data t="1.49" f="672.98" m="204.492" cg="205."/>
<eng-data t="1.58" f="646.66" m="167.548" cg="205."/>
<eng-data t="1.67" f="620.9" m="132.061" cg="205."/>
<eng-data t="1.76" f="595.57" m="98.0051" cg="205."/>
<eng-data t="1.85" f="571.72" m="65.3259" cg="205."/>
<eng-data t="1.94" f="546.82" m="34.0114" cg="205."/>
<eng-data t="2.03" f="272.82" m="11.0649" cg="205."/>
<eng-data t="2.12" f="57.95" m="1.80474" cg="205."/>
<eng-data t="2.21" f="4.51" m="0.0561161" cg="205."/>
<eng-data t="2.25" f="0." m="0." cg="205."/>
</data>
</engine>
<engine mfg="Aerotech" code="K700W" Type="reloadable" dia="54." len="568."
initWt="2035.26" propWt="1291.58" delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="635.592" peakThrust="1029.34" throatDia="0."
exitDia="0." Itot="2283.68" burn-time="3.59" massFrac="63.46" Isp="180.3"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>AeroTech K700W
Copyright Tripoli Motor Testing 1998 (www.tripoli.org)
provided by ThrustCurve.org (www.thrustcurve.org)
</comments>
<data>
<eng-data t="0." f="0." m="1291.58" cg="284."/>
<eng-data t="0.069" f="1005.47" m="1271.96" cg="284."/>
<eng-data t="0.209" f="1018.92" m="1191.82" cg="284."/>
<eng-data t="0.35" f="1026.61" m="1110.26" cg="284."/>
<eng-data t="0.491" f="1028.64" m="1028.31" cg="284."/>
<eng-data t="0.632" f="1029.34" m="946.25" cg="284."/>
<eng-data t="0.773" f="1004.2" m="865.167" cg="284."/>
<eng-data t="0.914" f="970.694" m="786.423" cg="284."/>
<eng-data t="1.055" f="946.516" m="709.979" cg="284."/>
<eng-data t="1.196" f="918.437" m="635.618" cg="284."/>
<eng-data t="1.336" f="873.783" m="564.664" cg="284."/>
<eng-data t="1.478" f="821.276" m="496.598" cg="284."/>
<eng-data t="1.619" f="773.27" m="433.02" cg="284."/>
<eng-data t="1.759" f="735.553" m="373.285" cg="284."/>
<eng-data t="1.9" f="692.732" m="316.336" cg="284."/>
<eng-data t="2.041" f="658.984" m="262.439" cg="284."/>
<eng-data t="2.182" f="626.737" m="211.174" cg="284."/>
<eng-data t="2.323" f="591.431" m="162.603" cg="284."/>
<eng-data t="2.464" f="508.666" m="118.739" cg="284."/>
<eng-data t="2.605" f="420.175" m="81.7036" cg="284."/>
<eng-data t="2.746" f="328.309" m="51.8596" cg="284."/>
<eng-data t="2.886" f="202.409" m="30.8485" cg="284."/>
<eng-data t="3.028" f="121.672" m="17.8349" cg="284."/>
<eng-data t="3.169" f="80.453" m="9.77565" cg="284."/>
<eng-data t="3.309" f="50.873" m="4.57647" cg="284."/>
<eng-data t="3.451" f="31.548" m="1.26682" cg="284."/>
<eng-data t="3.593" f="0." m="0." cg="284."/>
</data>
</engine>
<engine mfg="Aerotech" code="K780R" Type="reloadable" dia="75." len="395."
initWt="2934.4" propWt="1267.84" delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="770.832" peakThrust="953.578" throatDia="0."
exitDia="0." Itot="2361.06" burn-time="3.06" massFrac="43.21" Isp="189.9"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>AeroTech K780R
provided by ThrustCurve.org (www.thrustcurve.org)
</comments>
<data>
<eng-data t="0." f="0." m="1267.84" cg="197.5"/>
<eng-data t="0.053" f="383.29" m="1262.39" cg="197.5"/>
<eng-data t="0.173" f="718.241" m="1226.9" cg="197.5"/>
<eng-data t="0.292" f="849.343" m="1176.81" cg="197.5"/>
<eng-data t="0.413" f="885.503" m="1120.45" cg="197.5"/>
<eng-data t="0.533" f="903.243" m="1062.82" cg="197.5"/>
<eng-data t="0.652" f="924.403" m="1004.43" cg="197.5"/>
<eng-data t="0.772" f="938.825" m="944.395" cg="197.5"/>
<eng-data t="0.892" f="938.623" m="883.906" cg="197.5"/>
<eng-data t="1.013" f="947.13" m="822.643" cg="197.5"/>
<eng-data t="1.133" f="953.578" m="761.404" cg="197.5"/>
<eng-data t="1.253" f="944.001" m="700.267" cg="197.5"/>
<eng-data t="1.373" f="935.448" m="639.713" cg="197.5"/>
<eng-data t="1.495" f="929.447" m="578.627" cg="197.5"/>
<eng-data t="1.617" f="920.379" m="518.035" cg="197.5"/>
<eng-data t="1.737" f="897.293" m="459.471" cg="197.5"/>
<eng-data t="1.857" f="888.917" m="401.922" cg="197.5"/>
<eng-data t="1.977" f="861.127" m="345.538" cg="197.5"/>
<eng-data t="2.098" f="840.971" m="290.241" cg="197.5"/>
<eng-data t="2.217" f="812.36" m="237.417" cg="197.5"/>
<eng-data t="2.337" f="779.614" m="186.125" cg="197.5"/>
<eng-data t="2.457" f="747.866" m="136.912" cg="197.5"/>
<eng-data t="2.578" f="726.819" m="89.0033" cg="197.5"/>
<eng-data t="2.697" f="729.258" m="42.4812" cg="197.5"/>
<eng-data t="2.817" f="279.891" m="9.96767" cg="197.5"/>
<eng-data t="2.94" f="10.969" m="0.362243" cg="197.5"/>
<eng-data t="3.063" f="0." m="0." cg="197.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="K805G" Type="reloadable" dia="54." len="400.6"
initWt="1543." propWt="871.1" delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="720.852" peakThrust="828.29" throatDia="0." exitDia="0."
Itot="1730.04" burn-time="2.4" massFrac="56.45" Isp="202.52" tDiv="25"
tStep="-0.1" tFix="1" FDiv="20" FStep="-10." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="871.1" cg="853."/>
<eng-data t="0." f="7.66935" m="871.1" cg="853."/>
<eng-data t="0.00388199" f="437.153" m="870.665" cg="853."/>
<eng-data t="0.0427019" f="797.612" m="858.598" cg="853."/>
<eng-data t="0.0776398" f="828.29" m="844.296" cg="853."/>
<eng-data t="0.100932" f="774.604" m="834.897" cg="853."/>
<eng-data t="0.159161" f="736.257" m="812.748" cg="853."/>
<eng-data t="0.197981" f="743.927" m="798.282" cg="853."/>
<eng-data t="0.298913" f="774.604" m="759.696" cg="853."/>
<eng-data t="0.399845" f="789.943" m="719.94" cg="853."/>
<eng-data t="0.500776" f="797.612" m="679.6" cg="853."/>
<eng-data t="0.601708" f="812.951" m="638.675" cg="853."/>
<eng-data t="0.698758" f="812.951" m="598.95" cg="853."/>
<eng-data t="0.799689" f="812.951" m="557.635" cg="853."/>
<eng-data t="0.900621" f="812.951" m="516.321" cg="853."/>
<eng-data t="1.00155" f="812.951" m="475.006" cg="853."/>
<eng-data t="1.0986" f="782.274" m="436.03" cg="853."/>
<eng-data t="1.19953" f="766.935" m="396.664" cg="853."/>
<eng-data t="1.29658" f="759.265" m="359.374" cg="853."/>
<eng-data t="1.4014" f="759.265" m="319.304" cg="853."/>
<eng-data t="1.49845" f="743.927" m="282.577" cg="853."/>
<eng-data t="1.59938" f="720.919" m="245.355" cg="853."/>
<eng-data t="1.69643" f="697.911" m="210.688" cg="853."/>
<eng-data t="1.80124" f="682.572" m="174.261" cg="853."/>
<eng-data t="1.89829" f="659.564" m="141.468" cg="853."/>
<eng-data t="1.99922" f="644.225" m="108.339" cg="853."/>
<eng-data t="2.10016" f="628.887" m="75.9886" cg="853."/>
<eng-data t="2.20109" f="644.225" m="43.6385" cg="853."/>
<eng-data t="2.30202" f="544.524" m="13.432" cg="853."/>
<eng-data t="2.4" f="0." m="0." cg="853."/>
</data>
</engine>
<engine mfg="Aerotech" code="K1050W" Type="single-use" dia="54." len="676."
initWt="2128.45" propWt="1362.2" delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="983.886" peakThrust="1379.52" throatDia="0."
exitDia="0." Itot="2507.93" burn-time="2.55" massFrac="63.29" Isp="189.84"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>AeroTech K1050W-SU
Copyright Tripoli Motor Testing 1998 (www.tripoli.org)
provided by ThrustCurve.org (www.thrustcurve.org)
</comments>
<data>
<eng-data t="0." f="0." m="1347.14" cg="338."/>
<eng-data t="0.049" f="1305.65" m="1329.96" cg="338."/>
<eng-data t="0.149" f="1270.39" m="1260.77" cg="338."/>
<eng-data t="0.249" f="1288.92" m="1192.03" cg="338."/>
<eng-data t="0.349" f="1327.06" m="1121.77" cg="338."/>
<eng-data t="0.449" f="1345.72" m="1049.99" cg="338."/>
<eng-data t="0.549" f="1359.79" m="977.327" cg="338."/>
<eng-data t="0.649" f="1364.45" m="904.16" cg="338."/>
<eng-data t="0.749" f="1365.49" m="830.84" cg="338."/>
<eng-data t="0.849" f="1377.19" m="757.178" cg="338."/>
<eng-data t="0.949" f="1379.52" m="683.139" cg="338."/>
<eng-data t="1.049" f="1346.59" m="609.922" cg="338."/>
<eng-data t="1.149" f="1286.74" m="539.197" cg="338."/>
<eng-data t="1.249" f="1232.1" m="471.547" cg="338."/>
<eng-data t="1.349" f="1186.48" m="406.589" cg="338."/>
<eng-data t="1.449" f="1156.52" m="343.662" cg="338."/>
<eng-data t="1.549" f="1120.05" m="282.519" cg="338."/>
<eng-data t="1.649" f="1098.71" m="222.928" cg="338."/>
<eng-data t="1.749" f="1070.19" m="164.677" cg="338."/>
<eng-data t="1.849" f="889.885" m="112.034" cg="338."/>
<eng-data t="1.949" f="646.691" m="70.7649" cg="338."/>
<eng-data t="2.049" f="441.213" m="41.5464" cg="338."/>
<eng-data t="2.149" f="302.245" m="21.5788" cg="338."/>
<eng-data t="2.249" f="155.001" m="9.29826" cg="338."/>
<eng-data t="2.349" f="52.187" m="3.73367" cg="338."/>
<eng-data t="2.449" f="43.415" m="1.16603" cg="338."/>
<eng-data t="2.549" f="0." m="0." cg="338."/>
</data>
</engine>
<engine mfg="Aerotech" code="K1100T" Type="reloadable" dia="54." len="410."
initWt="1426.1" propWt="791.4" delays="6,10,14,18" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="1011.78" peakThrust="1627.57" throatDia="0."
exitDia="0." Itot="1618.86" burn-time="1.6" massFrac="55.49" Isp="208.59"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="791.4" cg="205."/>
<eng-data t="0." f="1627.57" m="791.4" cg="205."/>
<eng-data t="0.1" f="1244.55" m="721.196" cg="205."/>
<eng-data t="0.4" f="1196.65" m="542.184" cg="205."/>
<eng-data t="0.8" f="1124.9" m="315.2" cg="205."/>
<eng-data t="1." f="1077.04" m="207.555" cg="205."/>
<eng-data t="1.1" f="1053.06" m="155.488" cg="205."/>
<eng-data t="1.2" f="1029.09" m="104.594" cg="205."/>
<eng-data t="1.4" f="660.53" m="21.9947" cg="205."/>
<eng-data t="1.5" f="119.65" m="2.92463" cg="205."/>
<eng-data t="1.6" f="0." m="0." cg="205."/>
</data>
</engine>
<engine mfg="Aerotech" code="K1103X" Type="reloadable" dia="54." len="401."
initWt="1459." propWt="830." delays="14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1071.99" peakThrust="1619.8" throatDia="0." exitDia="0."
Itot="1809.52" burn-time="1.69" massFrac="56.89" Isp="222.31" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>K1103X Propellant X</comments>
<data>
<eng-data t="0." f="0." m="830." cg="200.5"/>
<eng-data t="0.012" f="1335.71" m="826.324" cg="200.5"/>
<eng-data t="0.016" f="1505.17" m="823.718" cg="200.5"/>
<eng-data t="0.028" f="1619.8" m="815.118" cg="200.5"/>
<eng-data t="0.045" f="1500.18" m="802.953" cg="200.5"/>
<eng-data t="0.081" f="1393.03" m="779.066" cg="200.5"/>
<eng-data t="0.151" f="1330.73" m="735.339" cg="200.5"/>
<eng-data t="0.201" f="1305.81" m="705.106" cg="200.5"/>
<eng-data t="0.399" f="1280.89" m="587.644" cg="200.5"/>
<eng-data t="0.602" f="1243.51" m="470.117" cg="200.5"/>
<eng-data t="0.803" f="1196.16" m="357.654" cg="200.5"/>
<eng-data t="1.001" f="1143.83" m="251.396" cg="200.5"/>
<eng-data t="1.203" f="1074.05" m="148.648" cg="200.5"/>
<eng-data t="1.296" f="1041.66" m="103.522" cg="200.5"/>
<eng-data t="1.384" f="1031.69" m="61.6779" cg="200.5"/>
<eng-data t="1.408" f="1004.28" m="50.4716" cg="200.5"/>
<eng-data t="1.423" f="961.912" m="43.7076" cg="200.5"/>
<eng-data t="1.438" f="839.804" m="37.5095" cg="200.5"/>
<eng-data t="1.46" f="737.632" m="29.5505" cg="200.5"/>
<eng-data t="1.49" f="510.86" m="20.9605" cg="200.5"/>
<eng-data t="1.505" f="446.068" m="17.6686" cg="200.5"/>
<eng-data t="1.603" f="176.932" m="3.6663" cg="200.5"/>
<eng-data t="1.608" f="209.328" m="3.22338" cg="200.5"/>
<eng-data t="1.638" f="97.188" m="1.11447" cg="200.5"/>
<eng-data t="1.688" f="0." m="0." cg="200.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="K1275R" Type="reloadable" dia="54." len="569."
initWt="2061." propWt="1308." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1066.15" peakThrust="1557.99" throatDia="0." exitDia="0."
Itot="2132.31" burn-time="2." massFrac="63.46" Isp="166.23" tDiv="10" tStep="-1."
tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="1308." cg="284.5"/>
<eng-data t="0.04" f="1282.62" m="1292.26" cg="284.5"/>
<eng-data t="0.12" f="1557.99" m="1222.56" cg="284.5"/>
<eng-data t="0.2" f="1540.2" m="1146.55" cg="284.5"/>
<eng-data t="0.28" f="1526.78" m="1071.29" cg="284.5"/>
<eng-data t="0.36" f="1500.69" m="997.007" cg="284.5"/>
<eng-data t="0.44" f="1456.58" m="924.445" cg="284.5"/>
<eng-data t="0.52" f="1425.79" m="853.721" cg="284.5"/>
<eng-data t="0.6" f="1390.42" m="784.62" cg="284.5"/>
<eng-data t="0.68" f="1355.11" m="717.254" cg="284.5"/>
<eng-data t="0.76" f="1323.31" m="651.534" cg="284.5"/>
<eng-data t="0.84" f="1282.83" m="587.588" cg="284.5"/>
<eng-data t="0.92" f="1247.8" m="525.494" cg="284.5"/>
<eng-data t="1." f="1194.42" m="465.57" cg="284.5"/>
<eng-data t="1.08" f="1150.98" m="408.022" cg="284.5"/>
<eng-data t="1.16" f="1108.22" m="352.588" cg="284.5"/>
<eng-data t="1.24" f="1068.75" m="299.172" cg="284.5"/>
<eng-data t="1.32" f="1036.92" m="247.506" cg="284.5"/>
<eng-data t="1.4" f="997.44" m="197.589" cg="284.5"/>
<eng-data t="1.48" f="964.57" m="149.448" cg="284.5"/>
<eng-data t="1.56" f="933.3" m="102.88" cg="284.5"/>
<eng-data t="1.64" f="889.99" m="58.1426" cg="284.5"/>
<eng-data t="1.72" f="599.47" m="21.596" cg="284.5"/>
<eng-data t="1.8" f="134.56" m="3.58531" cg="284.5"/>
<eng-data t="1.88" f="5.63" m="0.145503" cg="284.5"/>
<eng-data t="1.96" f="0.2" m="0.00245368" cg="284.5"/>
<eng-data t="2." f="0." m="0." cg="284.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="K1499N" Type="reloadable" dia="75." len="260."
initWt="1741." propWt="604." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1499.8" peakThrust="1720.12" throatDia="0." exitDia="0." Itot="1321.7"
burn-time="0.88" massFrac="0." Isp="223.1" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Entered by Jim Yehle
from TRA cert document</comments>
<data>
<eng-data t="0." f="0." m="604." cg="130."/>
<eng-data t="0.01" f="1450." m="600.684" cg="130."/>
<eng-data t="0.2" f="1720.12" m="462.926" cg="130."/>
<eng-data t="0.35" f="1700." m="345.594" cg="130."/>
<eng-data t="0.5" f="1600." m="232.378" cg="130."/>
<eng-data t="0.6" f="1575." m="159.76" cg="130."/>
<eng-data t="0.7" f="1500." m="89.429" cg="130."/>
<eng-data t="0.82" f="1400." m="9.8349" cg="130."/>
<eng-data t="0.84" f="250." m="2.28719" cg="130."/>
<eng-data t="0.88" f="0." m="0." cg="130."/>
</data>
</engine>
<engine mfg="Aerotech" code="K1999N" Type="reloadable" dia="98." len="289."
initWt="2989." propWt="1195." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1800.28" peakThrust="2002." throatDia="0." exitDia="0." Itot="2520.39"
burn-time="1.4" massFrac="39.98" Isp="215.07" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>98-2560
Greg Gardner - 09/15/06
</comments>
<data>
<eng-data t="0." f="0." m="1195." cg="144.5"/>
<eng-data t="0.025" f="1577." m="1185.65" cg="144.5"/>
<eng-data t="0.03" f="1647." m="1181.83" cg="144.5"/>
<eng-data t="0.05" f="1688." m="1166.02" cg="144.5"/>
<eng-data t="0.075" f="1799." m="1145.35" cg="144.5"/>
<eng-data t="0.1" f="1915." m="1123.34" cg="144.5"/>
<eng-data t="0.125" f="1888." m="1100.8" cg="144.5"/>
<eng-data t="0.15" f="1933." m="1078.16" cg="144.5"/>
<eng-data t="0.175" f="1986." m="1054.93" cg="144.5"/>
<eng-data t="0.182" f="2002." m="1048.31" cg="144.5"/>
<eng-data t="1.07" f="2002." m="205.412" cg="144.5"/>
<eng-data t="1.1" f="1978." m="177.106" cg="144.5"/>
<eng-data t="1.15" f="1910." m="131.021" cg="144.5"/>
<eng-data t="1.2" f="1790." m="87.1633" cg="144.5"/>
<eng-data t="1.225" f="1710." m="66.42" cg="144.5"/>
<eng-data t="1.25" f="1523." m="47.2591" cg="144.5"/>
<eng-data t="1.275" f="1265." m="30.7356" cg="144.5"/>
<eng-data t="1.3" f="998." m="17.3236" cg="144.5"/>
<eng-data t="1.35" f="243." m="2.61365" cg="144.5"/>
<eng-data t="1.375" f="99." m="0.586739" cg="144.5"/>
<eng-data t="1.4" f="0." m="0." cg="144.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="K375NW" Type="reloadable" dia="54." len="568."
initWt="2106." propWt="1318." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="384.474" peakThrust="1343.56" throatDia="0." exitDia="0."
Itot="2229.95" burn-time="5.8" massFrac="62.58" Isp="172.53" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>AeroTech K375
From RASP file created by C. Kobel 3/12/10
Converted to RockSim 9 by R. Geer 3/22/10</comments>
<data>
<eng-data t="0." f="0." m="1318." cg="284."/>
<eng-data t="0.027" f="886.971" m="1310.92" cg="284."/>
<eng-data t="0.036" f="1115.26" m="1305.6" cg="284."/>
<eng-data t="0.054" f="1268.7" m="1292.92" cg="284."/>
<eng-data t="0.135" f="1279.93" m="1231.91" cg="284."/>
<eng-data t="0.197" f="1313.62" m="1184.39" cg="284."/>
<eng-data t="0.292" f="1317.36" m="1110.52" cg="284."/>
<eng-data t="0.422" f="1343.56" m="1008.3" cg="284."/>
<eng-data t="0.444" f="1302.39" m="991.095" cg="284."/>
<eng-data t="0.489" f="1336.07" m="956.008" cg="284."/>
<eng-data t="0.552" f="452.842" m="922.702" cg="284."/>
<eng-data t="0.574" f="396.704" m="917.179" cg="284."/>
<eng-data t="0.718" f="452.842" m="881.026" cg="284."/>
<eng-data t="0.794" f="460.327" m="860.517" cg="284."/>
<eng-data t="0.902" f="437.872" m="831.849" cg="284."/>
<eng-data t="0.992" f="411.674" m="809.254" cg="284."/>
<eng-data t="1.189" f="404.189" m="761.756" cg="284."/>
<eng-data t="1.4" f="366.764" m="713.683" cg="284."/>
<eng-data t="1.575" f="381.734" m="674.973" cg="284."/>
<eng-data t="1.791" f="370.507" m="626.955" cg="284."/>
<eng-data t="4." f="366.764" m="145.658" cg="284."/>
<eng-data t="4.165" f="344.309" m="110.985" cg="284."/>
<eng-data t="4.29" f="239.52" m="89.4182" cg="284."/>
<eng-data t="4.398" f="239.52" m="74.1289" cg="284."/>
<eng-data t="4.537" f="183.382" m="56.7571" cg="284."/>
<eng-data t="4.645" f="183.382" m="45.0513" cg="284."/>
<eng-data t="4.761" f="93.562" m="35.5575" cg="284."/>
<eng-data t="5." f="93.562" m="22.3409" cg="284."/>
<eng-data t="5.2" f="63.622" m="13.0506" cg="284."/>
<eng-data t="5.4" f="44.91" m="6.6359" cg="284."/>
<eng-data t="5.6" f="33.682" m="1.99076" cg="284."/>
<eng-data t="5.8" f="0." m="0." cg="284."/>
</data>
</engine>
<engine mfg="Aerotech" code="K455NW" Type="single-use" dia="54." len="675."
initWt="2286." propWt="145.6" delays="17" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="431.165" peakThrust="1300.22" throatDia="0." exitDia="0."
