diff --git a/data/Aerotech.rse b/data/Aerotech.rse new file mode 100755 index 0000000..a17f491 --- /dev/null +++ b/data/Aerotech.rse @@ -0,0 +1,9008 @@ + + + + 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. + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + 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. + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + + + + + + + + + + +Based On NAR Test Data +12/23/93 + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +@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 + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + +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 + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +Input by Tim Van Milligan based on NAR Certification document Jan 14, 2009 +Created using Thrust Curve Tracer. + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +Curve fit of AT Instruction Sheet by C. Kobel 7/29/08 + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + +F44W Economax + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +Curve Fit From AT Instruction Sheet by C. Kobel 5/2/18 +delay times assumed by adjusting provided 10-sec delay grain + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + + + +From AT Instruction Sheet by C. Kobel 1/4/11 + + + + + + + + + + + + + + + + + + + + + + + + + + +Curve Fit From AT Instruction Sheet by C. Kobel 5/2/18 +delay times assumed by adjusting provided 10-sec delay grain + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +Curve Fit From AT Instruction Sheet by C. Kobel 5/2/18 +delay times assumed by adjusting provided 10-sec delay grain + + + + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +@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 + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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 + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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 + + + + + + + + + + + + + + + + + + + + + + + + + + +NAR Test Data +March 23, 2007 + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +G71R based on Aerotech instruction sheet by C. Kobel 3/29/07 + + + + + + + + + + + + + + + + + + + + + + + + +G74W Economax + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +29mm Aerotech G75 Metal Storm single use + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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 + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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 + + + + + + + + + + + + + + + + + + + + + + + + +@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 + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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 + + + + + + + + + + + + + + + + + + + + + + + + + +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 + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +At DMS G125 + + + + + + + + + + + + + + + + + + + + +AeroTech G138T +from the reload instruction sheet 08/11/2010 +Created by Scott Sager 10/10/2010 + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +Created from TRA Certification Record issued 23 Nov 2006 +Bill Wagstaff - 04/30/07 + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + +G53FJ based on Aerotech instruction sheet by C. Kobel 12/9/07 + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +G80 New Blue Thunder + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +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. + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +From AT DMS announcement May 2014. + + + + + + + + + + + + + + + + +AeroTech H55W +Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +provided by ThrustCurve.org (www.thrustcurve.org) + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +H100W DMS + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + + +Data Entered by Tim Van Milligan +For RockSim Users. http://www.rocksim.com +Based on Aerotech's RMS 38/240-360 Black Jack Instr. 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