Itot="2328.29" burn-time="5.4" massFrac="6.37" Isp="1630.63" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="145.6" cg="337.5"/>
<eng-data t="0.014" f="12.1761" m="145.595" cg="337.5"/>
<eng-data t="0.034" f="263.205" m="145.422" cg="337.5"/>
<eng-data t="0.062" f="1218.88" m="144.125" cg="337.5"/>
<eng-data t="0.111" f="1228.86" m="140.375" cg="337.5"/>
<eng-data t="0.2" f="1287.57" m="133.372" cg="337.5"/>
<eng-data t="0.409" f="1300.22" m="116.461" cg="337.5"/>
<eng-data t="0.505" f="1234.35" m="108.853" cg="337.5"/>
<eng-data t="0.548" f="1082.7" m="105.738" cg="337.5"/>
<eng-data t="0.587" f="395.753" m="103.935" cg="337.5"/>
<eng-data t="0.62" f="445.028" m="103.067" cg="337.5"/>
<eng-data t="0.85" f="476.417" m="96.4407" cg="337.5"/>
<eng-data t="1.23" f="447.072" m="85.4681" cg="337.5"/>
<eng-data t="1.725" f="437.524" m="71.7768" cg="337.5"/>
<eng-data t="2.22" f="428.648" m="58.3707" cg="337.5"/>
<eng-data t="2.714" f="414.93" m="45.3406" cg="337.5"/>
<eng-data t="3.208" f="401.805" m="32.7252" cg="337.5"/>
<eng-data t="3.664" f="395.35" m="21.3593" cg="337.5"/>
<eng-data t="3.941" f="399.6" m="14.4742" cg="337.5"/>
<eng-data t="4.12" f="294.943" m="10.5869" cg="337.5"/>
<eng-data t="4.5" f="164.816" m="5.12419" cg="337.5"/>
<eng-data t="4.881" f="101.877" m="1.94709" cg="337.5"/>
<eng-data t="5.147" f="62.2312" m="0.582167" cg="337.5"/>
<eng-data t="5.329" f="28.8252" m="0.063992" cg="337.5"/>
<eng-data t="5.4" f="0." m="0." cg="337.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="K456DM" Type="reloadable" dia="54." len="401."
initWt="1484." propWt="866." delays="14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="429.91" peakThrust="519.582" throatDia="0." exitDia="0."
Itot="1305.64" burn-time="3.04" massFrac="58.36" Isp="153.74" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>K456 Dark Matter</comments>
<data>
<eng-data t="0." f="0." m="866." cg="200.5"/>
<eng-data t="0.027" f="444.074" m="862.024" cg="200.5"/>
<eng-data t="0.038" f="519.582" m="858.508" cg="200.5"/>
<eng-data t="0.066" f="482.95" m="849.199" cg="200.5"/>
<eng-data t="0.129" f="461.269" m="829.471" cg="200.5"/>
<eng-data t="0.302" f="467.998" m="776.156" cg="200.5"/>
<eng-data t="0.389" f="468.745" m="749.128" cg="200.5"/>
<eng-data t="0.499" f="476.969" m="714.628" cg="200.5"/>
<eng-data t="0.655" f="476.221" m="665.315" cg="200.5"/>
<eng-data t="0.798" f="483.697" m="619.791" cg="200.5"/>
<eng-data t="0.946" f="488.93" m="572.052" cg="200.5"/>
<eng-data t="1.096" f="499.397" m="522.887" cg="200.5"/>
<eng-data t="1.401" f="500.892" m="421.708" cg="200.5"/>
<eng-data t="1.603" f="503.882" m="354.397" cg="200.5"/>
<eng-data t="1.801" f="501.64" m="288.37" cg="200.5"/>
<eng-data t="1.905" f="498.649" m="253.87" cg="200.5"/>
<eng-data t="2.1" f="485.94" m="190.197" cg="200.5"/>
<eng-data t="2.302" f="456.036" m="127.093" cg="200.5"/>
<eng-data t="2.404" f="435.851" m="96.9229" cg="200.5"/>
<eng-data t="2.505" f="420.151" m="68.2507" cg="200.5"/>
<eng-data t="2.574" f="398.471" m="49.5181" cg="200.5"/>
<eng-data t="2.607" f="373.052" m="41.0745" cg="200.5"/>
<eng-data t="2.645" f="356.605" m="31.8792" cg="200.5"/>
<eng-data t="2.703" f="289.321" m="19.4548" cg="200.5"/>
<eng-data t="2.768" f="178.676" m="9.36639" cg="200.5"/>
<eng-data t="2.804" f="123.354" m="5.76046" cg="200.5"/>
<eng-data t="2.837" f="88.964" m="3.43684" cg="200.5"/>
<eng-data t="2.875" f="50.837" m="1.67503" cg="200.5"/>
<eng-data t="2.908" f="24.671" m="0.848661" cg="200.5"/>
<eng-data t="2.957" f="10.466" m="0.277674" cg="200.5"/>
<eng-data t="3.037" f="0." m="0." cg="200.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="K513FJ" Type="reloadable" dia="54." len="410."
initWt="1647." propWt="974." delays="6,10,14,18" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="541.036" peakThrust="656.019" throatDia="0."
exitDia="0." Itot="1474.86" burn-time="2.73" massFrac="59.14" Isp="154.41"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Input by Tim Van Milligan using ThrustCurve Tracer by John Coker. Data from
Tripoli certification paperwork dated 25 November 2007.
</comments>
<data>
<eng-data t="0." f="0." m="974." cg="205."/>
<eng-data t="0.007" f="555.093" m="972.717" cg="205."/>
<eng-data t="0.015" f="652.655" m="969.527" cg="205."/>
<eng-data t="0.041" f="551.729" m="959.187" cg="205."/>
<eng-data t="0.059" f="592.099" m="952.388" cg="205."/>
<eng-data t="0.074" f="551.729" m="946.723" cg="205."/>
<eng-data t="0.2" f="575.278" m="899.834" cg="205."/>
<eng-data t="0.282" f="582.007" m="868.498" cg="205."/>
<eng-data t="0.412" f="605.556" m="817.521" cg="205."/>
<eng-data t="0.519" f="615.649" m="774.374" cg="205."/>
<eng-data t="0.679" f="635.834" m="708.256" cg="205."/>
<eng-data t="0.823" f="642.562" m="647.47" cg="205."/>
<eng-data t="0.986" f="649.291" m="577.939" cg="205."/>
<eng-data t="1.12" f="652.655" m="520.332" cg="205."/>
<eng-data t="1.328" f="656.019" m="430.45" cg="205."/>
<eng-data t="1.48" f="649.291" m="364.936" cg="205."/>
<eng-data t="1.602" f="629.105" m="313.437" cg="205."/>
<eng-data t="1.854" f="585.371" m="212.38" cg="205."/>
<eng-data t="1.999" f="555.093" m="157.775" cg="205."/>
<eng-data t="2.054" f="545." m="137.796" cg="205."/>
<eng-data t="2.08" f="545." m="128.439" cg="205."/>
<eng-data t="2.114" f="528.179" m="116.39" cg="205."/>
<eng-data t="2.184" f="524.815" m="92.0513" cg="205."/>
<eng-data t="2.229" f="521.451" m="76.5049" cg="205."/>
<eng-data t="2.258" f="504.63" m="66.6793" cg="205."/>
<eng-data t="2.295" f="474.352" m="54.7187" cg="205."/>
<eng-data t="2.325" f="437.346" m="45.6874" cg="205."/>
<eng-data t="2.358" f="380.155" m="36.7794" cg="205."/>
<eng-data t="2.37" f="349.877" m="33.8868" cg="205."/>
<eng-data t="2.399" f="312.871" m="27.5404" cg="205."/>
<eng-data t="2.451" f="272.5" m="17.4894" cg="205."/>
<eng-data t="2.492" f="238.858" m="10.5665" cg="205."/>
<eng-data t="2.529" f="161.482" m="5.67539" cg="205."/>
<eng-data t="2.57" f="84.105" m="2.35059" cg="205."/>
<eng-data t="2.592" f="43.735" m="1.42191" cg="205."/>
<eng-data t="2.618" f="26.914" m="0.815371" cg="205."/>
<eng-data t="2.655" f="13.457" m="0.322142" cg="205."/>
<eng-data t="2.692" f="6.728" m="0.0755339" cg="205."/>
<eng-data t="2.726" f="0." m="0." cg="205."/>
</data>
</engine>
<engine mfg="Aerotech" code="K828FJ" Type="reloadable" dia="54." len="579."
initWt="2223." propWt="1373." delays="6,10,14,18" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="862.878" peakThrust="1303.79" throatDia="0."
exitDia="0." Itot="2157.2" burn-time="2.5" massFrac="61.76" Isp="160.21"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Cert data from TRA
Converted from Mark Koelsch</comments>
<data>
<eng-data t="0." f="0." m="1373." cg="289.5"/>
<eng-data t="0.01" f="1112.06" m="1369.46" cg="289.5"/>
<eng-data t="0.02" f="1112.06" m="1362.38" cg="289.5"/>
<eng-data t="0.04" f="1238.6" m="1347.42" cg="289.5"/>
<eng-data t="0.06" f="1303.79" m="1331.24" cg="289.5"/>
<eng-data t="0.08" f="1135.06" m="1315.72" cg="289.5"/>
<eng-data t="0.13" f="1077.54" m="1280.51" cg="289.5"/>
<eng-data t="0.2" f="1031.53" m="1233.53" cg="289.5"/>
<eng-data t="0.5" f="1016.19" m="1038.03" cg="289.5"/>
<eng-data t="0.65" f="993.18" m="942.111" cg="289.5"/>
<eng-data t="1." f="1004.68" m="719.583" cg="289.5"/>
<eng-data t="1.08" f="985.51" m="668.915" cg="289.5"/>
<eng-data t="1.19" f="974.01" m="600.32" cg="289.5"/>
<eng-data t="1.42" f="974.01" m="457.735" cg="289.5"/>
<eng-data t="1.51" f="954.83" m="402.491" cg="289.5"/>
<eng-data t="1.69" f="935.66" m="294.198" cg="289.5"/>
<eng-data t="1.75" f="912.65" m="258.906" cg="289.5"/>
<eng-data t="1.83" f="885.81" m="213.119" cg="289.5"/>
<eng-data t="1.89" f="893.48" m="179.145" cg="289.5"/>
<eng-data t="1.95" f="843.63" m="145.976" cg="289.5"/>
<eng-data t="2." f="774.6" m="120.227" cg="289.5"/>
<eng-data t="2.15" f="667.23" m="51.4005" cg="289.5"/>
<eng-data t="2.2" f="444.82" m="33.7057" cg="289.5"/>
<eng-data t="2.23" f="364.29" m="25.9811" cg="289.5"/>
<eng-data t="2.27" f="260.76" m="18.0245" cg="289.5"/>
<eng-data t="2.33" f="184.06" m="9.53099" cg="289.5"/>
<eng-data t="2.39" f="111.21" m="3.89303" cg="289.5"/>
<eng-data t="2.5" f="0." m="0." cg="289.5"/>
<eng-data t="2.5" f="49.85" m="0." cg="289.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="K850DM" Type="reloadable" dia="54." len="635."
initWt="2041." propWt="1224." delays="16" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="882.603" peakThrust="1064.92" throatDia="0." exitDia="0."
Itot="1869.35" burn-time="2.12" massFrac="59.97" Isp="155.74" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Aerotech K850DM DMS</comments>
<data>
<eng-data t="0." f="0." m="1224." cg="317.5"/>
<eng-data t="0.02" f="50.816" m="1223.67" cg="317.5"/>
<eng-data t="0.032" f="236.404" m="1222.54" cg="317.5"/>
<eng-data t="0.034" f="450.714" m="1222.09" cg="317.5"/>
<eng-data t="0.04" f="1049.46" m="1219.14" cg="317.5"/>
<eng-data t="0.044" f="810.843" m="1216.71" cg="317.5"/>
<eng-data t="0.048" f="901.427" m="1214.46" cg="317.5"/>
<eng-data t="0.05" f="859.449" m="1213.31" cg="317.5"/>
<eng-data t="0.066" f="848.402" m="1204.36" cg="317.5"/>
<eng-data t="0.158" f="914.684" m="1151.26" cg="317.5"/>
<eng-data t="0.326" f="961.081" m="1048.09" cg="317.5"/>
<eng-data t="0.615" f="1029.57" m="859.748" cg="317.5"/>
<eng-data t="0.923" f="1064.92" m="648.55" cg="317.5"/>
<eng-data t="1.075" f="1060.5" m="542.784" cg="317.5"/>
<eng-data t="1.233" f="1040.62" m="434.099" cg="317.5"/>
<eng-data t="1.369" f="994.221" m="343.499" cg="317.5"/>
<eng-data t="1.407" f="1018.52" m="318.459" cg="317.5"/>
<eng-data t="1.483" f="978.756" m="268.764" cg="317.5"/>
<eng-data t="1.545" f="974.337" m="229.12" cg="317.5"/>
<eng-data t="1.567" f="985.384" m="215.005" cg="317.5"/>
<eng-data t="1.591" f="963.29" m="199.694" cg="317.5"/>
<eng-data t="1.673" f="947.824" m="148.389" cg="317.5"/>
<eng-data t="1.712" f="952.243" m="124.129" cg="317.5"/>
<eng-data t="1.76" f="910.265" m="94.8605" cg="317.5"/>
<eng-data t="1.854" f="702.583" m="45.2263" cg="317.5"/>
<eng-data t="1.926" f="444.086" m="18.1973" cg="317.5"/>
<eng-data t="1.978" f="225.357" m="6.80066" cg="317.5"/>
<eng-data t="2.028" f="79.538" m="1.80975" cg="317.5"/>
<eng-data t="2.07" f="24.303" m="0.38191" cg="317.5"/>
<eng-data t="2.118" f="0." m="0." cg="317.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="K990DM" Type="single-use" dia="54." len="598."
initWt="2109." propWt="1224." delays="14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="877.19" peakThrust="1068.83" throatDia="0." exitDia="0."
Itot="1874.56" burn-time="2.14" massFrac="58.04" Isp="156.17" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Aerotech K990DM 54/2800</comments>
<data>
<eng-data t="0." f="0." m="1224." cg="299."/>
<eng-data t="0.016" f="35.558" m="1223.81" cg="299."/>
<eng-data t="0.024" f="223.805" m="1223.14" cg="299."/>
<eng-data t="0.028" f="868.03" m="1221.71" cg="299."/>
<eng-data t="0.036" f="1068.83" m="1216.65" cg="299."/>
<eng-data t="0.044" f="895.222" m="1211.52" cg="299."/>
<eng-data t="0.048" f="863.847" m="1209.23" cg="299."/>
<eng-data t="0.06" f="840.839" m="1202.55" cg="299."/>
<eng-data t="0.228" f="966.337" m="1103.43" cg="299."/>
<eng-data t="0.286" f="953.788" m="1067.07" cg="299."/>
<eng-data t="0.369" f="964.246" m="1015.09" cg="299."/>
<eng-data t="0.407" f="993.529" m="990.805" cg="299."/>
<eng-data t="0.423" f="976.796" m="980.513" cg="299."/>
<eng-data t="0.498" f="989.345" m="932.37" cg="299."/>
<eng-data t="0.694" f="1024.9" m="803.479" cg="299."/>
<eng-data t="0.865" f="1043.73" m="687.993" cg="299."/>
<eng-data t="0.962" f="1054.19" m="621.555" cg="299."/>
<eng-data t="1.117" f="1054.19" m="514.863" cg="299."/>
<eng-data t="1.282" f="1029.09" m="402.64" cg="299."/>
<eng-data t="1.51" f="983.071" m="252.861" cg="299."/>
<eng-data t="1.589" f="960.063" m="202.744" cg="299."/>
<eng-data t="1.688" f="953.788" m="140.886" cg="299."/>
<eng-data t="1.732" f="968.429" m="113.274" cg="299."/>
<eng-data t="1.748" f="1001.89" m="102.981" cg="299."/>
<eng-data t="1.778" f="957.971" m="83.7858" cg="299."/>
<eng-data t="1.802" f="891.038" m="69.2979" cg="299."/>
<eng-data t="1.857" f="671.416" m="41.2421" cg="299."/>
<eng-data t="1.913" f="447.611" m="20.7832" cg="299."/>
<eng-data t="1.97" f="223.805" m="8.2887" cg="299."/>
<eng-data t="2.006" f="129.682" m="4.13411" cg="299."/>
<eng-data t="2.063" f="46.016" m="0.864505" cg="299."/>
<eng-data t="2.097" f="14.641" m="0.191198" cg="299."/>
<eng-data t="2.137" f="0." m="0." cg="299."/>
</data>
</engine>
<engine mfg="Aerotech" code="K2050ST" Type="reloadable" dia="54." len="410."
initWt="1283." propWt="626." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1812.27" peakThrust="2168.28" throatDia="0." exitDia="0."
Itot="1400.88" burn-time="0.77" massFrac="48.79" Isp="228.2" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>K2050 Super Thunder</comments>
<data>
<eng-data t="0." f="0." m="626." cg="205."/>
<eng-data t="0.017" f="1851.87" m="618.966" cg="205."/>
<eng-data t="0.023" f="1758.82" m="614.126" cg="205."/>
<eng-data t="0.032" f="1861.18" m="606.846" cg="205."/>
<eng-data t="0.036" f="1749.51" m="603.619" cg="205."/>
<eng-data t="0.044" f="1805.35" m="597.265" cg="205."/>
<eng-data t="0.063" f="1898.4" m="581.542" cg="205."/>
<eng-data t="0.082" f="1954.24" m="565.187" cg="205."/>
<eng-data t="0.112" f="2010.07" m="538.614" cg="205."/>
<eng-data t="0.138" f="2047.3" m="515.044" cg="205."/>
<eng-data t="0.169" f="2075.22" m="486.49" cg="205."/>
<eng-data t="0.203" f="2121.74" m="454.608" cg="205."/>
<eng-data t="0.235" f="2149.66" m="424.068" cg="205."/>
<eng-data t="0.264" f="2158.97" m="396.15" cg="205."/>
<eng-data t="0.29" f="2168.28" m="371.012" cg="205."/>
<eng-data t="0.317" f="2168.28" m="344.852" cg="205."/>
<eng-data t="0.337" f="2168.28" m="325.473" cg="205."/>
<eng-data t="0.372" f="2158.97" m="291.634" cg="205."/>
<eng-data t="0.406" f="2158.97" m="258.832" cg="205."/>
<eng-data t="0.432" f="2112.44" m="234.019" cg="205."/>
<eng-data t="0.459" f="2075.22" m="208.756" cg="205."/>
<eng-data t="0.483" f="2047.3" m="186.65" cg="205."/>
<eng-data t="0.502" f="2000.77" m="169.465" cg="205."/>
<eng-data t="0.525" f="1972.85" m="149.045" cg="205."/>
<eng-data t="0.55" f="1935.63" m="127.213" cg="205."/>
<eng-data t="0.571" f="1926.32" m="109.093" cg="205."/>
<eng-data t="0.595" f="1935.63" m="88.3836" cg="205."/>
<eng-data t="0.612" f="1982.16" m="73.5026" cg="205."/>
<eng-data t="0.633" f="2000.77" m="54.8145" cg="205."/>
<eng-data t="0.65" f="1926.32" m="39.8982" cg="205."/>
<eng-data t="0.664" f="1777.43" m="28.3128" cg="205."/>
<eng-data t="0.667" f="1628.53" m="26.0298" cg="205."/>
<eng-data t="0.677" f="1433.11" m="19.1891" cg="205."/>
<eng-data t="0.698" f="893.366" m="8.27322" cg="205."/>
<eng-data t="0.72" f="335.012" m="2.23516" cg="205."/>
<eng-data t="0.739" f="93.059" m="0.417924" cg="205."/>
<eng-data t="0.743" f="55.835" m="0.284854" cg="205."/>
<eng-data t="0.753" f="27.918" m="0.0977245" cg="205."/>
<eng-data t="0.762" f="9.306" m="0.0228717" cg="205."/>
<eng-data t="0.773" f="0." m="0." cg="205."/>
</data>
</engine>
<engine mfg="Aerotech" code="L339N" Type="reloadable" dia="98." len="309."
initWt="3149." propWt="1355." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="332.359" peakThrust="421.031" throatDia="0." exitDia="0."
Itot="2800.46" burn-time="8.43" massFrac="39.91" Isp="159." tDiv="10" tStep="-1."
tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Entered by Tim Van Milligan. Used John Coker's ThrustCurve Tracer software and
data supplied by Aerotech thrust stand data.</comments>
<data>
<eng-data t="0." f="0." m="1796." cg="154.5"/>
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<eng-data t="0.427" f="417.426" m="1700.2" cg="154.5"/>
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<eng-data t="2.404" f="377.053" m="1198.05" cg="154.5"/>
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<eng-data t="2.552" f="377.053" m="1162.19" cg="154.5"/>
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<eng-data t="4.233" f="336.681" m="782.632" cg="154.5"/>
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<eng-data t="4.668" f="330.913" m="689.579" cg="154.5"/>
<eng-data t="4.996" f="329.471" m="620.121" cg="154.5"/>
<eng-data t="5.39" f="323.704" m="537.599" cg="154.5"/>
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<eng-data t="6.178" f="310.727" m="376.968" cg="154.5"/>
<eng-data t="6.325" f="306.401" m="347.879" cg="154.5"/>
<eng-data t="6.514" f="302.075" m="311.002" cg="154.5"/>
<eng-data t="6.621" f="302.075" m="290.273" cg="154.5"/>
<eng-data t="6.851" f="297.75" m="246.035" cg="154.5"/>
<eng-data t="7.195" f="290.54" m="181.142" cg="154.5"/>
<eng-data t="7.277" f="293.424" m="165.787" cg="154.5"/>
<eng-data t="7.326" f="287.656" m="156.657" cg="154.5"/>
<eng-data t="7.441" f="283.331" m="135.601" cg="154.5"/>
<eng-data t="7.49" f="286.214" m="126.652" cg="154.5"/>
<eng-data t="7.54" f="283.331" m="117.52" cg="154.5"/>
<eng-data t="7.696" f="275.4" m="89.5709" cg="154.5"/>
<eng-data t="7.81" f="273.958" m="69.4889" cg="154.5"/>
<eng-data t="7.884" f="276.842" m="56.419" cg="154.5"/>
<eng-data t="7.942" f="278.284" m="46.0945" cg="154.5"/>
<eng-data t="8.015" f="276.121" m="33.1169" cg="154.5"/>
<eng-data t="8.073" f="270.354" m="22.9533" cg="154.5"/>
<eng-data t="8.188" f="155.003" m="7.26781" cg="154.5"/>
<eng-data t="8.212" f="118.956" m="5.15945" cg="154.5"/>
<eng-data t="8.278" f="54.071" m="1.49757" cg="154.5"/>
<eng-data t="8.311" f="26.675" m="0.643127" cg="154.5"/>
<eng-data t="8.352" f="7.93" m="0.188171" cg="154.5"/>
<eng-data t="8.426" f="0." m="0." cg="154.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="L400W" Type="reloadable" dia="98." len="443.2"
initWt="5084.74" propWt="2648.97" delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="293.408" peakThrust="720.612" throatDia="0."
exitDia="0." Itot="4676.34" burn-time="15.94" massFrac="52.1" Isp="180.02"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Aerotech L400W-PS created using TCtracer and AT thrustcurve</comments>
<data>
<eng-data t="0." f="0." m="2648.97" cg="221.6"/>
<eng-data t="0.031" f="436.662" m="2645.13" cg="221.6"/>
<eng-data t="0.062" f="493.929" m="2636.96" cg="221.6"/>
<eng-data t="0.063" f="586.988" m="2636.65" cg="221.6"/>
<eng-data t="0.108" f="634.711" m="2621.08" cg="221.6"/>
<eng-data t="0.154" f="606.077" m="2604.92" cg="221.6"/>
<eng-data t="0.277" f="622.78" m="2562.11" cg="221.6"/>
<eng-data t="0.4" f="639.483" m="2518.13" cg="221.6"/>
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<eng-data t="1.631" f="720.612" m="2051.87" cg="221.6"/>
<eng-data t="1.954" f="706.295" m="1921.33" cg="221.6"/>
<eng-data t="2.385" f="703.909" m="1749.18" cg="221.6"/>
<eng-data t="2.6" f="701.523" m="1663.6" cg="221.6"/>
<eng-data t="2.769" f="689.592" m="1597.01" cg="221.6"/>
<eng-data t="3.2" f="656.186" m="1432.73" cg="221.6"/>
<eng-data t="3.754" f="586.988" m="1237.67" cg="221.6"/>
<eng-data t="4.354" f="527.335" m="1048.3" cg="221.6"/>
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<eng-data t="5.815" f="386.553" m="672.435" cg="221.6"/>
<eng-data t="6.477" f="336.445" m="536.874" cg="221.6"/>
<eng-data t="7.354" f="276.791" m="384.551" cg="221.6"/>
<eng-data t="8.046" f="217.138" m="287.743" cg="221.6"/>
<eng-data t="8.846" f="167.029" m="200.696" cg="221.6"/>
<eng-data t="9.862" f="107.376" m="121.733" cg="221.6"/>
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<eng-data t="11.969" f="40.564" m="38.1303" cg="221.6"/>
<eng-data t="12.969" f="26.247" m="19.2074" cg="221.6"/>
<eng-data t="13.985" f="14.317" m="7.53463" cg="221.6"/>
<eng-data t="14.938" f="7.158" m="1.73813" cg="221.6"/>
<eng-data t="15.462" f="2.386" m="0.321675" cg="221.6"/>
<eng-data t="15.938" f="0." m="0." cg="221.6"/>
</data>
</engine>
<engine mfg="Aerotech" code="L850W" Type="reloadable" dia="75." len="531."
initWt="3673.15" propWt="2065.28" delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="786.668" peakThrust="1184.8" throatDia="0."
exitDia="0." Itot="3694.98" burn-time="4.7" massFrac="56.23" Isp="182.44"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="2065.28" cg="265.5"/>
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<eng-data t="0.274" f="1064.94" m="1933.02" cg="265.5"/>
<eng-data t="0.458" f="1101.37" m="1821.62" cg="265.5"/>
<eng-data t="0.643" f="1143.36" m="1705.57" cg="265.5"/>
<eng-data t="0.827" f="1170.93" m="1586.56" cg="265.5"/>
<eng-data t="1.011" f="1184.8" m="1465.42" cg="265.5"/>
<eng-data t="1.196" f="1178.04" m="1343.26" cg="265.5"/>
<eng-data t="1.38" f="1177.6" m="1222.12" cg="265.5"/>
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<eng-data t="1.748" f="1170.02" m="980.569" cg="265.5"/>
<eng-data t="1.932" f="1113.72" m="863.133" cg="265.5"/>
<eng-data t="2.117" f="1042.59" m="751.647" cg="265.5"/>
<eng-data t="2.301" f="972.795" m="648.01" cg="265.5"/>
<eng-data t="2.485" f="908.071" m="551.291" cg="265.5"/>
<eng-data t="2.67" f="844.471" m="460.681" cg="265.5"/>
<eng-data t="2.854" f="773.595" m="377.476" cg="265.5"/>
<eng-data t="3.039" f="714.046" m="300.562" cg="265.5"/>
<eng-data t="3.222" f="649.095" m="230.846" cg="265.5"/>
<eng-data t="3.406" f="597.341" m="166.751" cg="265.5"/>
<eng-data t="3.591" f="557.444" m="107.046" cg="265.5"/>
<eng-data t="3.775" f="422.233" m="56.6687" cg="265.5"/>
<eng-data t="3.959" f="200.739" m="24.6338" cg="265.5"/>
<eng-data t="4.144" f="79.411" m="10.1494" cg="265.5"/>
<eng-data t="4.328" f="43.959" m="3.80542" cg="265.5"/>
<eng-data t="4.513" f="14.862" m="0.764244" cg="265.5"/>
<eng-data t="4.697" f="0." m="0." cg="265.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="L952W" Type="reloadable" dia="98." len="443."
initWt="5026.5" propWt="2660." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="760.884" peakThrust="1056.44" throatDia="0." exitDia="0."
Itot="5097.92" burn-time="6.7" massFrac="52.92" Isp="195.43" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="2660." cg="221.5"/>
<eng-data t="0." f="1.51" m="2660." cg="221.5"/>
<eng-data t="0.1" f="776.75" m="2639.7" cg="221.5"/>
<eng-data t="1." f="909.97" m="2243.65" cg="221.5"/>
<eng-data t="1.3" f="962.28" m="2097.12" cg="221.5"/>
<eng-data t="2.8" f="1056.44" m="1307.12" cg="221.5"/>
<eng-data t="3.3" f="1047.59" m="1032.66" cg="221.5"/>
<eng-data t="3.4" f="1034.25" m="978.343" cg="221.5"/>
<eng-data t="4." f="887.78" m="677.479" cg="221.5"/>
<eng-data t="5.3" f="519.39" m="200.227" cg="221.5"/>
<eng-data t="6." f="288.5" m="52.6869" cg="221.5"/>
<eng-data t="6.7" f="0." m="0." cg="221.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="L1000W" Type="single-use" dia="54." len="635."
initWt="2194." propWt="1400." delays="18" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="900.695" peakThrust="1322.28" throatDia="0." exitDia="0."
Itot="2702.09" burn-time="3." massFrac="63.81" Isp="196.81" tDiv="10" tStep="-1."
tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>per AT announcement 5/8/14</comments>
<data>
<eng-data t="0." f="0." m="1400." cg="317.5"/>
<eng-data t="0.004" f="10.664" m="1399.99" cg="317.5"/>
<eng-data t="0.011" f="1268.96" m="1397.67" cg="317.5"/>
<eng-data t="0.04" f="1322.28" m="1378.2" cg="317.5"/>
<eng-data t="0.195" f="1226.31" m="1275.86" cg="317.5"/>
<eng-data t="0.249" f="1268.96" m="1240.96" cg="317.5"/>
<eng-data t="0.296" f="1242.3" m="1210.38" cg="317.5"/>
<eng-data t="0.372" f="1252.97" m="1161.25" cg="317.5"/>
<eng-data t="0.416" f="1215.64" m="1133.11" cg="317.5"/>
<eng-data t="0.6" f="1226.31" m="1016.71" cg="317.5"/>
<eng-data t="0.788" f="1215.64" m="897.784" cg="317.5"/>
<eng-data t="1.066" f="1183.65" m="724.99" cg="317.5"/>
<eng-data t="1.261" f="1167.66" m="606.21" cg="317.5"/>
<eng-data t="1.507" f="1125." m="460.102" cg="317.5"/>
<eng-data t="1.746" f="1087.68" m="323.103" cg="317.5"/>
<eng-data t="1.865" f="1050.36" m="257.192" cg="317.5"/>
<eng-data t="1.995" f="1045.03" m="186.624" cg="317.5"/>
<eng-data t="2.093" f="911.733" m="136.946" cg="317.5"/>
<eng-data t="2.158" f="746.448" m="109.024" cg="317.5"/>
<eng-data t="2.263" f="554.504" m="73.6369" cg="317.5"/>
<eng-data t="2.389" f="405.215" m="42.3103" cg="317.5"/>
<eng-data t="2.577" f="191.944" m="13.2268" cg="317.5"/>
<eng-data t="2.693" f="85.308" m="4.89511" cg="317.5"/>
<eng-data t="2.761" f="42.654" m="2.64093" cg="317.5"/>
<eng-data t="3." f="0." m="0." cg="317.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="L1090W" Type="reloadable" dia="54." len="625.5"
initWt="2432." propWt="1400." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="911.024" peakThrust="1321.59" throatDia="0." exitDia="0."
Itot="2698.45" burn-time="2.96" massFrac="57.57" Isp="196.55" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>AT L1090w 54-2800</comments>
<data>
<eng-data t="0." f="0." m="1400." cg="312.75"/>
<eng-data t="0.009" f="1114.88" m="1397.4" cg="312.75"/>
<eng-data t="0.012" f="1253.42" m="1395.55" cg="312.75"/>
<eng-data t="0.052" f="1321.59" m="1368.83" cg="312.75"/>
<eng-data t="0.116" f="1253.42" m="1326.08" cg="312.75"/>
<eng-data t="0.205" f="1218.23" m="1269.02" cg="312.75"/>
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<eng-data t="0.295" f="1240.22" m="1210.71" cg="312.75"/>
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<eng-data t="0.631" f="1229.23" m="996.025" cg="312.75"/>
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<eng-data t="0.827" f="1202.84" m="871.883" cg="312.75"/>
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<eng-data t="2.5" f="274.872" m="20.9052" cg="312.75"/>
<eng-data t="2.554" f="222.097" m="13.9437" cg="312.75"/>
<eng-data t="2.598" f="162.724" m="9.55134" cg="312.75"/>
<eng-data t="2.624" f="147.332" m="7.46014" cg="312.75"/>
<eng-data t="2.688" f="79.163" m="3.69984" cg="312.75"/>
<eng-data t="2.754" f="32.985" m="1.77977" cg="312.75"/>
<eng-data t="2.962" f="0." m="0." cg="312.75"/>
</data>
</engine>
<engine mfg="Aerotech" code="L1150R" Type="reloadable" dia="75." len="531."
initWt="3673.6" propWt="2065.28" delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="1102.23" peakThrust="1309.71" throatDia="0."
exitDia="0." Itot="3488.55" burn-time="3.17" massFrac="56.22" Isp="172.24"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>AeroTech L1150
provided by ThrustCurve.org (www.thrustcurve.org)
</comments>
<data>
<eng-data t="0." f="0." m="2065.28" cg="265.5"/>
<eng-data t="0.053" f="935.855" m="2050.6" cg="265.5"/>
<eng-data t="0.175" f="1292.64" m="1970.12" cg="265.5"/>
<eng-data t="0.3" f="1260.93" m="1875.64" cg="265.5"/>
<eng-data t="0.425" f="1241.48" m="1783.04" cg="265.5"/>
<eng-data t="0.55" f="1257.06" m="1690.6" cg="265.5"/>
<eng-data t="0.675" f="1272.29" m="1597.01" cg="265.5"/>
<eng-data t="0.8" f="1287.61" m="1502.29" cg="265.5"/>
<eng-data t="0.925" f="1301.01" m="1406.51" cg="265.5"/>
<eng-data t="1.048" f="1309.71" m="1311.45" cg="265.5"/>
<eng-data t="1.17" f="1308.42" m="1216.9" cg="265.5"/>
<eng-data t="1.295" f="1304.83" m="1120.21" cg="265.5"/>
<eng-data t="1.42" f="1285.27" m="1024.37" cg="265.5"/>
<eng-data t="1.545" f="1267.66" m="929.913" cg="265.5"/>
<eng-data t="1.67" f="1255.62" m="836.549" cg="265.5"/>
<eng-data t="1.795" f="1227.21" m="744.682" cg="265.5"/>
<eng-data t="1.92" f="1202.44" m="654.783" cg="265.5"/>
<eng-data t="2.043" f="1182.62" m="567.945" cg="265.5"/>
<eng-data t="2.165" f="1150.71" m="483.681" cg="265.5"/>
<eng-data t="2.29" f="1117.91" m="399.74" cg="265.5"/>
<eng-data t="2.415" f="1081.74" m="318.351" cg="265.5"/>
<eng-data t="2.54" f="1037.55" m="239.935" cg="265.5"/>
<eng-data t="2.665" f="1007.09" m="164.281" cg="265.5"/>
<eng-data t="2.79" f="1008.91" m="89.6868" cg="265.5"/>
<eng-data t="2.915" f="643.124" m="28.5598" cg="265.5"/>
<eng-data t="3.04" f="64.371" m="2.38179" cg="265.5"/>
<eng-data t="3.165" f="0." m="0." cg="265.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="L1300R" Type="reloadable" dia="98." len="443."
initWt="4884." propWt="2508." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1301.84" peakThrust="1552.47" throatDia="0." exitDia="0."
Itot="4556.42" burn-time="3.5" massFrac="51.35" Isp="185.26" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="2508." cg="221.5"/>
<eng-data t="0.0231839" f="1299.23" m="2499.71" cg="221.5"/>
<eng-data t="0.502318" f="1332.26" m="2152.71" cg="221.5"/>
<eng-data t="0.996909" f="1497.42" m="1767.53" cg="221.5"/>
<eng-data t="1.49923" f="1552.47" m="1345.9" cg="221.5"/>
<eng-data t="1.99382" f="1508.43" m="929.249" cg="221.5"/>
<eng-data t="2.49614" f="1354.29" m="533.488" cg="221.5"/>
<eng-data t="2.99845" f="1101.05" m="194.053" cg="221.5"/>
<eng-data t="3.12983" f="1090.03" m="114.828" cg="221.5"/>
<eng-data t="3.21484" f="1145.09" m="62.5348" cg="221.5"/>
<eng-data t="3.3694" f="176.167" m="6.33201" cg="221.5"/>
<eng-data t="3.5" f="0." m="0." cg="221.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="L1390G" Type="reloadable" dia="75." len="517.91"
initWt="3876." propWt="1973." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1355.71" peakThrust="1649.83" throatDia="0." exitDia="0."
Itot="3946.48" burn-time="2.91" massFrac="50.9" Isp="203.97" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve
Tracer program. Thrust curve and engine data from Aerotech thrust stand.
</comments>
<data>
<eng-data t="0." f="0." m="1973." cg="298.5"/>
<eng-data t="0.018" f="906.203" m="1968.92" cg="298.5"/>
<eng-data t="0.041" f="1249.41" m="1956.53" cg="298.5"/>
<eng-data t="0.055" f="1336.72" m="1947.48" cg="298.5"/>
<eng-data t="0.099" f="1369.84" m="1917.71" cg="298.5"/>
<eng-data t="0.173" f="1402.96" m="1866.42" cg="298.5"/>
<eng-data t="0.236" f="1411.99" m="1822.09" cg="298.5"/>
<eng-data t="0.284" f="1411.99" m="1788.21" cg="298.5"/>
<eng-data t="0.678" f="1586.61" m="1492.88" cg="298.5"/>
<eng-data t="0.869" f="1649.83" m="1338.36" cg="298.5"/>
<eng-data t="0.939" f="1640.8" m="1280.78" cg="298.5"/>
<eng-data t="1.102" f="1625.74" m="1147.69" cg="298.5"/>
<eng-data t="1.197" f="1628.76" m="1070.4" cg="298.5"/>
<eng-data t="1.293" f="1619.72" m="992.446" cg="298.5"/>
<eng-data t="1.374" f="1607.68" m="927.099" cg="298.5"/>
<eng-data t="1.455" f="1601.66" m="862.118" cg="298.5"/>
<eng-data t="1.518" f="1589.62" m="811.861" cg="298.5"/>
<eng-data t="1.592" f="1550.48" m="753.777" cg="298.5"/>
<eng-data t="1.691" f="1499.3" m="678.304" cg="298.5"/>
<eng-data t="1.838" f="1424.03" m="570.885" cg="298.5"/>
<eng-data t="1.96" f="1366.83" m="485.774" cg="298.5"/>
<eng-data t="2.1" f="1312.64" m="392.004" cg="298.5"/>
<eng-data t="2.225" f="1261.46" m="311.573" cg="298.5"/>
<eng-data t="2.343" f="1228.34" m="238.133" cg="298.5"/>
<eng-data t="2.417" f="1213.29" m="192.968" cg="298.5"/>
<eng-data t="2.479" f="1204.26" m="155.501" cg="298.5"/>
<eng-data t="2.524" f="1198.23" m="128.476" cg="298.5"/>
<eng-data t="2.564" f="1198.23" m="104.514" cg="298.5"/>
<eng-data t="2.601" f="1165.12" m="82.6561" cg="298.5"/>
<eng-data t="2.638" f="1074.8" m="61.9394" cg="298.5"/>
<eng-data t="2.66" f="957.383" m="50.7637" cg="298.5"/>
<eng-data t="2.689" f="839.968" m="37.7345" cg="298.5"/>
<eng-data t="2.712" f="713.522" m="28.8031" cg="298.5"/>
<eng-data t="2.737" f="590.085" m="20.6565" cg="298.5"/>
<eng-data t="2.763" f="427.511" m="14.0429" cg="298.5"/>
<eng-data t="2.8" f="295.043" m="7.36013" cg="298.5"/>
<eng-data t="2.844" f="153.543" m="2.42629" cg="298.5"/>
<eng-data t="2.877" f="69.245" m="0.588511" cg="298.5"/>
<eng-data t="2.911" f="0." m="0." cg="298.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="L1420R" Type="reloadable" dia="75." len="443."
initWt="4562." propWt="2560." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1424.79" peakThrust="1662.58" throatDia="0." exitDia="0."
Itot="4616.31" burn-time="3.24" massFrac="56.12" Isp="183.88" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="2560." cg="221.5"/>
<eng-data t="0.0386399" f="1332.26" m="2545.73" cg="221.5"/>
<eng-data t="0.123648" f="1563.48" m="2477.47" cg="221.5"/>
<eng-data t="0.502318" f="1519.44" m="2153.77" cg="221.5"/>
<eng-data t="0.996909" f="1574.49" m="1729.48" cg="221.5"/>
<eng-data t="1.49923" f="1662.58" m="1278.61" cg="221.5"/>
<eng-data t="2.00155" f="1574.49" m="827.745" cg="221.5"/>
<eng-data t="2.48068" f="1409.34" m="431.337" cg="221.5"/>
<eng-data t="2.92117" f="1299.23" m="100.518" cg="221.5"/>
<eng-data t="2.99073" f="1167.11" m="52.9487" cg="221.5"/>
<eng-data t="3.11437" f="187.178" m="6.52023" cg="221.5"/>
<eng-data t="3.24" f="0." m="0." cg="221.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="L1500T" Type="reloadable" dia="98." len="443."
initWt="4659.2" propWt="2464." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1324.98" peakThrust="1704.29" throatDia="0." exitDia="0."
Itot="5056.11" burn-time="3.82" massFrac="52.88" Isp="209.25" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>AeroTech L1500T
Copyright Tripoli Motor Testing 1998 (www.tripoli.org)
provided by ThrustCurve.org (www.thrustcurve.org)
</comments>
<data>
<eng-data t="0." f="0." m="2464." cg="221.5"/>
<eng-data t="0.073" f="1320.33" m="2440.51" cg="221.5"/>
<eng-data t="0.222" f="1454.82" m="2339.76" cg="221.5"/>
<eng-data t="0.372" f="1508.99" m="2231.43" cg="221.5"/>
<eng-data t="0.522" f="1556.78" m="2119.38" cg="221.5"/>
<eng-data t="0.672" f="1602.41" m="2003.91" cg="221.5"/>
<eng-data t="0.822" f="1642." m="1885.33" cg="221.5"/>
<eng-data t="0.971" f="1670.1" m="1765.08" cg="221.5"/>
<eng-data t="1.12" f="1694.8" m="1642.91" cg="221.5"/>
<eng-data t="1.27" f="1701.3" m="1518.79" cg="221.5"/>
<eng-data t="1.42" f="1704.29" m="1394.31" cg="221.5"/>
<eng-data t="1.57" f="1701.01" m="1269.85" cg="221.5"/>
<eng-data t="1.72" f="1694.55" m="1145.74" cg="221.5"/>
<eng-data t="1.869" f="1683.86" m="1023.09" cg="221.5"/>
<eng-data t="2.018" f="1659.69" m="901.693" cg="221.5"/>
<eng-data t="2.168" f="1620.16" m="781.815" cg="221.5"/>
<eng-data t="2.318" f="1570.03" m="665.214" cg="221.5"/>
<eng-data t="2.468" f="1517.93" m="552.35" cg="221.5"/>
<eng-data t="2.618" f="1463.32" m="443.385" cg="221.5"/>
<eng-data t="2.767" f="1400.99" m="339.393" cg="221.5"/>
<eng-data t="2.916" f="1331.42" m="240.19" cg="221.5"/>
<eng-data t="3.066" f="1279.48" m="144.762" cg="221.5"/>
<eng-data t="3.216" f="1108.99" m="57.464" cg="221.5"/>
<eng-data t="3.366" f="217.788" m="8.97064" cg="221.5"/>
<eng-data t="3.516" f="10.579" m="0.623869" cg="221.5"/>
<eng-data t="3.666" f="3.245" m="0.118604" cg="221.5"/>
<eng-data t="3.816" f="0." m="0." cg="221.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="L1520T" Type="reloadable" dia="75." len="531."
initWt="3620." propWt="1773." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1449.61" peakThrust="1696.63" throatDia="0." exitDia="0." Itot="3769."
burn-time="2.6" massFrac="48.98" Isp="216.77" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Based on AT Instruction Sheet by C. Kobel 12/22/2010</comments>
<data>
<eng-data t="0." f="0." m="1773." cg="265.5"/>
<eng-data t="0.011" f="1484.55" m="1769.16" cg="265.5"/>
<eng-data t="0.055" f="1506.3" m="1738.21" cg="265.5"/>
<eng-data t="0.089" f="1468.24" m="1714.42" cg="265.5"/>
<eng-data t="0.155" f="1560.68" m="1667.4" cg="265.5"/>
<eng-data t="0.2" f="1571.56" m="1634.25" cg="265.5"/>
<eng-data t="0.3" f="1582.43" m="1560.06" cg="265.5"/>
<eng-data t="0.4" f="1598.75" m="1485.24" cg="265.5"/>
<eng-data t="0.5" f="1620.5" m="1409.52" cg="265.5"/>
<eng-data t="0.6" f="1642.25" m="1332.77" cg="265.5"/>
<eng-data t="0.7" f="1653.13" m="1255.26" cg="265.5"/>
<eng-data t="0.8" f="1674.88" m="1176.99" cg="265.5"/>
<eng-data t="0.9" f="1691.19" m="1097.81" cg="265.5"/>
<eng-data t="1." f="1685.76" m="1018.38" cg="265.5"/>
<eng-data t="1.1" f="1696.63" m="938.828" cg="265.5"/>
<eng-data t="1.2" f="1691.19" m="859.144" cg="265.5"/>
<eng-data t="1.3" f="1691.19" m="779.587" cg="265.5"/>
<eng-data t="1.4" f="1680.32" m="700.286" cg="265.5"/>
<eng-data t="1.5" f="1664." m="621.625" cg="265.5"/>
<eng-data t="1.6" f="1636.81" m="543.987" cg="265.5"/>
<eng-data t="1.7" f="1620.5" m="467.372" cg="265.5"/>
<eng-data t="1.8" f="1604.19" m="391.525" cg="265.5"/>
<eng-data t="1.9" f="1577." m="316.701" cg="265.5"/>
<eng-data t="2." f="1560.68" m="242.9" cg="265.5"/>
<eng-data t="2.1" f="1538.93" m="169.994" cg="265.5"/>
<eng-data t="2.2" f="1500.87" m="98.4954" cg="265.5"/>
<eng-data t="2.227" f="1435.61" m="79.847" cg="265.5"/>
<eng-data t="2.25" f="1125.65" m="65.9911" cg="265.5"/>
<eng-data t="2.29" f="832.002" m="47.5728" cg="265.5"/>
<eng-data t="2.366" f="647.113" m="21.1324" cg="265.5"/>
<eng-data t="2.4" f="456.785" m="12.3044" cg="265.5"/>
<eng-data t="2.44" f="244.706" m="5.70453" cg="265.5"/>
<eng-data t="2.5" f="59.817" m="1.40695" cg="265.5"/>
<eng-data t="2.6" f="0." m="0." cg="265.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="L2200G" Type="reloadable" dia="75." len="665."
initWt="4751." propWt="2516." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="2126.72" peakThrust="3101.77" throatDia="0." exitDia="0."
Itot="5104.13" burn-time="2.4" massFrac="52.96" Isp="206.87" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Curvefit of Aerotech Instructions by C. Kobel 11/19/08</comments>
<data>
<eng-data t="0." f="0." m="2516." cg="332.5"/>
<eng-data t="0.011" f="1195.18" m="2512.76" cg="332.5"/>
<eng-data t="0.024" f="2029.9" m="2502.43" cg="332.5"/>
<eng-data t="0.037" f="2380.87" m="2488.29" cg="332.5"/>
<eng-data t="0.05" f="2542.12" m="2472.52" cg="332.5"/>
<eng-data t="0.1" f="2570.58" m="2409.51" cg="332.5"/>
<eng-data t="0.15" f="2561.09" m="2346.28" cg="332.5"/>
<eng-data t="0.2" f="2523.15" m="2283.62" cg="332.5"/>
<eng-data t="0.25" f="2485.21" m="2221.9" cg="332.5"/>
<eng-data t="0.3" f="2523.15" m="2160.18" cg="332.5"/>
<eng-data t="0.35" f="2570.58" m="2097.41" cg="332.5"/>
<eng-data t="0.4" f="2674.92" m="2032.77" cg="332.5"/>
<eng-data t="0.5" f="2912.06" m="1895.07" cg="332.5"/>
<eng-data t="0.6" f="3073.31" m="1747.55" cg="332.5"/>
<eng-data t="0.7" f="3073.31" m="1596.05" cg="332.5"/>
<eng-data t="0.8" f="3101.77" m="1443.86" cg="332.5"/>
<eng-data t="0.9" f="3092.28" m="1291.2" cg="332.5"/>
<eng-data t="1." f="3092.28" m="1138.77" cg="332.5"/>
<eng-data t="1.1" f="2959.49" m="989.61" cg="332.5"/>
<eng-data t="1.186" f="2807.72" m="867.368" cg="332.5"/>
<eng-data t="1.227" f="2437.78" m="814.361" cg="332.5"/>
<eng-data t="1.27" f="2257.56" m="764.6" cg="332.5"/>
<eng-data t="1.3" f="2162.7" m="731.916" cg="332.5"/>
<eng-data t="1.4" f="1991.96" m="629.518" cg="332.5"/>
<eng-data t="1.5" f="1878.13" m="534.133" cg="332.5"/>
<eng-data t="1.6" f="1792.77" m="443.657" cg="332.5"/>
<eng-data t="1.7" f="1688.42" m="357.858" cg="332.5"/>
<eng-data t="1.8" f="1612.54" m="276.5" cg="332.5"/>
<eng-data t="1.9" f="1584.08" m="197.714" cg="332.5"/>
<eng-data t="2." f="1536.66" m="120.798" cg="332.5"/>
<eng-data t="2.048" f="1498.71" m="84.888" cg="332.5"/>
<eng-data t="2.084" f="1403.86" m="59.134" cg="332.5"/>
<eng-data t="2.102" f="1166.72" m="47.7299" cg="332.5"/>
<eng-data t="2.134" f="796.784" m="32.2439" cg="332.5"/>
<eng-data t="2.186" f="455.305" m="16.1967" cg="332.5"/>
<eng-data t="2.237" f="237.138" m="7.49285" cg="332.5"/>
<eng-data t="2.3" f="94.855" m="2.33786" cg="332.5"/>
<eng-data t="2.4" f="0." m="0." cg="332.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="L875DM" Type="single-use" dia="75." len="638."
initWt="4581." propWt="2472." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="814.57" peakThrust="1038.62" throatDia="0." exitDia="0." Itot="3779.6"
burn-time="4.64" massFrac="53.96" Isp="155.91" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>L875 Dark Matter DMS</comments>
<data>
<eng-data t="0." f="0." m="2472." cg="319."/>
<eng-data t="0.023" f="444.123" m="2468.66" cg="319."/>
<eng-data t="0.028" f="853.275" m="2466.54" cg="319."/>
<eng-data t="0.074" f="814.808" m="2441.45" cg="319."/>
<eng-data t="0.148" f="793.825" m="2402.52" cg="319."/>
<eng-data t="0.158" f="874.257" m="2397.06" cg="319."/>
<eng-data t="0.241" f="902.233" m="2348.84" cg="319."/>
<eng-data t="0.287" f="928.461" m="2321.31" cg="319."/>
<eng-data t="0.422" f="910.976" m="2240.1" cg="319."/>
<eng-data t="0.528" f="903.982" m="2177.19" cg="319."/>
<eng-data t="0.992" f="917.97" m="1900.73" cg="319."/>
<eng-data t="1.497" f="956.437" m="1591.18" cg="319."/>
<eng-data t="2.007" f="1000.15" m="1264.86" cg="319."/>
<eng-data t="2.489" f="1033.37" m="944.333" cg="319."/>
<eng-data t="2.619" f="1038.62" m="856.248" cg="319."/>
<eng-data t="2.827" f="1031.62" m="715.431" cg="319."/>
<eng-data t="3.115" f="989.659" m="525.064" cg="319."/>
<eng-data t="3.495" f="912.724" m="288.66" cg="319."/>
<eng-data t="3.606" f="907.479" m="222.589" cg="319."/>
<eng-data t="3.843" f="671.429" m="100.218" cg="319."/>
<eng-data t="3.935" f="606.734" m="61.7637" cg="319."/>
<eng-data t="4." f="442.374" m="39.4636" cg="319."/>
<eng-data t="4.097" f="220.313" m="18.4427" cg="319."/>
<eng-data t="4.195" f="103.162" m="8.076" cg="319."/>
<eng-data t="4.315" f="31.473" m="2.79263" cg="319."/>
<eng-data t="4.478" f="10.491" m="0.555781" cg="319."/>
<eng-data t="4.64" f="0." m="0." cg="319."/>
</data>
</engine>
<engine mfg="Aerotech" code="L900DM" Type="reloadable" dia="75." len="665.5"
initWt="4724." propWt="2472." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="861.541" peakThrust="1054.59" throatDia="0." exitDia="0."
Itot="3863.15" burn-time="4.48" massFrac="52.33" Isp="159.36" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>L900 Dark Matter</comments>
<data>
<eng-data t="0." f="0." m="2472." cg="332.75"/>
<eng-data t="0.016" f="577.998" m="2469.04" cg="332.75"/>
<eng-data t="0.041" f="870.377" m="2457.46" cg="332.75"/>
<eng-data t="0.086" f="851.787" m="2432.66" cg="332.75"/>
<eng-data t="0.303" f="931.219" m="2308.87" cg="332.75"/>
<eng-data t="0.417" f="944.74" m="2240.45" cg="332.75"/>
<eng-data t="0.515" f="910.939" m="2182.26" cg="332.75"/>
<eng-data t="0.998" f="936.289" m="1896.8" cg="332.75"/>
<eng-data t="1.272" f="976.851" m="1729.09" cg="332.75"/>
<eng-data t="1.501" f="992.061" m="1584.83" cg="332.75"/>
<eng-data t="1.747" f="1019.1" m="1426.54" cg="332.75"/>
<eng-data t="2." f="1029.24" m="1260.73" cg="332.75"/>
<eng-data t="2.205" f="1054.59" m="1124.05" cg="332.75"/>
<eng-data t="2.495" f="1047.83" m="928.983" cg="332.75"/>
<eng-data t="2.77" f="1034.31" m="745.785" cg="332.75"/>
<eng-data t="3.003" f="998.821" m="594.22" cg="332.75"/>
<eng-data t="3.166" f="981.921" m="490.922" cg="332.75"/>
<eng-data t="3.498" f="909.249" m="290.038" cg="332.75"/>
<eng-data t="3.592" f="880.518" m="236.211" cg="332.75"/>
<eng-data t="3.702" f="890.658" m="173.876" cg="332.75"/>
<eng-data t="3.768" f="856.857" m="136.975" cg="332.75"/>
<eng-data t="3.862" f="672.641" m="90.975" cg="332.75"/>
<eng-data t="3.964" f="442.794" m="54.5733" cg="332.75"/>
<eng-data t="4.021" f="353.221" m="40.0564" cg="332.75"/>
<eng-data t="4.111" f="285.619" m="21.661" cg="332.75"/>
<eng-data t="4.242" f="104.783" m="5.29806" cg="332.75"/>
<eng-data t="4.3" f="50.702" m="2.41275" cg="332.75"/>
<eng-data t="4.369" f="21.971" m="0.808396" cg="332.75"/>
<eng-data t="4.484" f="0." m="0." cg="332.75"/>
</data>
</engine>
<engine mfg="Aerotech" code="L1040DM" Type="reloadable" dia="75." len="681."
initWt="4717." propWt="2602." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="938.105" peakThrust="1268.42" throatDia="0." exitDia="0."
Itot="3871.56" burn-time="4.13" massFrac="55.16" Isp="151.73" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>L1040 Dark Matter</comments>
<data>
<eng-data t="0." f="0." m="2602." cg="340.5"/>
<eng-data t="0.018" f="1126.17" m="2595.19" cg="340.5"/>
<eng-data t="0.042" f="1036.41" m="2577.75" cg="340.5"/>
<eng-data t="0.053" f="1002.54" m="2570.21" cg="340.5"/>
<eng-data t="0.116" f="988.995" m="2528.05" cg="340.5"/>
<eng-data t="0.504" f="1049.96" m="2262.2" cg="340.5"/>
<eng-data t="0.794" f="1095.68" m="2053.1" cg="340.5"/>
<eng-data t="1.002" f="1146.49" m="1896.38" cg="340.5"/>
<eng-data t="1.252" f="1192.21" m="1699.91" cg="340.5"/>
<eng-data t="1.499" f="1237.94" m="1498.2" cg="340.5"/>
<eng-data t="1.753" f="1261.65" m="1284.85" cg="340.5"/>
<eng-data t="1.912" f="1268.42" m="1149.67" cg="340.5"/>
<eng-data t="2.095" f="1254.87" m="994.5" cg="340.5"/>
<eng-data t="2.511" f="1134.63" m="660.464" cg="340.5"/>
<eng-data t="2.772" f="1056.73" m="468.266" cg="340.5"/>
<eng-data t="3.012" f="966.98" m="305.054" cg="340.5"/>
<eng-data t="3.153" f="933.11" m="215.025" cg="340.5"/>
<eng-data t="3.217" f="863.677" m="176.382" cg="340.5"/>
<eng-data t="3.291" f="817.953" m="134.565" cg="340.5"/>
<eng-data t="3.34" f="758.681" m="108.604" cg="340.5"/>
<eng-data t="3.488" f="438.613" m="49.058" cg="340.5"/>
<eng-data t="3.552" f="284.505" m="33.5062" cg="340.5"/>
<eng-data t="3.598" f="220.153" m="25.7053" cg="340.5"/>
<eng-data t="3.657" f="167.655" m="18.0165" cg="340.5"/>
<eng-data t="3.746" f="118.544" m="9.45696" cg="340.5"/>
<eng-data t="3.88" f="42.337" m="2.21258" cg="340.5"/>
<eng-data t="3.996" f="6.774" m="0.2982" cg="340.5"/>
<eng-data t="4.127" f="0." m="0." cg="340.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="L1170FJ" Type="reloadable" dia="75." len="665."
initWt="4990." propWt="2800." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1136.94" peakThrust="1465.3" throatDia="0." exitDia="0." Itot="4222.6"
burn-time="3.71" massFrac="56.11" Isp="153.78" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Entered by Tim Van Milligan for RockSim Users. Used John
Coker's ThrustCurve Tracer software and TRA cert paperwork dated 10-14-08.
</comments>
<data>
<eng-data t="0." f="0." m="2800." cg="332.5"/>
<eng-data t="0.036" f="891.737" m="2789.36" cg="332.5"/>
<eng-data t="0.05" f="1260.15" m="2779.37" cg="332.5"/>
<eng-data t="0.064" f="1461.11" m="2766.74" cg="332.5"/>
<eng-data t="0.077" f="1327.14" m="2754.72" cg="332.5"/>
<eng-data t="0.118" f="1327.14" m="2718.64" cg="332.5"/>
<eng-data t="0.123" f="1465.3" m="2714.01" cg="332.5"/>
<eng-data t="0.141" f="1389.94" m="2696.97" cg="332.5"/>
<eng-data t="0.205" f="1335.51" m="2639.14" cg="332.5"/>
<eng-data t="0.25" f="1318.77" m="2599.54" cg="332.5"/>
<eng-data t="0.332" f="1306.21" m="2528.17" cg="332.5"/>
<eng-data t="0.409" f="1297.83" m="2461.69" cg="332.5"/>
<eng-data t="0.505" f="1318.77" m="2378.41" cg="332.5"/>
<eng-data t="0.564" f="1331.33" m="2326.57" cg="332.5"/>
<eng-data t="0.636" f="1318.77" m="2263.31" cg="332.5"/>
<eng-data t="0.736" f="1331.33" m="2175.44" cg="332.5"/>
<eng-data t="0.855" f="1356.44" m="2069.4" cg="332.5"/>
<eng-data t="0.923" f="1364.82" m="2008.05" cg="332.5"/>
<eng-data t="1." f="1356.44" m="1938.58" cg="332.5"/>
<eng-data t="1.082" f="1377.38" m="1864.25" cg="332.5"/>
<eng-data t="1.136" f="1385.75" m="1814.78" cg="332.5"/>
<eng-data t="1.186" f="1385.75" m="1768.84" cg="332.5"/>
<eng-data t="1.236" f="1406.68" m="1722.54" cg="332.5"/>
<eng-data t="1.323" f="1402.5" m="1641.51" cg="332.5"/>
<eng-data t="1.441" f="1423.43" m="1530.96" cg="332.5"/>
<eng-data t="1.514" f="1423.43" m="1462.05" cg="332.5"/>
<eng-data t="1.645" f="1427.62" m="1338.22" cg="332.5"/>
<eng-data t="1.768" f="1435.99" m="1221.44" cg="332.5"/>
<eng-data t="1.873" f="1423.43" m="1121.9" cg="332.5"/>
<eng-data t="2.005" f="1410.87" m="997.859" cg="332.5"/>
<eng-data t="2.164" f="1389.94" m="850.21" cg="332.5"/>
<eng-data t="2.314" f="1356.44" m="713.626" cg="332.5"/>
<eng-data t="2.427" f="1327.14" m="613.085" cg="332.5"/>
<eng-data t="2.595" f="1264.34" m="468.739" cg="332.5"/>
<eng-data t="2.705" f="1218.29" m="378.197" cg="332.5"/>
<eng-data t="2.805" f="1184.8" m="298.523" cg="332.5"/>
<eng-data t="2.864" f="1172.24" m="252.416" cg="332.5"/>
<eng-data t="2.905" f="1172.24" m="220.546" cg="332.5"/>
<eng-data t="2.941" f="1159.68" m="192.713" cg="332.5"/>
<eng-data t="2.968" f="1126.18" m="172.25" cg="332.5"/>
<eng-data t="3.009" f="1038.27" m="142.828" cg="332.5"/>
<eng-data t="3.064" f="862.431" m="108.168" cg="332.5"/>
<eng-data t="3.105" f="694.969" m="86.9975" cg="332.5"/>
<eng-data t="3.15" f="573.559" m="68.0714" cg="332.5"/>
<eng-data t="3.218" f="439.589" m="45.2296" cg="332.5"/>
<eng-data t="3.295" f="297.246" m="26.4188" cg="332.5"/>
<eng-data t="3.355" f="217.701" m="16.1749" cg="332.5"/>
<eng-data t="3.409" f="142.343" m="9.72884" cg="332.5"/>
<eng-data t="3.45" f="100.477" m="6.42806" cg="332.5"/>
<eng-data t="3.495" f="58.612" m="4.0545" cg="332.5"/>
<eng-data t="3.559" f="37.679" m="2.01128" cg="332.5"/>
<eng-data t="3.618" f="25.119" m="0.782865" cg="332.5"/>
<eng-data t="3.664" f="12.56" m="0.208213" cg="332.5"/>
<eng-data t="3.714" f="0." m="0." cg="332.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="L1256WS" Type="reloadable" dia="75." len="561."
initWt="3756." propWt="1964." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1230.13" peakThrust="1469.66" throatDia="0." exitDia="0."
Itot="3762.97" burn-time="3.06" massFrac="52.29" Isp="195.37" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="1964." cg="280.5"/>
<eng-data t="0.017" f="13.8651" m="1963.94" cg="280.5"/>
<eng-data t="0.045" f="1220." m="1954.92" cg="280.5"/>
<eng-data t="0.19" f="1400.24" m="1855.77" cg="280.5"/>
<eng-data t="0.465" f="1439.08" m="1652.01" cg="280.5"/>
<eng-data t="0.77" f="1469.66" m="1420.49" cg="280.5"/>
<eng-data t="1.076" f="1466.08" m="1186.06" cg="280.5"/>
<eng-data t="1.381" f="1445.4" m="954.32" cg="280.5"/>
<eng-data t="1.723" f="1340.96" m="705.638" cg="280.5"/>
<eng-data t="2.029" f="1231.09" m="500.247" cg="280.5"/>
<eng-data t="2.485" f="1098.46" m="223.033" cg="280.5"/>
<eng-data t="2.71" f="1064.1" m="96.0542" cg="280.5"/>
<eng-data t="2.788" f="829.729" m="57.5049" cg="280.5"/>
<eng-data t="2.939" f="376.032" m="9.99119" cg="280.5"/>
<eng-data t="3.023" f="55.7705" m="0.525652" cg="280.5"/>
<eng-data t="3.041" f="28.0667" m="0.131839" cg="280.5"/>
<eng-data t="3.059" f="0." m="0." cg="280.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="L2500ST" Type="reloadable" dia="98." len="443."
initWt="4989.49" propWt="2313.31" delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="2429.51" peakThrust="2822.15" throatDia="0."
exitDia="0." Itot="4671.95" burn-time="1.92" massFrac="46.36" Isp="205.94"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="2313.31" cg="221.5"/>
<eng-data t="0.016" f="24.712" m="2313.21" cg="221.5"/>
<eng-data t="0.027" f="449.764" m="2311.92" cg="221.5"/>
<eng-data t="0.03" f="1329.52" m="2310.6" cg="221.5"/>
<eng-data t="0.039" f="1784.23" m="2303.66" cg="221.5"/>
<eng-data t="0.043" f="2041.24" m="2299.87" cg="221.5"/>
<eng-data t="0.08" f="2224.11" m="2260.8" cg="221.5"/>
<eng-data t="0.118" f="2357.56" m="2217.7" cg="221.5"/>
<eng-data t="0.198" f="2476.18" m="2121.96" cg="221.5"/>
<eng-data t="0.399" f="2678.82" m="1865.43" cg="221.5"/>
<eng-data t="0.495" f="2748.01" m="1736.45" cg="221.5"/>
<eng-data t="0.601" f="2787.55" m="1591.18" cg="221.5"/>
<eng-data t="0.701" f="2822.15" m="1452.3" cg="221.5"/>
<eng-data t="0.799" f="2822.15" m="1315.36" cg="221.5"/>
<eng-data t="1.001" f="2807.32" m="1033.83" cg="221.5"/>
<eng-data t="1.199" f="2757.9" m="761.024" cg="221.5"/>
<eng-data t="1.399" f="2668.93" m="492.316" cg="221.5"/>
<eng-data t="1.501" f="2565.14" m="360.142" cg="221.5"/>
<eng-data t="1.6" f="2402.04" m="238.397" cg="221.5"/>
<eng-data t="1.675" f="2233.99" m="152.315" cg="221.5"/>
<eng-data t="1.752" f="2006.64" m="71.4746" cg="221.5"/>
<eng-data t="1.777" f="1818.83" m="47.7974" cg="221.5"/>
<eng-data t="1.805" f="1334.47" m="25.9385" cg="221.5"/>
<eng-data t="1.827" f="884.702" m="13.8515" cg="221.5"/>
<eng-data t="1.852" f="434.937" m="5.68375" cg="221.5"/>
<eng-data t="1.87" f="242.181" m="2.66628" cg="221.5"/>
<eng-data t="1.895" f="88.964" m="0.616706" cg="221.5"/>
<eng-data t="1.923" f="0." m="0." cg="221.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="M650W" Type="reloadable" dia="75." len="801."
initWt="5125." propWt="3351." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="522.259" peakThrust="1328." throatDia="0." exitDia="0." Itot="6005.98"
burn-time="11.5" massFrac="65.39" Isp="182.76" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>75-6400 case
Greg Gardner - 10/25/07
</comments>
<data>
<eng-data t="0." f="0." m="3351." cg="400.5"/>
<eng-data t="0.08" f="1240." m="3323.33" cg="400.5"/>
<eng-data t="0.12" f="1328." m="3294.67" cg="400.5"/>
<eng-data t="0.25" f="1230." m="3201.9" cg="400.5"/>
<eng-data t="0.5" f="1142." m="3036.47" cg="400.5"/>
<eng-data t="1." f="1071." m="2727.79" cg="400.5"/>
<eng-data t="1.5" f="1048." m="2432.22" cg="400.5"/>
<eng-data t="2." f="1018." m="2144.04" cg="400.5"/>
<eng-data t="2.5" f="982." m="1865.07" cg="400.5"/>
<eng-data t="3." f="950." m="1595.58" cg="400.5"/>
<eng-data t="3.5" f="853." m="1344.09" cg="400.5"/>
<eng-data t="4." f="781." m="1116.17" cg="400.5"/>
<eng-data t="5." f="595." m="732.301" cg="400.5"/>
<eng-data t="6." f="443." m="442.728" cg="400.5"/>
<eng-data t="7." f="297." m="236.289" cg="400.5"/>
<eng-data t="8." f="155." m="110.194" cg="400.5"/>
<eng-data t="9." f="88." m="42.4037" cg="400.5"/>
<eng-data t="10." f="32." m="8.9271" cg="400.5"/>
<eng-data t="10.5" f="12." m="2.78972" cg="400.5"/>
<eng-data t="11." f="4." m="0.557944" cg="400.5"/>
<eng-data t="11.5" f="0." m="0." cg="400.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="M685W" Type="reloadable" dia="75." len="935."
initWt="7008." propWt="4320." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="630.119" peakThrust="1380.01" throatDia="0." exitDia="0."
Itot="7557.65" burn-time="11.99" massFrac="61.64" Isp="178.39" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>M685W-PS Moonburner</comments>
<data>
<eng-data t="0." f="0." m="4320." cg="400.5"/>
<eng-data t="0.083" f="1333.47" m="4288.37" cg="400.5"/>
<eng-data t="0.13" f="1368.38" m="4252.07" cg="400.5"/>
<eng-data t="0.249" f="1361.39" m="4159.23" cg="400.5"/>
<eng-data t="0.308" f="1380.01" m="4113.01" cg="400.5"/>
<eng-data t="0.403" f="1359.07" m="4038.64" cg="400.5"/>
<eng-data t="0.675" f="1184.53" m="3840.9" cg="400.5"/>
<eng-data t="1.018" f="1072.83" m="3619.61" cg="400.5"/>
<eng-data t="1.456" f="996.029" m="3360.63" cg="400.5"/>
<eng-data t="1.977" f="958.794" m="3069.55" cg="400.5"/>
<eng-data t="2.995" f="914.578" m="2524.5" cg="400.5"/>
<eng-data t="3.99" f="856.399" m="2020.88" cg="400.5"/>
<eng-data t="4.985" f="781.929" m="1554.98" cg="400.5"/>
<eng-data t="5.494" f="730.732" m="1334.92" cg="400.5"/>
<eng-data t="5.991" f="679.534" m="1134.6" cg="400.5"/>
<eng-data t="7.258" f="542.231" m="692.188" cg="400.5"/>
<eng-data t="7.862" f="463.107" m="518.642" cg="400.5"/>
<eng-data t="8.015" f="456.125" m="478.445" cg="400.5"/>
<eng-data t="8.998" f="330.458" m="257.459" cg="400.5"/>
<eng-data t="9.993" f="207.118" m="104.586" cg="400.5"/>
<eng-data t="10.514" f="137.303" m="53.301" cg="400.5"/>
<eng-data t="11.496" f="34.908" m="4.96846" cg="400.5"/>
<eng-data t="11.994" f="0." m="0." cg="400.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="M750W" Type="reloadable" dia="98." len="732."
initWt="8776." propWt="5300." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="578.494" peakThrust="1218." throatDia="0." exitDia="0." Itot="9255.91"
burn-time="16." massFrac="60.39" Isp="178.08" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>98-10240 case
Greg Gardner - 10/25/07
</comments>
<data>
<eng-data t="0." f="0." m="5300." cg="366."/>
<eng-data t="0.1" f="1032." m="5270.45" cg="366."/>
<eng-data t="0.2" f="992." m="5212.51" cg="366."/>
<eng-data t="0.3" f="974." m="5156.22" cg="366."/>
<eng-data t="0.48" f="966." m="5056.24" cg="366."/>
<eng-data t="1." f="1055." m="4755.36" cg="366."/>
<eng-data t="1.5" f="1152." m="4439.42" cg="366."/>
<eng-data t="2." f="1192." m="4103.88" cg="366."/>
<eng-data t="2.5" f="1218." m="3758.88" cg="366."/>
<eng-data t="4." f="1103." m="2762.11" cg="366."/>
<eng-data t="6." f="818." m="1662.14" cg="366."/>
<eng-data t="8." f="561." m="872.51" cg="366."/>
<eng-data t="10." f="318." m="369.188" cg="366."/>
<eng-data t="11." f="216." m="216.302" cg="366."/>
<eng-data t="12." f="125." m="118.673" cg="366."/>
<eng-data t="13." f="76." m="61.1258" cg="366."/>
<eng-data t="14." f="47." m="25.9105" cg="366."/>
<eng-data t="15." f="23." m="5.86922" cg="366."/>
<eng-data t="15.5" f="9." m="1.28837" cg="366."/>
<eng-data t="16." f="0." m="0." cg="366."/>
</data>
</engine>
<engine mfg="Aerotech" code="M1297W" Type="reloadable" dia="75." len="665.48"
initWt="4636.8" propWt="2721.6" delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1304.33" peakThrust="2047.83" throatDia="0." exitDia="0."
Itot="5439.04" burn-time="4.17" massFrac="58.7" Isp="203.79" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="2721.6" cg="332.74"/>
<eng-data t="0.03" f="2047.83" m="2706.23" cg="332.74"/>
<eng-data t="0.08" f="1891.3" m="2656.95" cg="332.74"/>
<eng-data t="0.5" f="1734.78" m="2275.92" cg="332.74"/>
<eng-data t="1." f="1669.57" m="1850.05" cg="332.74"/>
<eng-data t="1.5" f="1650." m="1434.79" cg="332.74"/>
<eng-data t="2." f="1558.7" m="1033.4" cg="332.74"/>
<eng-data t="2.5" f="1336.96" m="671.162" cg="332.74"/>
<eng-data t="3." f="1115.22" m="364.405" cg="332.74"/>
<eng-data t="3.37" f="1069.57" m="162.157" cg="332.74"/>
<eng-data t="3.52" f="710.87" m="95.3393" cg="332.74"/>
<eng-data t="3.6" f="489.13" m="71.321" cg="332.74"/>
<eng-data t="3.97" f="182.61" m="9.13748" cg="332.74"/>
<eng-data t="4.17" f="0." m="0." cg="332.74"/>
</data>
</engine>
<engine mfg="Aerotech" code="M1305M" Type="unspecified" dia="98." len="597."
initWt="7098." propWt="4080." delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1207.16" peakThrust="1927.67" throatDia="0." exitDia="0."
Itot="6889.26" burn-time="5.71" massFrac="57.48" Isp="172.18" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>M1305 Metalstorm</comments>
<data>
<eng-data t="0." f="0." m="4080." cg="298.5"/>
<eng-data t="0.016" f="1288.08" m="4073.9" cg="298.5"/>
<eng-data t="0.043" f="1462.78" m="4051.9" cg="298.5"/>
<eng-data t="0.08" f="1370.99" m="4020.86" cg="298.5"/>
<eng-data t="0.407" f="1622.68" m="3730.98" cg="298.5"/>
<eng-data t="0.535" f="1640.45" m="3607.3" cg="298.5"/>
<eng-data t="0.787" f="1705.59" m="3357.62" cg="298.5"/>
<eng-data t="0.985" f="1693.74" m="3158.32" cg="298.5"/>
<eng-data t="1.13" f="1717.43" m="3011.85" cg="298.5"/>
<eng-data t="1.328" f="1693.74" m="2811.85" cg="298.5"/>
<eng-data t="1.349" f="1927.67" m="2789.33" cg="298.5"/>
<eng-data t="1.397" f="1726.32" m="2737.4" cg="298.5"/>
<eng-data t="1.751" f="1711.51" m="2377.03" cg="298.5"/>
<eng-data t="2.018" f="1687.82" m="2108.27" cg="298.5"/>
<eng-data t="2.275" f="1690.78" m="1851.16" cg="298.5"/>
<eng-data t="2.297" f="1892.14" m="1827.82" cg="298.5"/>
<eng-data t="2.318" f="1678.94" m="1805.61" cg="298.5"/>
<eng-data t="2.929" f="1412.44" m="1246.3" cg="298.5"/>
<eng-data t="3.748" f="1113.37" m="633.75" cg="298.5"/>
<eng-data t="4.24" f="906.095" m="339.539" cg="298.5"/>
<eng-data t="4.503" f="802.456" m="206.481" cg="298.5"/>
<eng-data t="4.717" f="663.285" m="113.6" cg="298.5"/>
<eng-data t="4.813" f="538.919" m="79.4249" cg="298.5"/>
<eng-data t="4.92" f="387.903" m="50.0594" cg="298.5"/>
<eng-data t="5.027" f="245.771" m="29.982" cg="298.5"/>
<eng-data t="5.166" f="145.094" m="13.8941" cg="298.5"/>
<eng-data t="5.263" f="79.95" m="7.4302" cg="298.5"/>
<eng-data t="5.386" f="32.572" m="3.33193" cg="298.5"/>
<eng-data t="5.498" f="23.689" m="1.46606" cg="298.5"/>
<eng-data t="5.707" f="0." m="0." cg="298.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="M1315W" Type="reloadable" dia="75." len="801."
initWt="5644.8" propWt="3449.6" delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1117.05" peakThrust="1728.68" throatDia="0." exitDia="0."
Itot="6645.35" burn-time="5.95" massFrac="61.11" Isp="196.44" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="3449.6" cg="400.5"/>
<eng-data t="0.116" f="1728.68" m="3397.55" cg="400.5"/>
<eng-data t="0.349" f="1673.34" m="3191.82" cg="400.5"/>
<eng-data t="0.582" f="1686.81" m="2988.61" cg="400.5"/>
<eng-data t="0.816" f="1696.07" m="2783.15" cg="400.5"/>
<eng-data t="1.049" f="1663.17" m="2580." cg="400.5"/>
<eng-data t="1.282" f="1631.24" m="2380.77" cg="400.5"/>
<eng-data t="1.516" f="1620.47" m="2183.28" cg="400.5"/>
<eng-data t="1.749" f="1619.7" m="1987.33" cg="400.5"/>
<eng-data t="1.982" f="1621.04" m="1791.35" cg="400.5"/>
<eng-data t="2.216" f="1615.32" m="1594.79" cg="400.5"/>
<eng-data t="2.449" f="1567.09" m="1402.33" cg="400.5"/>
<eng-data t="2.682" f="1493.72" m="1217.23" cg="400.5"/>
<eng-data t="2.916" f="1420.08" m="1040.26" cg="400.5"/>
<eng-data t="3.149" f="1358.66" m="872.214" cg="400.5"/>
<eng-data t="3.382" f="1292.51" m="711.884" cg="400.5"/>
<eng-data t="3.616" f="1224.81" m="558.995" cg="400.5"/>
<eng-data t="3.849" f="1171.99" m="414.049" cg="400.5"/>
<eng-data t="4.082" f="928.809" m="287.003" cg="400.5"/>
<eng-data t="4.316" f="577.949" m="195.49" cg="400.5"/>
<eng-data t="4.549" f="395.445" m="136.624" cg="400.5"/>
<eng-data t="4.782" f="314.006" m="93.7198" cg="400.5"/>
<eng-data t="5.016" f="228.273" m="60.7847" cg="400.5"/>
<eng-data t="5.249" f="159.803" m="37.3157" cg="400.5"/>
<eng-data t="5.482" f="118.348" m="20.4945" cg="400.5"/>
<eng-data t="5.716" f="109.782" m="6.63908" cg="400.5"/>
<eng-data t="5.949" f="0." m="0." cg="400.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="M1340W" Type="single-use" dia="98." len="557."
initWt="6998." propWt="4036." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1306.49" peakThrust="1891.73" throatDia="0." exitDia="0."
Itot="7371.22" burn-time="5.64" massFrac="57.67" Isp="186.24" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>98 White Lightning DMS</comments>
<data>
<eng-data t="0." f="0." m="4036." cg="278.5"/>
<eng-data t="0.016" f="42.431" m="4035.81" cg="278.5"/>
<eng-data t="0.027" f="1053.71" m="4032.51" cg="278.5"/>
<eng-data t="0.043" f="862.771" m="4024.12" cg="278.5"/>
<eng-data t="0.076" f="1329.52" m="4004.31" cg="278.5"/>
<eng-data t="0.098" f="1403.77" m="3987.85" cg="278.5"/>
<eng-data t="0.152" f="1424.99" m="3946.03" cg="278.5"/>
<eng-data t="0.986" f="1729.08" m="3225.89" cg="278.5"/>
<eng-data t="1.154" f="1810.4" m="3063.1" cg="278.5"/>
<eng-data t="1.518" f="1874.05" m="2695.94" cg="278.5"/>
<eng-data t="1.642" f="1842.23" m="2569.78" cg="278.5"/>
<eng-data t="2." f="1888.19" m="2204.16" cg="278.5"/>
<eng-data t="2.558" f="1891.73" m="1626.73" cg="278.5"/>
<eng-data t="2.775" f="1782.12" m="1408.48" cg="278.5"/>
<eng-data t="2.818" f="1707.86" m="1367.4" cg="278.5"/>
<eng-data t="2.894" f="1615.93" m="1298.24" cg="278.5"/>
<eng-data t="2.997" f="1520.46" m="1209.8" cg="278.5"/>
<eng-data t="4." f="1011.28" m="514.613" cg="278.5"/>
<eng-data t="4.509" f="763.764" m="267.265" cg="278.5"/>
<eng-data t="4.862" f="608.183" m="134.68" cg="278.5"/>
<eng-data t="4.981" f="583.431" m="95.8589" cg="278.5"/>
<eng-data t="5.062" f="526.856" m="71.2381" cg="278.5"/>
<eng-data t="5.149" f="438.457" m="48.2465" cg="278.5"/>
<eng-data t="5.322" f="226.301" m="16.7624" cg="278.5"/>
<eng-data t="5.458" f="99.006" m="4.65041" cg="278.5"/>
<eng-data t="5.577" f="28.288" m="0.503382" cg="278.5"/>
<eng-data t="5.642" f="0." m="0." cg="278.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="M1350W" Type="single-use" dia="75." len="622."
initWt="4808." propWt="2690." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1296.16" peakThrust="1749.91" throatDia="0." exitDia="0."
Itot="5179.48" burn-time="4." massFrac="55.95" Isp="196.34" tDiv="10" tStep="-1."
tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="2690." cg="311."/>
<eng-data t="0.03" f="1428.89" m="2678.87" cg="311."/>
<eng-data t="0.044" f="1724.73" m="2667.4" cg="311."/>
<eng-data t="0.056" f="1548.48" m="2657.2" cg="311."/>
<eng-data t="0.078" f="1620.87" m="2639.1" cg="311."/>
<eng-data t="0.115" f="1589.4" m="2608.25" cg="311."/>
<eng-data t="0.178" f="1642.9" m="2555.37" cg="311."/>
<eng-data t="0.455" f="1749.91" m="2311.32" cg="311."/>
<eng-data t="0.496" f="1724.73" m="2274.33" cg="311."/>
<eng-data t="0.54" f="1737.32" m="2234.77" cg="311."/>
<eng-data t="1.132" f="1746.77" m="1699.16" cg="311."/>
<eng-data t="1.499" f="1731.03" m="1367.72" cg="311."/>
<eng-data t="1.639" f="1715.29" m="1242.43" cg="311."/>
<eng-data t="2.505" f="1334.47" m="556.597" cg="311."/>
<eng-data t="3.086" f="1051.21" m="196.662" cg="311."/>
<eng-data t="3.179" f="985.113" m="147.485" cg="311."/>
<eng-data t="3.227" f="928.461" m="123.633" cg="311."/>
<eng-data t="3.315" f="670.38" m="87.0965" cg="311."/>
<eng-data t="3.419" f="446.92" m="56.922" cg="311."/>
<eng-data t="3.46" f="396.563" m="47.9416" cg="311."/>
<eng-data t="3.545" f="298.996" m="32.5888" cg="311."/>
<eng-data t="3.697" f="173.103" m="13.9544" cg="311."/>
<eng-data t="3.737" f="173.103" m="10.3584" cg="311."/>
<eng-data t="3.845" f="81.83" m="3.20868" cg="311."/>
<eng-data t="3.996" f="0." m="0." cg="311."/>
</data>
</engine>
<engine mfg="Aerotech" code="M1419W" Type="reloadable" dia="98." len="597."
initWt="6930.7" propWt="3990." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1083.24" peakThrust="1462.23" throatDia="0." exitDia="0."
Itot="7582.66" burn-time="7." massFrac="57.57" Isp="193.79" tDiv="10" tStep="-1."
tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="3990." cg="298.5"/>
<eng-data t="0." f="0.22" m="3990." cg="298.5"/>
<eng-data t="0.1" f="1307.13" m="3955.6" cg="298.5"/>
<eng-data t="0.2" f="1218.53" m="3889.15" cg="298.5"/>
<eng-data t="1.4" f="1373.59" m="3070.77" cg="298.5"/>
<eng-data t="2.5" f="1462.23" m="2250.05" cg="298.5"/>
<eng-data t="3." f="1440.04" m="1868.26" cg="298.5"/>
<eng-data t="3.6" f="1404.63" m="1419.2" cg="298.5"/>
<eng-data t="4.4" f="1160.84" m="879.219" cg="298.5"/>
<eng-data t="5.8" f="664.66" m="206.814" cg="298.5"/>
<eng-data t="6.1" f="629.17" m="104.692" cg="298.5"/>
<eng-data t="6.5" f="177.25" m="19.8246" cg="298.5"/>
<eng-data t="6.9" f="8.9" m="0.234159" cg="298.5"/>
<eng-data t="7." f="0." m="0." cg="298.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="M1500G" Type="reloadable" dia="75." len="665."
initWt="4896." propWt="2631." delays="0,6,10,14,18" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="1449.23" peakThrust="1716.51" throatDia="0."
exitDia="0." Itot="5217.24" burn-time="3.6" massFrac="53.74" Isp="202.21"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Curvefit of AeroTech Instructions by C. Kobel 11/19/08</comments>
<data>
<eng-data t="0." f="0." m="2631." cg="332.5"/>
<eng-data t="0.012" f="1183.8" m="2627.42" cg="332.5"/>
<eng-data t="0.023" f="1614.27" m="2619.66" cg="332.5"/>
<eng-data t="0.05" f="1694.99" m="2597.13" cg="332.5"/>
<eng-data t="0.1" f="1716.51" m="2554.12" cg="332.5"/>
<eng-data t="0.15" f="1694.99" m="2511.11" cg="332.5"/>
<eng-data t="0.2" f="1603.51" m="2469.52" cg="332.5"/>
<eng-data t="0.25" f="1517.42" m="2430.18" cg="332.5"/>
<eng-data t="0.3" f="1490.51" m="2392.26" cg="332.5"/>
<eng-data t="0.4" f="1474.37" m="2317.5" cg="332.5"/>
<eng-data t="0.5" f="1485.13" m="2242.88" cg="332.5"/>
<eng-data t="0.6" f="1512.04" m="2167.3" cg="332.5"/>
<eng-data t="0.7" f="1533.56" m="2090.51" cg="332.5"/>
<eng-data t="0.8" f="1571.23" m="2012.22" cg="332.5"/>
<eng-data t="0.9" f="1608.89" m="1932.04" cg="332.5"/>
<eng-data t="1." f="1630.42" m="1850.36" cg="332.5"/>
<eng-data t="1.1" f="1657.32" m="1767.46" cg="332.5"/>
<eng-data t="1.2" f="1684.22" m="1683.21" cg="332.5"/>
<eng-data t="1.3" f="1694.99" m="1598." cg="332.5"/>
<eng-data t="1.4" f="1694.99" m="1512.53" cg="332.5"/>
<eng-data t="1.5" f="1700.37" m="1426.91" cg="332.5"/>
<eng-data t="1.6" f="1700.37" m="1341.17" cg="332.5"/>
<eng-data t="1.7" f="1705.75" m="1255.28" cg="332.5"/>
<eng-data t="1.8" f="1689.61" m="1169.67" cg="332.5"/>
<eng-data t="1.9" f="1662.7" m="1085.14" cg="332.5"/>
<eng-data t="2." f="1657.32" m="1001.43" cg="332.5"/>
<eng-data t="2.1" f="1608.89" m="919.076" cg="332.5"/>
<eng-data t="2.2" f="1581.99" m="838.619" cg="332.5"/>
<eng-data t="2.3" f="1555.08" m="759.52" cg="332.5"/>
<eng-data t="2.4" f="1522.8" m="681.912" cg="332.5"/>
<eng-data t="2.5" f="1490.51" m="605.933" cg="332.5"/>
<eng-data t="2.6" f="1463.61" m="531.447" cg="332.5"/>
<eng-data t="2.7" f="1431.32" m="458.452" cg="332.5"/>
<eng-data t="2.8" f="1415.18" m="386.679" cg="332.5"/>
<eng-data t="2.9" f="1388.28" m="315.992" cg="332.5"/>
<eng-data t="3." f="1361.37" m="246.661" cg="332.5"/>
<eng-data t="3.1" f="1372.13" m="177.737" cg="332.5"/>
<eng-data t="3.2" f="1286.04" m="110.712" cg="332.5"/>
<eng-data t="3.25" f="1226.85" m="79.0318" cg="332.5"/>
<eng-data t="3.3" f="973.945" m="51.2859" cg="332.5"/>
<eng-data t="3.4" f="478.901" m="14.6531" cg="332.5"/>
<eng-data t="3.45" f="220.617" m="5.83412" cg="332.5"/>
<eng-data t="3.5" f="80.714" m="2.03516" cg="332.5"/>
<eng-data t="3.6" f="0." m="0." cg="332.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="M1550R" Type="reloadable" dia="75." len="800."
initWt="5715." propWt="3493." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1531.61" peakThrust="2125.33" throatDia="0." exitDia="0."
Itot="5529.12" burn-time="3.61" massFrac="61.12" Isp="161.41" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="3493." cg="400."/>
<eng-data t="0.07" f="1720.76" m="3454.95" cg="400."/>
<eng-data t="0.21" f="2125.33" m="3284.87" cg="400."/>
<eng-data t="0.36" f="1995.95" m="3089.6" cg="400."/>
<eng-data t="0.5" f="1908.44" m="2916.94" cg="400."/>
<eng-data t="0.65" f="1868.71" m="2737.97" cg="400."/>
<eng-data t="0.79" f="1835.5" m="2574.16" cg="400."/>
<eng-data t="0.94" f="1808.66" m="2401.5" cg="400."/>
<eng-data t="1.08" f="1796.3" m="2242.08" cg="400."/>
<eng-data t="1.22" f="1785.42" m="2083.69" cg="400."/>
<eng-data t="1.37" f="1773.15" m="1915.08" cg="400."/>
<eng-data t="1.51" f="1746.59" m="1759.43" cg="400."/>
<eng-data t="1.66" f="1715.71" m="1595.38" cg="400."/>
<eng-data t="1.8" f="1689.63" m="1444.79" cg="400."/>
<eng-data t="1.95" f="1660.72" m="1286.05" cg="400."/>
<eng-data t="2.09" f="1633.28" m="1140.38" cg="400."/>
<eng-data t="2.23" f="1606.04" m="997.13" cg="400."/>
<eng-data t="2.38" f="1570.22" m="846.636" cg="400."/>
<eng-data t="2.52" f="1534.71" m="709.329" cg="400."/>
<eng-data t="2.67" f="1503.35" m="565.382" cg="400."/>
<eng-data t="2.81" f="1461.32" m="434.278" cg="400."/>
<eng-data t="2.96" f="1427.57" m="297.4" cg="400."/>
<eng-data t="3.1" f="1393.23" m="172.657" cg="400."/>
<eng-data t="3.24" f="939.96" m="69.4785" cg="400."/>
<eng-data t="3.39" f="268.5" m="12.2204" cg="400."/>
<eng-data t="3.53" f="4.99" m="0.126097" cg="400."/>
<eng-data t="3.61" f="0." m="0." cg="400."/>
</data>
</engine>
<engine mfg="Aerotech" code="M1600R" Type="reloadable" dia="98." len="579."
initWt="7004." propWt="4082." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1554.04" peakThrust="1856.37" throatDia="0." exitDia="0."
Itot="6993.2" burn-time="4.5" massFrac="58.28" Isp="174.7" tDiv="10" tStep="-1."
tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="4082." cg="289.5"/>
<eng-data t="0.09" f="1370.36" m="4046." cg="289.5"/>
<eng-data t="0.27" f="1626.63" m="3888.56" cg="289.5"/>
<eng-data t="0.45" f="1672.65" m="3715.24" cg="289.5"/>
<eng-data t="0.63" f="1720.6" m="3536.98" cg="289.5"/>
<eng-data t="0.81" f="1763.29" m="3353.95" cg="289.5"/>
<eng-data t="0.99" f="1801.28" m="3166.69" cg="289.5"/>
<eng-data t="1.17" f="1829.83" m="2975.94" cg="289.5"/>
<eng-data t="1.35" f="1845.15" m="2782.88" cg="289.5"/>
<eng-data t="1.53" f="1856.37" m="2588.42" cg="289.5"/>
<eng-data t="1.71" f="1850.09" m="2393.71" cg="289.5"/>
<eng-data t="1.89" f="1847.37" m="2199.46" cg="289.5"/>
<eng-data t="2.07" f="1829.45" m="2006.31" cg="289.5"/>
<eng-data t="2.25" f="1810.98" m="1815.06" cg="289.5"/>
<eng-data t="2.43" f="1784.91" m="1626.15" cg="289.5"/>
<eng-data t="2.61" f="1754.27" m="1440.23" cg="289.5"/>
<eng-data t="2.79" f="1726.9" m="1257.35" cg="289.5"/>
<eng-data t="2.97" f="1689.29" m="1077.88" cg="289.5"/>
<eng-data t="3.15" f="1641.58" m="902.898" cg="289.5"/>
<eng-data t="3.33" f="1581.59" m="733.573" cg="289.5"/>
<eng-data t="3.51" f="1511.04" m="571.105" cg="289.5"/>
<eng-data t="3.69" f="1431.4" m="416.527" cg="289.5"/>
<eng-data t="3.87" f="1361.03" m="269.83" cg="289.5"/>
<eng-data t="4.05" f="1234.57" m="133.473" cg="289.5"/>
<eng-data t="4.23" f="621.21" m="35.9813" cg="289.5"/>
<eng-data t="4.41" f="42.47" m="1.11556" cg="289.5"/>
<eng-data t="4.5" f="0." m="0." cg="289.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="M1850W" Type="reloadable" dia="75." len="935."
initWt="6871." propWt="3979." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1133.21" peakThrust="2411." throatDia="0." exitDia="0." Itot="7365.9"
burn-time="6.5" massFrac="57.91" Isp="188.77" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>75-7680 case
Greg Gardner - 10/25/07
</comments>
<data>
<eng-data t="0." f="0." m="3979." cg="467.5"/>
<eng-data t="0.1" f="2411." m="3913.88" cg="467.5"/>
<eng-data t="0.2" f="2135." m="3791.09" cg="467.5"/>
<eng-data t="0.3" f="2015." m="3679." cg="467.5"/>
<eng-data t="0.4" f="2000." m="3570.56" cg="467.5"/>
<eng-data t="0.5" f="2055." m="3461.04" cg="467.5"/>
<eng-data t="1." f="2098." m="2900.18" cg="467.5"/>
<eng-data t="1.5" f="1860." m="2365.66" cg="467.5"/>
<eng-data t="2." f="1788." m="1873.01" cg="467.5"/>
<eng-data t="2.5" f="1659." m="1407.5" cg="467.5"/>
<eng-data t="3." f="1468." m="985.202" cg="467.5"/>
<eng-data t="3.25" f="1423." m="789.99" cg="467.5"/>
<eng-data t="3.35" f="1334." m="715.525" cg="467.5"/>
<eng-data t="3.5" f="1201." m="612.821" cg="467.5"/>
<eng-data t="3.75" f="934." m="468.657" cg="467.5"/>
<eng-data t="3.8" f="930." m="443.484" cg="467.5"/>
<eng-data t="4." f="881." m="345.655" cg="467.5"/>
<eng-data t="4.25" f="600." m="245.652" cg="467.5"/>
<eng-data t="4.5" f="468." m="173.537" cg="467.5"/>
<eng-data t="4.75" f="400." m="114.926" cg="467.5"/>
<eng-data t="5." f="290." m="68.3343" cg="467.5"/>
<eng-data t="5.5" f="85." m="17.6913" cg="467.5"/>
<eng-data t="6." f="23." m="3.1061" cg="467.5"/>
<eng-data t="6.5" f="0." m="0." cg="467.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="M1939W" Type="reloadable" dia="98." len="751."
initWt="8844.5" propWt="5320." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1477.12" peakThrust="2084.16" throatDia="0." exitDia="0."
Itot="10339.8" burn-time="7." massFrac="60.15" Isp="198.19" tDiv="10" tStep="-1."
tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="5320." cg="375.5"/>
<eng-data t="0." f="1.33" m="5320." cg="375.5"/>
<eng-data t="0.1" f="1806.56" m="5273.49" cg="375.5"/>
<eng-data t="0.6" f="1881.42" m="4799.11" cg="375.5"/>
<eng-data t="1.3" f="1982.79" m="4103.24" cg="375.5"/>
<eng-data t="1.9" f="2062.09" m="3478.89" cg="375.5"/>
<eng-data t="2.1" f="2079.71" m="3265.79" cg="375.5"/>
<eng-data t="2.6" f="2084.16" m="2730.2" cg="375.5"/>
<eng-data t="3.3" f="1982.79" m="1997.82" cg="375.5"/>
<eng-data t="4.1" f="1696.38" m="1240.62" cg="375.5"/>
<eng-data t="5.2" f="1145.58" m="436.393" cg="375.5"/>
<eng-data t="5.6" f="991.37" m="216.494" cg="375.5"/>
<eng-data t="6.2" f="176.23" m="36.2693" cg="375.5"/>
<eng-data t="7." f="0." m="0." cg="375.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="M2000R" Type="reloadable" dia="98." len="732."
initWt="9099." propWt="5729." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1953.41" peakThrust="2316.16" throatDia="0." exitDia="0."
Itot="9181.04" burn-time="4.7" massFrac="62.96" Isp="163.42" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="5729." cg="366."/>
<eng-data t="0.09" f="1530.96" m="5686.01" cg="366."/>
<eng-data t="0.28" f="2186.27" m="5465.65" cg="366."/>
<eng-data t="0.47" f="2166.7" m="5207.61" cg="366."/>
<eng-data t="0.66" f="2187.24" m="4949.5" cg="366."/>
<eng-data t="0.84" f="2219.07" m="4702.04" cg="366."/>
<eng-data t="1.03" f="2248.07" m="4437.23" cg="366."/>
<eng-data t="1.22" f="2273.74" m="4169.18" cg="366."/>
<eng-data t="1.41" f="2298.31" m="3898.14" cg="366."/>
<eng-data t="1.6" f="2309.75" m="3624.98" cg="366."/>
<eng-data t="1.78" f="2315.71" m="3365.21" cg="366."/>
<eng-data t="1.97" f="2316.16" m="3090.63" cg="366."/>
<eng-data t="2.16" f="2306.31" m="2816.61" cg="366."/>
<eng-data t="2.35" f="2282.23" m="2544.6" cg="366."/>
<eng-data t="2.54" f="2252.1" m="2275.8" cg="366."/>
<eng-data t="2.73" f="2209.64" m="2011.31" cg="366."/>
<eng-data t="2.92" f="2168.8" m="1751.75" cg="366."/>
<eng-data t="3.1" f="2117.18" m="1511.05" cg="366."/>
<eng-data t="3.29" f="2067.53" m="1262.98" cg="366."/>
<eng-data t="3.48" f="2004.51" m="1021.59" cg="366."/>
<eng-data t="3.67" f="1934.44" m="788.088" cg="366."/>
<eng-data t="3.86" f="1831.48" m="564.843" cg="366."/>
<eng-data t="4.04" f="1745.63" m="363.952" cg="366."/>
<eng-data t="4.23" f="1504.27" m="171.297" cg="366."/>
<eng-data t="4.42" f="649.8" m="43.603" cg="366."/>
<eng-data t="4.61" f="58.18" m="1.6337" cg="366."/>
<eng-data t="4.7" f="0." m="0." cg="366."/>
</data>
</engine>
<engine mfg="Aerotech" code="M2050X" Type="single-use" dia="75." len="700."
initWt="4559." propWt="2268." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1986.74" peakThrust="2562.07" throatDia="0." exitDia="0."
Itot="5491.36" burn-time="2.76" massFrac="49.75" Isp="246.9" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="2268." cg="350."/>
<eng-data t="0.028" f="417.223" m="2265.59" cg="350."/>
<eng-data t="0.067" f="2562.08" m="2241.59" cg="350."/>
<eng-data t="0.151" f="2409.04" m="2155.36" cg="350."/>
<eng-data t="0.261" f="2391.86" m="2046.31" cg="350."/>
<eng-data t="0.372" f="2297.6" m="1938.81" cg="350."/>
<eng-data t="0.557" f="2265.37" m="1764.49" cg="350."/>
<eng-data t="0.779" f="2242.44" m="1557.83" cg="350."/>
<eng-data t="0.965" f="2220.18" m="1386.42" cg="350."/>
<eng-data t="1.15" f="2188.68" m="1217.99" cg="350."/>
<eng-data t="1.372" f="2145.75" m="1019.28" cg="350."/>
<eng-data t="1.816" f="2059.65" m="633.691" cg="350."/>
<eng-data t="2.149" f="2027.93" m="352.602" cg="350."/>
<eng-data t="2.325" f="2021." m="205.443" cg="350."/>
<eng-data t="2.419" f="1865." m="130.01" cg="350."/>
<eng-data t="2.495" f="1461.84" m="77.7965" cg="350."/>
<eng-data t="2.611" f="804.758" m="23.5007" cg="350."/>
<eng-data t="2.697" f="307.633" m="3.74511" cg="350."/>
<eng-data t="2.736" f="91.61" m="0.529705" cg="350."/>
<eng-data t="2.764" f="0." m="0." cg="350."/>
</data>
</engine>
<engine mfg="Aerotech" code="M2100G" Type="reloadable" dia="98." len="597."
initWt="7030." propWt="4030." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="2162.06" peakThrust="2968.18" throatDia="0." exitDia="0."
Itot="7655.85" burn-time="3.54" massFrac="57.33" Isp="193.72" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Entered by Tim Van Milligan for RockSim Users. Used John Coker's ThrustCurve
Tracer software and TRA cert paperwork dated 10-14-08.
</comments>
<data>
<eng-data t="0." f="0." m="4030." cg="298.5"/>
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<eng-data t="3.401" f="1188.89" m="69.5517" cg="298.5"/>
<eng-data t="3.447" f="1140.36" m="41.3513" cg="298.5"/>
<eng-data t="3.478" f="1035.22" m="23.6004" cg="298.5"/>
<eng-data t="3.513" f="913.907" m="5.64519" cg="298.5"/>
<eng-data t="3.516" f="541.874" m="4.49572" cg="298.5"/>
<eng-data t="3.527" f="444.822" m="1.63906" cg="298.5"/>
<eng-data t="3.541" f="0." m="0." cg="298.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="M2400T" Type="reloadable" dia="98." len="597."
initWt="6483." propWt="3692.6" delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="2177.07" peakThrust="3237.07" throatDia="0." exitDia="0."
Itot="7619.76" burn-time="3.5" massFrac="56.96" Isp="210.42" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="3692.6" cg="298.5"/>
<eng-data t="0.0231839" f="3237.07" m="3674.42" cg="298.5"/>
<eng-data t="0.0386399" f="2356.24" m="3653.47" cg="298.5"/>
<eng-data t="0.0618238" f="2576.45" m="3625.76" cg="298.5"/>
<eng-data t="0.0850077" f="2356.24" m="3598.05" cg="298.5"/>
<eng-data t="0.340031" f="2532.4" m="3295.96" cg="298.5"/>
<eng-data t="1.14374" f="2708.57" m="2275.33" cg="298.5"/>
<eng-data t="1.52241" f="2642.51" m="1784.35" cg="298.5"/>
<eng-data t="2.00927" f="2532.4" m="1173.87" cg="298.5"/>
<eng-data t="2.50386" f="2313.08" m="593.185" cg="298.5"/>
<eng-data t="2.86708" f="2025.92" m="211.311" cg="298.5"/>
<eng-data t="2.99845" f="1519.44" m="98.457" cg="298.5"/>
<eng-data t="3.19938" f="198.188" m="14.8323" cg="298.5"/>
<eng-data t="3.40804" f="66.0627" m="1.47203" cg="298.5"/>
<eng-data t="3.5" f="0." m="0." cg="298.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="M2500T" Type="reloadable" dia="98." len="751."
initWt="8064." propWt="4659.2" delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="2245.07" peakThrust="2861.69" throatDia="0." exitDia="0." Itot="9573."
burn-time="4.26" massFrac="57.78" Isp="209.52" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>AeroTech M2500T
Copyright Tripoli Motor Testing 1998 (www.tripoli.org)
provided by ThrustCurve.org (www.thrustcurve.org)
</comments>
<data>
<eng-data t="0." f="0." m="4659.2" cg="375.5"/>
<eng-data t="0.082" f="2651.86" m="4606.28" cg="375.5"/>
<eng-data t="0.249" f="2780.28" m="4385.52" cg="375.5"/>
<eng-data t="0.416" f="2820.73" m="4157.9" cg="375.5"/>
<eng-data t="0.583" f="2843.01" m="3927.73" cg="375.5"/>
<eng-data t="0.751" f="2847.76" m="3695.07" cg="375.5"/>
<eng-data t="0.918" f="2851.22" m="3463.47" cg="375.5"/>
<eng-data t="1.084" f="2854.74" m="3232.97" cg="375.5"/>
<eng-data t="1.252" f="2861.69" m="2999.26" cg="375.5"/>
<eng-data t="1.42" f="2858.09" m="2765.42" cg="375.5"/>
<eng-data t="1.586" f="2851.09" m="2534.79" cg="375.5"/>
<eng-data t="1.754" f="2844.62" m="2301.93" cg="375.5"/>
<eng-data t="1.922" f="2830.86" m="2069.9" cg="375.5"/>
<eng-data t="2.089" f="2804.71" m="1840.87" cg="375.5"/>
<eng-data t="2.255" f="2765.8" m="1615.85" cg="375.5"/>
<eng-data t="2.423" f="2710.51" m="1391.96" cg="375.5"/>
<eng-data t="2.591" f="2648.26" m="1172.88" cg="375.5"/>
<eng-data t="2.757" f="2586.91" m="961.395" cg="375.5"/>
<eng-data t="2.925" f="2520.79" m="752.577" cg="375.5"/>
<eng-data t="3.093" f="2462.22" m="548.856" cg="375.5"/>
<eng-data t="3.259" f="2419.94" m="351.635" cg="375.5"/>
<eng-data t="3.426" f="1894.94" m="176.28" cg="375.5"/>
<eng-data t="3.594" f="808.043" m="65.7738" cg="375.5"/>
<eng-data t="3.761" f="282.403" m="21.4585" cg="375.5"/>
<eng-data t="3.928" f="97.876" m="6.00408" cg="375.5"/>
<eng-data t="4.096" f="24.492" m="1.00131" cg="375.5"/>
<eng-data t="4.264" f="0." m="0." cg="375.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="M1075DM" Type="reloadable" dia="98." len="597."
initWt="6971." propWt="3846." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1023.31" peakThrust="1264.43" throatDia="0." exitDia="0."
Itot="5628.19" burn-time="5.5" massFrac="55.17" Isp="149.22" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>M1075 Dark Matter</comments>
<data>
<eng-data t="0." f="0." m="3846." cg="298.5"/>
<eng-data t="0.02" f="927.501" m="3839.66" cg="298.5"/>
<eng-data t="0.112" f="988.073" m="3779.45" cg="298.5"/>
<eng-data t="0.26" f="1033.5" m="3677.22" cg="298.5"/>
<eng-data t="0.53" f="1080.82" m="3482.17" cg="298.5"/>
<eng-data t="0.897" f="1124.36" m="3205.66" cg="298.5"/>
<eng-data t="1.509" f="1198.18" m="2720." cg="298.5"/>
<eng-data t="1.998" f="1239.82" m="2312.67" cg="298.5"/>
<eng-data t="2.355" f="1260.64" m="2007.67" cg="298.5"/>
<eng-data t="2.503" f="1264.43" m="1879.98" cg="298.5"/>
<eng-data t="2.773" f="1237.93" m="1649.13" cg="298.5"/>
<eng-data t="2.997" f="1222.79" m="1460.8" cg="298.5"/>
<eng-data t="3.502" f="1162.22" m="1049.28" cg="298.5"/>
<eng-data t="4.001" f="1063.79" m="669.761" cg="298.5"/>
<eng-data t="4.501" f="906.68" m="333.133" cg="298.5"/>
<eng-data t="4.741" f="834.751" m="190.333" cg="298.5"/>
<eng-data t="4.878" f="742.001" m="116.527" cg="298.5"/>
<eng-data t="4.96" f="664.394" m="77.1236" cg="298.5"/>
<eng-data t="5.062" f="448.608" m="38.3348" cg="298.5"/>
<eng-data t="5.164" f="223.357" m="14.9164" cg="298.5"/>
<eng-data t="5.26" f="79.5" m="4.98249" cg="298.5"/>
<eng-data t="5.352" f="30.286" m="1.53149" cg="298.5"/>
<eng-data t="5.5" f="0." m="0." cg="298.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="M1780NT" Type="reloadable" dia="75." len="665."
initWt="4606." propWt="2371." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1759.83" peakThrust="2197.23" throatDia="0." exitDia="0."
Itot="5341.08" burn-time="3.04" massFrac="51.48" Isp="229.71" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments><![CDATA[AT M1780NT 1" Core Revised]]></comments>
<data>
<eng-data t="0." f="0." m="2371." cg="332.5"/>
<eng-data t="0.009" f="1337.15" m="2368.33" cg="332.5"/>
<eng-data t="0.026" f="2005.73" m="2355.72" cg="332.5"/>
<eng-data t="0.04" f="2106.52" m="2342.94" cg="332.5"/>
<eng-data t="0.046" f="2163.64" m="2337.25" cg="332.5"/>
<eng-data t="0.085" f="2156.92" m="2299.85" cg="332.5"/>
<eng-data t="0.108" f="2126.68" m="2277.98" cg="332.5"/>
<eng-data t="0.134" f="2113.24" m="2253.51" cg="332.5"/>
<eng-data t="0.168" f="2130.04" m="2221.49" cg="332.5"/>
<eng-data t="0.205" f="2126.68" m="2186.53" cg="332.5"/>
<eng-data t="0.259" f="2197.23" m="2134.71" cg="332.5"/>
<eng-data t="0.299" f="2156.92" m="2096.05" cg="332.5"/>
<eng-data t="0.347" f="2130.04" m="2050.38" cg="332.5"/>
<eng-data t="0.399" f="2123.32" m="2001.28" cg="332.5"/>
<eng-data t="0.495" f="2103.16" m="1911.23" cg="332.5"/>
<eng-data t="0.595" f="2089.72" m="1818.16" cg="332.5"/>
<eng-data t="0.697" f="2079.64" m="1723.77" cg="332.5"/>
<eng-data t="0.8" f="2083." m="1628.6" cg="332.5"/>
<eng-data t="0.9" f="2076.28" m="1536.28" cg="332.5"/>
<eng-data t="0.999" f="2069.57" m="1445.18" cg="332.5"/>
<eng-data t="1.201" f="2056.13" m="1260.2" cg="332.5"/>
<eng-data t="1.398" f="2029.25" m="1081.57" cg="332.5"/>
<eng-data t="1.603" f="2002.37" m="898.123" cg="332.5"/>
<eng-data t="1.799" f="1965.41" m="725.509" cg="332.5"/>
<eng-data t="1.998" f="1904.94" m="554.556" cg="332.5"/>
<eng-data t="2.2" f="1817.59" m="387.654" cg="332.5"/>
<eng-data t="2.3" f="1757.11" m="308.31" cg="332.5"/>
<eng-data t="2.354" f="1723.52" m="266.592" cg="332.5"/>
<eng-data t="2.405" f="1713.44" m="227.686" cg="332.5"/>
<eng-data t="2.46" f="1629.45" m="186.877" cg="332.5"/>
<eng-data t="2.502" f="1558.89" m="157.154" cg="332.5"/>
<eng-data t="2.571" f="1333.79" m="112.852" cg="332.5"/>
<eng-data t="2.622" f="1115.41" m="85.1274" cg="332.5"/>
<eng-data t="2.67" f="890.316" m="63.7583" cg="332.5"/>
<eng-data t="2.724" f="665.217" m="45.1141" cg="332.5"/>
<eng-data t="2.758" f="571.146" m="35.7837" cg="332.5"/>
<eng-data t="2.798" f="507.312" m="26.2088" cg="332.5"/>
<eng-data t="2.83" f="446.838" m="19.4318" cg="332.5"/>
<eng-data t="2.901" f="265.415" m="8.2073" cg="332.5"/>
<eng-data t="3.003" f="73.913" m="0.524981" cg="332.5"/>
<eng-data t="3.035" f="0." m="0." cg="332.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="M1800FJ" Type="reloadable" dia="98." len="751."
initWt="9162." propWt="5599." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1658.46" peakThrust="3007.36" throatDia="0." exitDia="0."
Itot="8212.7" burn-time="4.95" massFrac="61.11" Isp="149.57" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Entered by Tim Van Milligan. Used John Coker's ThrustCurve Tracer software and
data from TRA certification dated 10-14-08
</comments>
<data>
<eng-data t="0." f="0." m="5599." cg="375.5"/>
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<eng-data t="2.142" f="2220.06" m="2621.7" cg="375.5"/>
<eng-data t="2.393" f="2220.06" m="2241.81" cg="375.5"/>
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<eng-data t="2.655" f="2106.57" m="1854.59" cg="375.5"/>
<eng-data t="2.831" f="2007.27" m="1607.79" cg="375.5"/>
<eng-data t="2.922" f="1978.9" m="1484.14" cg="375.5"/>
<eng-data t="3.029" f="1915.07" m="1342.11" cg="375.5"/>
<eng-data t="3.21" f="1808.67" m="1112.36" cg="375.5"/>
<eng-data t="3.349" f="1695.19" m="946.343" cg="375.5"/>
<eng-data t="3.526" f="1588.8" m="748.205" cg="375.5"/>
<eng-data t="3.723" f="1439.85" m="544.825" cg="375.5"/>
<eng-data t="3.851" f="1397.29" m="421.035" cg="375.5"/>
<eng-data t="3.921" f="1361.82" m="355.199" cg="375.5"/>
<eng-data t="4.017" f="1255.43" m="269.552" cg="375.5"/>
<eng-data t="4.097" f="1120.67" m="204.756" cg="375.5"/>
<eng-data t="4.167" f="978.811" m="154.66" cg="375.5"/>
<eng-data t="4.263" f="780.212" m="97.0976" cg="375.5"/>
<eng-data t="4.327" f="624.169" m="66.4596" cg="375.5"/>
<eng-data t="4.402" f="453.941" m="38.8971" cg="375.5"/>
<eng-data t="4.428" f="375.92" m="31.5423" cg="375.5"/>
<eng-data t="4.482" f="276.621" m="19.5308" cg="375.5"/>
<eng-data t="4.53" f="177.321" m="12.1034" cg="375.5"/>
<eng-data t="4.583" f="99.3" m="7.10588" cg="375.5"/>
<eng-data t="4.653" f="42.557" m="3.72099" cg="375.5"/>
<eng-data t="4.76" f="21.279" m="1.39267" cg="375.5"/>
<eng-data t="4.952" f="0." m="0." cg="375.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="M1845NT" Type="reloadable" dia="98." len="597."
initWt="6682." propWt="3772." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1711.45" peakThrust="2433.83" throatDia="0." exitDia="0."
Itot="8093.46" burn-time="4.73" massFrac="56.45" Isp="218.8" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="3772." cg="298.5"/>
<eng-data t="0.024" f="2261.64" m="3759.35" cg="298.5"/>
<eng-data t="0.067" f="2115.94" m="3715.49" cg="298.5"/>
<eng-data t="1.032" f="2268.26" m="2729.6" cg="298.5"/>
<eng-data t="1.354" f="2433.83" m="2376.78" cg="298.5"/>
<eng-data t="2.253" f="2288.13" m="1387.57" cg="298.5"/>
<eng-data t="2.406" f="2149.05" m="1229.37" cg="298.5"/>
<eng-data t="2.578" f="1821.23" m="1070.24" cg="298.5"/>
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<eng-data t="4.352" f="248.35" m="11.3584" cg="298.5"/>
<eng-data t="4.498" f="33.113" m="1.78245" cg="298.5"/>
<eng-data t="4.729" f="0." m="0." cg="298.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="M4500ST" Type="reloadable" dia="98." len="597."
initWt="6622.41" propWt="7.55" delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="4321.33" peakThrust="5548.68" throatDia="0." exitDia="0."
Itot="7307.37" burn-time="1.69" massFrac="0.11" Isp="98694.6" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="7.55" cg="298.5"/>
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<eng-data t="0.025" f="4161.51" m="7.48633" cg="298.5"/>
<eng-data t="0.032" f="4004.1" m="7.4568" cg="298.5"/>
<eng-data t="0.033" f="4102.48" m="7.45262" cg="298.5"/>
<eng-data t="0.098" f="4564.87" m="7.16157" cg="298.5"/>
<eng-data t="0.199" f="4840.34" m="6.67084" cg="298.5"/>
<eng-data t="0.4" f="5224.02" m="5.62579" cg="298.5"/>
<eng-data t="0.506" f="5440.46" m="5.0418" cg="298.5"/>
<eng-data t="0.536" f="5420.78" m="4.87347" cg="298.5"/>
<eng-data t="0.597" f="5489.65" m="4.52966" cg="298.5"/>
<eng-data t="0.798" f="5548.68" m="3.38347" cg="298.5"/>
<eng-data t="0.904" f="5460.14" m="2.78063" cg="298.5"/>
<eng-data t="1." f="5263.38" m="2.24881" cg="298.5"/>
<eng-data t="1.08" f="5096.13" m="1.82067" cg="298.5"/>
<eng-data t="1.112" f="4968.23" m="1.65429" cg="298.5"/>
<eng-data t="1.201" f="4545.19" m="1.21689" cg="298.5"/>
<eng-data t="1.341" f="3561.39" m="0.630586" cg="298.5"/>
<eng-data t="1.449" f="2675.96" m="0.282585" cg="298.5"/>
<eng-data t="1.492" f="2302.11" m="0.172003" cg="298.5"/>
<eng-data t="1.52" f="1987.29" m="0.109957" cg="298.5"/>
<eng-data t="1.535" f="1711.83" m="0.0812926" cg="298.5"/>
<eng-data t="1.572" f="905.104" m="0.0312719" cg="298.5"/>
<eng-data t="1.593" f="511.58" m="0.0159028" cg="298.5"/>
<eng-data t="1.625" f="186.924" m="0.00435561" cg="298.5"/>
<eng-data t="1.65" f="59.029" m="0.00117911" cg="298.5"/>
<eng-data t="1.675" f="19.676" m="0.000162635" cg="298.5"/>
<eng-data t="1.691" f="0." m="0." cg="298.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="M6000ST" Type="unspecified" dia="98." len="751."
initWt="8459." propWt="4128." delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="5533.41" peakThrust="7099.55" throatDia="0." exitDia="0." Itot="9606."
burn-time="1.74" massFrac="48.8" Isp="237.29" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>98/10240 Super Thunder</comments>
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<engine mfg="Aerotech" code="N1000W" Type="reloadable" dia="98." len="1046."
initWt="12777." propWt="7925." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="876.235" peakThrust="2119.9" throatDia="0." exitDia="0."
Itot="14138.4" burn-time="16.14" massFrac="62.03" Isp="181.92" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>@File: N1000.txt, @Pts-I: 8069, @Pts-O: 32, @Sm: 3, @CO: 5%
@TI: 14137.65, @TIa: 14071.08, @TIe: 0.0%, @ThMax: 2137.42, @ThAvg: 1048.203, @Tb: 13.424
Exported using ThrustCurveTool, www.ThrustGear.com
</comments>
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<eng-data t="1.7839" f="1594.08" m="6350.09" cg="523."/>
<eng-data t="1.8239" f="1551.16" m="6314.83" cg="523."/>
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<eng-data t="10.9216" f="424.692" m="438.118" cg="523."/>
<eng-data t="13.5895" f="106.05" m="41.2722" cg="523."/>
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<engine mfg="Aerotech" code="N2000W" Type="reloadable" dia="98." len="1046."
initWt="12282.8" propWt="7667.07" delays="1000" auto-calc-mass="1"
auto-calc-cg="1" avgThrust="1727.23" peakThrust="2834.35" throatDia="0."
exitDia="0." Itot="13263.4" burn-time="7.68" massFrac="62.42" Isp="176.4"
tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"
mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>AeroTech N2000W
Copyright Tripoli Motor Testing 1997 (www.tripoli.org)
provided by ThrustCurve.org (www.thrustcurve.org)
</comments>
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initWt="12269." propWt="7512." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="3105.81" peakThrust="3775.78" throatDia="0." exitDia="0."
Itot="14035.1" burn-time="4.52" massFrac="61.23" Isp="190.52" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
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<engine mfg="Aerotech" code="N4800T" Type="reloadable" dia="98." len="1201."
initWt="14784." propWt="9766.4" delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="3702.24" peakThrust="6007.53" throatDia="0." exitDia="0."
Itot="19273.9" burn-time="5.21" massFrac="66.06" Isp="201.24" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>AeroTech N4800T
provided by ThrustCurve.org (www.thrustcurve.org)
</comments>
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</engine>
<engine mfg="Aerotech" code="O5280X" Type="single-use" dia="98." len="1499."
initWt="15681." propWt="9779." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="4920.07" peakThrust="6321." throatDia="0." exitDia="0." Itot="22223.9"
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</engine>
<engine mfg="Aerotech" code="H283ST" Type="single-use" dia="38." len="155."
initWt="247." propWt="97." delays="7,11,15" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="269.031" peakThrust="337.193" throatDia="0." exitDia="0."
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tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
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<comments>38mm DMS Super Thunder</comments>
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<eng-data t="0.677" f="121.389" m="2.03094" cg="77.5"/>
<eng-data t="0.688" f="91.962" m="1.4592" cg="77.5"/>
<eng-data t="0.691" f="98.092" m="1.3203" cg="77.5"/>
<eng-data t="0.722" f="41.689" m="0.264658" cg="77.5"/>
<eng-data t="0.738" f="23.297" m="0.0113511" cg="77.5"/>
<eng-data t="0.74" f="0." m="0." cg="77.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="I175WS" Type="single-use" dia="38." len="214."
initWt="348." propWt="180." delays="5,9,13" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="169.135" peakThrust="252.63" throatDia="0." exitDia="0."
Itot="333.196" burn-time="1.97" massFrac="51.72" Isp="188.76" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>data from TMT certification, tested April 22, 2020</comments>
<data>
<eng-data t="0." f="0." m="180." cg="107."/>
<eng-data t="0.022" f="2.71" m="179.984" cg="107."/>
<eng-data t="0.028" f="93.62" m="179.828" cg="107."/>
<eng-data t="0.06" f="219.78" m="177.119" cg="107."/>
<eng-data t="0.097" f="244.93" m="172.475" cg="107."/>
<eng-data t="0.209" f="252.63" m="157.422" cg="107."/>
<eng-data t="0.299" f="249.21" m="145.222" cg="107."/>
<eng-data t="0.581" f="226.99" m="108.95" cg="107."/>
<eng-data t="0.97" f="190.27" m="65.1067" cg="107."/>
<eng-data t="1.381" f="136.13" m="28.8712" cg="107."/>
<eng-data t="1.749" f="109.02" m="4.50305" cg="107."/>
<eng-data t="1.802" f="65.53" m="2.00421" cg="107."/>
<eng-data t="1.857" f="24.89" m="0.660922" cg="107."/>
<eng-data t="1.908" f="10.42" m="0.174503" cg="107."/>
<eng-data t="1.97" f="0." m="0." cg="107."/>
</data>
</engine>
<engine mfg="Aerotech" code="G80T" Type="single-use" dia="29." len="124." initWt="104.9"
propWt="57.4" delays="4,7,10" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="77.501" peakThrust="105.18" throatDia="0." exitDia="0." Itot="116.252"
burn-time="1.5" massFrac="54.72" Isp="206.52" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>Aerotech G80 RASP.ENG file made from NAR published data
File produced July 4, 2000
Note: This is for the 116N-sec G80T produced before Sept. 2006
</comments>
<data>
<eng-data t="0." f="0." m="57.4" cg="62."/>
<eng-data t="0.006" f="101.291" m="57.25" cg="62."/>
<eng-data t="0.013" f="105.18" m="56.8932" cg="62."/>
<eng-data t="0.031" f="103.473" m="55.9659" cg="62."/>
<eng-data t="0.038" f="104.069" m="55.6073" cg="62."/>
<eng-data t="0.067" f="99.803" m="54.1477" cg="62."/>
<eng-data t="0.103" f="96.906" m="52.3994" cg="62."/>
<eng-data t="0.181" f="94.733" m="48.7091" cg="62."/>
<eng-data t="0.271" f="94.039" m="44.5148" cg="62."/>
<eng-data t="0.303" f="96.985" m="43.0057" cg="62."/>
<eng-data t="0.367" f="95.547" m="39.9637" cg="62."/>
<eng-data t="0.428" f="94.842" m="37.0965" cg="62."/>
<eng-data t="0.456" f="97.055" m="35.77" cg="62."/>
<eng-data t="0.463" f="92.65" m="35.4422" cg="62."/>
<eng-data t="0.51" f="94.872" m="33.2663" cg="62."/>
<eng-data t="0.596" f="93.444" m="29.2681" cg="62."/>
<eng-data t="0.606" f="95.646" m="28.8013" cg="62."/>
<eng-data t="0.624" f="91.985" m="27.9675" cg="62."/>
<eng-data t="0.635" f="95.656" m="27.4579" cg="62."/>
<eng-data t="0.646" f="91.995" m="26.9483" cg="62."/>
<eng-data t="0.696" f="90.547" m="24.695" cg="62."/>
<eng-data t="0.846" f="85.477" m="18.1766" cg="62."/>
<eng-data t="0.96" f="80.388" m="13.5085" cg="62."/>
<eng-data t="1.071" f="74.564" m="9.26228" cg="62."/>
<eng-data t="1.207" f="62.878" m="4.64762" cg="62."/>
<eng-data t="1.296" f="52.639" m="2.10948" cg="62."/>
<eng-data t="1.35" f="37.252" m="0.911107" cg="62."/>
<eng-data t="1.382" f="20.397" m="0.455676" cg="62."/>
<eng-data t="1.418" f="10.139" m="0.184285" cg="62."/>
<eng-data t="1.457" f="4.281" m="0.0454459" cg="62."/>
<eng-data t="1.5" f="0." m="0." cg="62."/>
</data>
</engine>
<engine mfg="Aerotech" code="F52C" Type="single-use" dia="29." len="111." initWt="81.4"
propWt="30." delays="5,8,12" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="49.895" peakThrust="61.323" throatDia="0." exitDia="0." Itot="66.311"
burn-time="1.33" massFrac="36.86" Isp="225.39" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>AeroTech F52C, data from TMT test firing</comments>
<data>
<eng-data t="0." f="0." m="30." cg="55.5"/>
<eng-data t="0.02" f="0.267" m="29.9988" cg="55.5"/>
<eng-data t="0.024" f="3.465" m="29.9954" cg="55.5"/>
<eng-data t="0.038" f="38.82" m="29.8615" cg="55.5"/>
<eng-data t="0.073" f="53.881" m="29.1276" cg="55.5"/>
<eng-data t="0.143" f="56.492" m="27.3799" cg="55.5"/>
<eng-data t="0.323" f="61.323" m="22.5827" cg="55.5"/>
<eng-data t="0.826" f="57.346" m="9.08031" cg="55.5"/>
<eng-data t="1.141" f="51.074" m="1.3548" cg="55.5"/>
<eng-data t="1.17" f="35.612" m="0.786142" cg="55.5"/>
<eng-data t="1.225" f="11.761" m="0.196755" cg="55.5"/>
<eng-data t="1.266" f="4.559" m="0.0453946" cg="55.5"/>
<eng-data t="1.291" f="1.512" m="0.011062" cg="55.5"/>
<eng-data t="1.32" f="0.133" m="0.00027077" cg="55.5"/>
<eng-data t="1.329" f="0." m="0." cg="55.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="G12ST" Type="single-use" dia="29." len="156." initWt="150."
propWt="82." delays="0" auto-calc-mass="1" auto-calc-cg="1" avgThrust="11.574"
peakThrust="31.263" throatDia="0." exitDia="0." Itot="145.847" burn-time="12.6"
massFrac="54.67" Isp="181.37" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<data>
<eng-data t="0." f="0." m="82." cg="78."/>
<eng-data t="0.005" f="0.1561" m="81.9998" cg="78."/>
<eng-data t="0.032" f="1.672" m="81.9859" cg="78."/>
<eng-data t="0.043" f="5.2585" m="81.9645" cg="78."/>
<eng-data t="0.078" f="21.9365" m="81.6969" cg="78."/>
<eng-data t="0.15" f="24.0015" m="80.7671" cg="78."/>
<eng-data t="0.33" f="28.2116" m="78.1251" cg="78."/>
<eng-data t="0.478" f="31.0011" m="75.6615" cg="78."/>
<eng-data t="0.502" f="31.2631" m="75.2414" cg="78."/>
<eng-data t="0.644" f="15.2447" m="73.3849" cg="78."/>
<eng-data t="0.876" f="12.2725" m="71.5902" cg="78."/>
<eng-data t="1.164" f="11.4507" m="69.6696" cg="78."/>
<eng-data t="1.755" f="10.679" m="65.9929" cg="78."/>
<eng-data t="3.003" f="10.1589" m="58.6823" cg="78."/>
<eng-data t="4.025" f="9.8697" m="52.9281" cg="78."/>
<eng-data t="5.141" f="9.9547" m="46.7086" cg="78."/>
<eng-data t="6.725" f="10.9102" m="37.4177" cg="78."/>
<eng-data t="8.856" f="12.0202" m="23.681" cg="78."/>
<eng-data t="11.232" f="12.7126" m="7.16116" cg="78."/>
<eng-data t="12.01" f="11.3399" m="1.90066" cg="78."/>
<eng-data t="12.19" f="9.21" m="0.860817" cg="78."/>
<eng-data t="12.261" f="6.9116" m="0.539041" cg="78."/>
<eng-data t="12.344" f="4.5435" m="0.271763" cg="78."/>
<eng-data t="12.472" f="1.5521" m="0.0524252" cg="78."/>
<eng-data t="12.568" f="0.2906" m="0.00269585" cg="78."/>
<eng-data t="12.601" f="0." m="0." cg="78."/>
</data>
</engine>
<engine mfg="Aerotech" code="H13ST" Type="single-use" dia="29." len="213."
initWt="203.4" propWt="116.4" delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="13.928" peakThrust="44.529" throatDia="0." exitDia="0." Itot="214.935"
burn-time="15.43" massFrac="57.23" Isp="188.29" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>AeroTech H13ST, data from TMT test firing</comments>
<data>
<eng-data t="0." f="0." m="116.4" cg="106.5"/>
<eng-data t="0.005" f="0.107" m="116.4" cg="106.5"/>
<eng-data t="0.024" f="2.636" m="116.386" cg="106.5"/>
<eng-data t="0.035" f="18.978" m="116.321" cg="106.5"/>
<eng-data t="0.081" f="32.724" m="115.677" cg="106.5"/>
<eng-data t="0.147" f="36.421" m="114.442" cg="106.5"/>
<eng-data t="0.379" f="44.529" m="109.356" cg="106.5"/>
<eng-data t="0.452" f="23.851" m="108.005" cg="106.5"/>
<eng-data t="0.566" f="18.89" m="106.685" cg="106.5"/>
<eng-data t="0.818" f="16.728" m="104.255" cg="106.5"/>
<eng-data t="1.286" f="15.676" m="100.148" cg="106.5"/>
<eng-data t="2.114" f="14.753" m="93.3261" cg="106.5"/>
<eng-data t="3.23" f="14.032" m="84.6275" cg="106.5"/>
<eng-data t="4.382" f="13.926" m="75.9064" cg="106.5"/>
<eng-data t="5.786" f="13.469" m="65.4915" cg="106.5"/>
<eng-data t="7.082" f="13.119" m="56.1609" cg="106.5"/>
<eng-data t="8.666" f="12.916" m="44.9941" cg="106.5"/>
<eng-data t="10.286" f="12.82" m="33.7047" cg="106.5"/>
<eng-data t="12.086" f="12.612" m="21.309" cg="106.5"/>
<eng-data t="13.598" f="12.333" m="11.0961" cg="106.5"/>
<eng-data t="14.75" f="11.908" m="3.53438" cg="106.5"/>
<eng-data t="15.23" f="11.078" m="0.546789" cg="106.5"/>
<eng-data t="15.302" f="6.048" m="0.212898" cg="106.5"/>
<eng-data t="15.432" f="0." m="0." cg="106.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="G8ST" Type="unspecified" dia="29." len="156." initWt="157."
propWt="83." delays="0" auto-calc-mass="1" auto-calc-cg="1" avgThrust="6.505"
peakThrust="7.423" throatDia="0." exitDia="0." Itot="129.868" burn-time="19.96"
massFrac="52.87" Isp="159.55" tDiv="10" tStep="-1." tFix="1" FDiv="10"
FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
cgFix="1">
<data>
<eng-data t="0." f="0." m="83." cg="78."/>
<eng-data t="0.024" f="0.3704" m="82.9972" cg="78."/>
<eng-data t="0.066" f="0.8746" m="82.9804" cg="78."/>
<eng-data t="0.138" f="4.5044" m="82.8567" cg="78."/>
<eng-data t="0.246" f="6.6207" m="82.4727" cg="78."/>
<eng-data t="0.426" f="6.7351" m="81.7045" cg="78."/>
<eng-data t="1.218" f="7.3232" m="78.1465" cg="78."/>
<eng-data t="2.082" f="7.423" m="74.0752" cg="78."/>
<eng-data t="3.306" f="7.183" m="68.3622" cg="78."/>
<eng-data t="5.322" f="6.8385" m="59.3292" cg="78."/>
<eng-data t="6.978" f="6.7193" m="52.1547" cg="78."/>
<eng-data t="8.632" f="6.5512" m="45.1406" cg="78."/>
<eng-data t="10.144" f="6.4792" m="38.8447" cg="78."/>
<eng-data t="12.088" f="6.4254" m="30.8282" cg="78."/>
<eng-data t="15.472" f="6.3333" m="17.0312" cg="78."/>
<eng-data t="17.632" f="6.1305" m="8.42823" cg="78."/>
<eng-data t="19.108" f="6.0385" m="2.68855" cg="78."/>
<eng-data t="19.511" f="5.9607" m="1.14328" cg="78."/>
<eng-data t="19.804" f="4.4295" m="0.170452" cg="78."/>
<eng-data t="19.867" f="1.6687" m="0.047683" cg="78."/>
<eng-data t="19.937" f="0.3341" m="0.00288261" cg="78."/>
<eng-data t="19.964" f="0." m="0." cg="78."/>
</data>
</engine>
<engine mfg="Aerotech" code="K400C" Type="single-use" dia="54." len="359."
initWt="1194." propWt="493." delays="14" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="401.122" peakThrust="548.466" throatDia="0." exitDia="0."
Itot="1307.26" burn-time="3.26" massFrac="41.29" Isp="270.39" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Aerotech K400C DMS</comments>
<data>
<eng-data t="0." f="0." m="493." cg="179.5"/>
<eng-data t="0.008" f="376.374" m="492.432" cg="179.5"/>
<eng-data t="0.025" f="526.181" m="489.539" cg="179.5"/>
<eng-data t="0.034" f="548.466" m="487.715" cg="179.5"/>
<eng-data t="0.063" f="500.182" m="481.981" cg="179.5"/>
<eng-data t="0.178" f="527.419" m="459.698" cg="179.5"/>
<eng-data t="0.394" f="522.467" m="416.936" cg="179.5"/>
<eng-data t="0.69" f="502.658" m="359.719" cg="179.5"/>
<eng-data t="1.003" f="487.801" m="301.262" cg="179.5"/>
<eng-data t="1.494" f="446.944" m="214.72" cg="179.5"/>
<eng-data t="2.002" f="402.374" m="133.364" cg="179.5"/>
<eng-data t="2.243" f="377.612" m="97.9183" cg="179.5"/>
<eng-data t="2.501" f="363.994" m="61.8398" cg="179.5"/>
<eng-data t="2.658" f="354.089" m="40.5814" cg="179.5"/>
<eng-data t="2.772" f="337.994" m="25.7043" cg="179.5"/>
<eng-data t="2.844" f="304.566" m="16.9806" cg="179.5"/>
<eng-data t="2.882" f="268.662" m="12.8732" cg="179.5"/>
<eng-data t="2.929" f="177.044" m="8.92311" cg="179.5"/>
<eng-data t="2.963" f="116.379" m="7.04194" cg="179.5"/>
<eng-data t="3.001" f="99.046" m="5.49834" cg="179.5"/>
<eng-data t="3.064" f="94.094" m="3.20394" cg="179.5"/>
<eng-data t="3.123" f="61.904" m="1.46843" cg="179.5"/>
<eng-data t="3.208" f="18.571" m="0.178592" cg="179.5"/>
<eng-data t="3.259" f="0." m="0." cg="179.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="H219T" Type="single-use" dia="38." len="155." initWt="261."
propWt="144." delays="14" auto-calc-mass="1" auto-calc-cg="1" avgThrust="216.985"
peakThrust="295.987" throatDia="0." exitDia="0." Itot="234.561" burn-time="1.08"
massFrac="55.17" Isp="166.1" tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1."
FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>Aerotech H219 BT DMS</comments>
<data>
<eng-data t="0." f="0." m="144." cg="77.5"/>
<eng-data t="0.009" f="88.796" m="143.755" cg="77.5"/>
<eng-data t="0.012" f="133.194" m="143.55" cg="77.5"/>
<eng-data t="0.017" f="221.318" m="143.006" cg="77.5"/>
<eng-data t="0.019" f="243.517" m="142.721" cg="77.5"/>
<eng-data t="0.04" f="256.971" m="139.495" cg="77.5"/>
<eng-data t="0.104" f="278.497" m="128.975" cg="77.5"/>
<eng-data t="0.112" f="295.987" m="127.564" cg="77.5"/>
<eng-data t="0.124" f="275.806" m="125.458" cg="77.5"/>
<eng-data t="0.203" f="276.479" m="112.066" cg="77.5"/>
<eng-data t="0.294" f="273.116" m="96.7138" cg="77.5"/>
<eng-data t="0.4" f="264.371" m="79.2254" cg="77.5"/>
<eng-data t="0.499" f="254.28" m="63.4642" cg="77.5"/>
<eng-data t="0.6" f="241.499" m="48.0938" cg="77.5"/>
<eng-data t="0.65" f="234.772" m="40.7841" cg="77.5"/>
<eng-data t="0.698" f="226.027" m="33.9947" cg="77.5"/>
<eng-data t="0.74" f="213.918" m="28.3229" cg="77.5"/>
<eng-data t="0.8" f="191.719" m="20.8521" cg="77.5"/>
<eng-data t="0.842" f="177.592" m="16.0909" cg="77.5"/>
<eng-data t="0.891" f="161.448" m="10.9914" cg="77.5"/>
<eng-data t="0.937" f="150.685" m="6.5841" cg="77.5"/>
<eng-data t="0.957" f="151.357" m="4.72983" cg="77.5"/>
<eng-data t="0.971" f="133.867" m="3.50411" cg="77.5"/>
<eng-data t="0.999" f="91.487" m="1.56724" cg="77.5"/>
<eng-data t="1.024" f="44.398" m="0.524474" cg="77.5"/>
<eng-data t="1.04" f="21.526" m="0.200701" cg="77.5"/>
<eng-data t="1.055" f="8.072" m="0.0644216" cg="77.5"/>
<eng-data t="1.081" f="0." m="0." cg="77.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="J99N" Type="reloadable" dia="54." len="231." initWt="899."
propWt="556." delays="1000" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="92.951" peakThrust="144.305" throatDia="0." exitDia="0." Itot="929.51"
burn-time="10." massFrac="61.85" Isp="170.47" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<data>
<eng-data t="0." f="0." m="556." cg="115.5"/>
<eng-data t="0.031" f="117.296" m="554.912" cg="115.5"/>
<eng-data t="0.078" f="135.045" m="551.365" cg="115.5"/>
<eng-data t="0.242" f="144.305" m="537.663" cg="115.5"/>
<eng-data t="0.828" f="131.38" m="489.346" cg="115.5"/>
<eng-data t="2.539" f="110.737" m="365.448" cg="115.5"/>
<eng-data t="3.594" f="102.056" m="298.305" cg="115.5"/>
<eng-data t="4.82" f="94.146" m="226.362" cg="115.5"/>
<eng-data t="5.938" f="86.043" m="166.112" cg="115.5"/>
<eng-data t="7.523" f="81.22" m="86.8216" cg="115.5"/>
<eng-data t="8.984" f="76.976" m="17.6964" cg="115.5"/>
<eng-data t="9.047" f="74.082" m="14.8502" cg="115.5"/>
<eng-data t="9.547" f="16.012" m="1.37743" cg="115.5"/>
<eng-data t="9.711" f="5.209" m="0.336546" cg="115.5"/>
<eng-data t="9.82" f="1.929" m="0.103847" cg="115.5"/>
<eng-data t="10." f="0." m="0." cg="115.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="L1940X" Type="reloadable" dia="75." len="560.4"
initWt="3855.51" propWt="1823.43" delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1869.65" peakThrust="2289.18" throatDia="0." exitDia="0."
Itot="4317.02" burn-time="2.31" massFrac="47.29" Isp="241.42" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>from TMT document and posted thrust curve</comments>
<data>
<eng-data t="0." f="0." m="1823.43" cg="280.2"/>
<eng-data t="0.02" f="48.137" m="1823.23" cg="280.2"/>
<eng-data t="0.04" f="2107.33" m="1814.12" cg="280.2"/>
<eng-data t="0.055" f="2289.18" m="1800.2" cg="280.2"/>
<eng-data t="0.073" f="2150.12" m="1783.32" cg="280.2"/>
<eng-data t="0.156" f="2101.99" m="1708.79" cg="280.2"/>
<eng-data t="0.397" f="2150.12" m="1492.37" cg="280.2"/>
<eng-data t="0.691" f="2155.47" m="1225.03" cg="280.2"/>
<eng-data t="0.982" f="2118.03" m="962.398" cg="280.2"/>
<eng-data t="1.41" f="2000.36" m="590.138" cg="280.2"/>
<eng-data t="1.696" f="1898.74" m="354.63" cg="280.2"/>
<eng-data t="1.935" f="1839.9" m="165.923" cg="280.2"/>
<eng-data t="2.06" f="1818.51" m="69.3452" cg="280.2"/>
<eng-data t="2.103" f="1652.7" m="37.8224" cg="280.2"/>
<eng-data t="2.116" f="1374.58" m="29.5111" cg="280.2"/>
<eng-data t="2.133" f="935.998" m="21.2155" cg="280.2"/>
<eng-data t="2.163" f="534.856" m="11.8966" cg="280.2"/>
<eng-data t="2.214" f="240.685" m="3.54346" cg="280.2"/>
<eng-data t="2.244" f="112.32" m="1.30692" cg="280.2"/>
<eng-data t="2.296" f="5.349" m="0.0146856" cg="280.2"/>
<eng-data t="2.309" f="0." m="0." cg="280.2"/>
</data>
</engine>
<engine mfg="Aerotech" code="I40N-P" Type="reloadable" dia="38." len="203."
initWt="358.336" propWt="195.044" delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="37.821" peakThrust="95.015" throatDia="0." exitDia="0." Itot="377.419"
burn-time="9.98" massFrac="54.43" Isp="197.32" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>rough average of TMT burns 1-3 with steps removed</comments>
<data>
<eng-data t="0." f="0." m="195.044" cg="101.5"/>
<eng-data t="0.021" f="58.159" m="194.728" cg="101.5"/>
<eng-data t="0.134" f="95.015" m="190.256" cg="101.5"/>
<eng-data t="0.289" f="94.589" m="182.662" cg="101.5"/>
<eng-data t="0.371" f="89.476" m="178.762" cg="101.5"/>
<eng-data t="0.485" f="51.555" m="174.608" cg="101.5"/>
<eng-data t="1.072" f="41.116" m="160.552" cg="101.5"/>
<eng-data t="2.155" f="38.56" m="138.255" cg="101.5"/>
<eng-data t="2.845" f="38.347" m="124.544" cg="101.5"/>
<eng-data t="3.619" f="37.282" m="109.418" cg="101.5"/>
<eng-data t="4.433" f="36.429" m="93.9144" cg="101.5"/>
<eng-data t="5.474" f="35.151" m="74.6605" cg="101.5"/>
<eng-data t="6.144" f="34.725" m="62.5634" cg="101.5"/>
<eng-data t="6.794" f="34.725" m="50.8989" cg="101.5"/>
<eng-data t="7.433" f="34.299" m="39.5022" cg="101.5"/>
<eng-data t="7.969" f="33.66" m="30.09" cg="101.5"/>
<eng-data t="8.794" f="32.382" m="16.0117" cg="101.5"/>
<eng-data t="9.546" f="31.743" m="3.55152" cg="101.5"/>
<eng-data t="9.979" f="0." m="0." cg="101.5"/>
</data>
</engine>
<engine mfg="Aerotech" code="J615ST" Type="reloadable" dia="54." len="230.1"
initWt="805." propWt="373." delays="20" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="613.757" peakThrust="829.659" throatDia="0." exitDia="0." Itot="762.9"
burn-time="1.24" massFrac="46.34" Isp="208.56" tDiv="10" tStep="-1." tFix="1"
FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"
cgStep="-1." cgFix="1">
<comments>from TMT thrustcurve posted on TRF;</comments>
<data>
<eng-data t="0." f="0." m="373." cg="115.05"/>
<eng-data t="0.003" f="2.405" m="372.998" cg="115.05"/>
<eng-data t="0.025" f="21.643" m="372.869" cg="115.05"/>
<eng-data t="0.037" f="829.659" m="370.372" cg="115.05"/>
<eng-data t="0.052" f="726.253" m="364.666" cg="115.05"/>
<eng-data t="0.093" f="668.537" m="350.686" cg="115.05"/>
<eng-data t="0.174" f="680.561" m="323.972" cg="115.05"/>
<eng-data t="0.369" f="719.038" m="257.253" cg="115.05"/>
<eng-data t="0.532" f="728.657" m="199.567" cg="115.05"/>
<eng-data t="0.688" f="704.609" m="144.908" cg="115.05"/>
<eng-data t="0.851" f="649.299" m="90.958" cg="115.05"/>
<eng-data t="0.953" f="589.178" m="60.0764" cg="115.05"/>
<eng-data t="1.031" f="531.463" m="38.708" cg="115.05"/>
<eng-data t="1.113" f="478.557" m="18.4613" cg="115.05"/>
<eng-data t="1.166" f="387.174" m="7.24449" cg="115.05"/>
<eng-data t="1.198" f="254.91" m="2.22161" cg="115.05"/>
<eng-data t="1.212" f="122.645" m="0.929442" cg="115.05"/>
<eng-data t="1.243" f="0." m="0." cg="115.05"/>
</data>
</engine>
<engine mfg="Aerotech" code="N1975W-PS" Type="reloadable" dia="98." len="1110."
initWt="12206.1" propWt="7674.74" delays="0" auto-calc-mass="1" auto-calc-cg="1"
avgThrust="1884.94" peakThrust="2816.63" throatDia="0." exitDia="0."
Itot="13822.3" burn-time="7.33" massFrac="62.88" Isp="183.65" tDiv="10"
tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
<comments>average of TMT burns 1 and 2</comments>
<data>
<eng-data t="0." f="0." m="7674.74" cg="555."/>
<eng-data t="0.08" f="1985.38" m="7630.65" cg="555."/>
<eng-data t="0.217" f="2638.02" m="7454.8" cg="555."/>
<eng-data t="0.819" f="2699.85" m="6562.69" cg="555."/>
<eng-data t="1.237" f="2768.55" m="5928.1" cg="555."/>
<eng-data t="1.663" f="2816.63" m="5267.56" cg="555."/>
<eng-data t="2.137" f="2802.89" m="4528.07" cg="555."/>
<eng-data t="2.651" f="2672.37" m="3746.76" cg="555."/>
<eng-data t="3.245" f="2404.44" m="2909.55" cg="555."/>
<eng-data t="4.032" f="2054.08" m="1935.41" cg="555."/>
<eng-data t="4.602" f="1854.86" m="1316.84" cg="555."/>
<eng-data t="5.229" f="1531.97" m="727.3" cg="555."/>
<eng-data t="5.39" f="1353.36" m="598.334" cg="555."/>
<eng-data t="5.566" f="1071.69" m="479.842" cg="555."/>
<eng-data t="5.863" f="796.901" m="325.769" cg="555."/>
<eng-data t="6.161" f="604.546" m="209.825" cg="555."/>
<eng-data t="6.297" f="563.327" m="165.73" cg="555."/>
<eng-data t="6.763" f="316.013" m="51.968" cg="555."/>
<eng-data t="6.996" f="199.225" m="18.6393" cg="555."/>
<eng-data t="7.333" f="0." m="0." cg="555."/>
</data>
</engine>
</engine-list>
</engine-database>
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