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. Sheet 38/240 Non hazmat H123 equivalalent AeroTech Pro-SU 29mm H135 14sec adjustable delay. From Tripoli Data Sheet updated 2013/02/10 Created by Robert Belknap 2013/03/04 AT H170 Metalstorm for 38-360 From AT DMS announcement May 2014. 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. By Tobin Yehle, 11/11/07. Greg Gardner - 09/15/06 Greg Gardner - 09/15/06 AT H115 Dark Matter DMS H178-14 Dark Matter AT H550 ST DMS From AT DMS announcement May 2014. 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. Aerotech I115W from TRA Cert Data AT I140W DMS Aerotech I170G from TRA Cert Data Created by Mark Hairfield 12-29-10 38/360 Non hazmat I161W equivalalent From AT DMS announcement May 2014. Aerotech I215R from TRA Cert Data From Aerotech pre-cert data. Created 11/11/07 by Jim Yehle. Aerotech I350-10R single use motor file created using Aerotech instruction sheet data and thrust tracer utility. Aerotech I49N-P At DMS I500T Aerotech I599N from TRA Cert Data Aerotech I59WN-P 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 Aerotech I117FJ from TRA Cert Data Entered by Jim Yehle from TRA cert document Converted from RASP file by Chris Kobel mfr data Curvefit to instruction sheet on Aerotech website (12/27/06) I280DM DMS I305FJ based on Aerotech instruction sheet by C. Kobel 3/30/07 I327-14 Dark Matter 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 J270W DMS AT J340 Metalstorm for 38-720 From AT DMS announcement May 2014. Taken from Aerotech curves, not cert docs. Jim Yehle 15 Nov 07 Certified 8/26/2018 TMT Aerotech J825R AT 54-852 Greg Gardner - 09/15/06 This is the J1799N. It was a replacement for the J1999N. Aerotech J250FJ from TRA Cert Data Input by Tim Van Milligan using ThrustCurve Tracer by John Coker. Data from Tripoli certification paperwork dated 25 November 2007. 38mm DMS Certified 5-19-18 AeroTech K185W Copyright Tripoli Motor Testing 1998 (www.tripoli.org) provided by ThrustCurve.org (www.thrustcurve.org) AeroTech K250W Copyright Tripoli Motor Testing 1998 (www.tripoli.org) provided by ThrustCurve.org (www.thrustcurve.org) 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. From AT Instruction Sheet by C. Kobel 3/12/10 revised per AT post on TRF 5/19/14 AT K540 Metalstorm 54-1706 AeroTech K650T Copyright Tripoli Motor Testing 1998 (www.tripoli.org) provided by ThrustCurve.org (www.thrustcurve.org) 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. AeroTech K700W Copyright Tripoli Motor Testing 1998 (www.tripoli.org) provided by ThrustCurve.org (www.thrustcurve.org) AeroTech K780R provided by ThrustCurve.org (www.thrustcurve.org) AeroTech K1050W-SU Copyright Tripoli Motor Testing 1998 (www.tripoli.org) provided by ThrustCurve.org (www.thrustcurve.org) K1103X Propellant X Entered by Jim Yehle from TRA cert document 98-2560 Greg Gardner - 09/15/06 AeroTech K375 From RASP file created by C. Kobel 3/12/10 Converted to RockSim 9 by R. Geer 3/22/10 K456 Dark Matter Input by Tim Van Milligan using ThrustCurve Tracer by John Coker. Data from Tripoli certification paperwork dated 25 November 2007. Cert data from TRA Converted from Mark Koelsch Aerotech K850DM DMS Aerotech K990DM 54/2800 K2050 Super Thunder Entered by Tim Van Milligan. Used John Coker's ThrustCurve Tracer software and data supplied by Aerotech thrust stand data. Aerotech L400W-PS created using TCtracer and AT thrustcurve per AT announcement 5/8/14 AT L1090w 54-2800 AeroTech L1150 provided by ThrustCurve.org (www.thrustcurve.org) Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve Tracer program. Thrust curve and engine data from Aerotech thrust stand. AeroTech L1500T Copyright Tripoli Motor Testing 1998 (www.tripoli.org) provided by ThrustCurve.org (www.thrustcurve.org) Based on AT Instruction Sheet by C. Kobel 12/22/2010 Curvefit of Aerotech Instructions by C. Kobel 11/19/08 L875 Dark Matter DMS L900 Dark Matter L1040 Dark Matter Entered by Tim Van Milligan for RockSim Users. Used John Coker's ThrustCurve Tracer software and TRA cert paperwork dated 10-14-08. 75-6400 case Greg Gardner - 10/25/07 M685W-PS Moonburner 98-10240 case Greg Gardner - 10/25/07 M1305 Metalstorm 98 White Lightning DMS Curvefit of AeroTech Instructions by C. Kobel 11/19/08 75-7680 case Greg Gardner - 10/25/07 Entered by Tim Van Milligan for RockSim Users. Used John Coker's ThrustCurve Tracer software and TRA cert paperwork dated 10-14-08. AeroTech M2500T Copyright Tripoli Motor Testing 1998 (www.tripoli.org) provided by ThrustCurve.org (www.thrustcurve.org) M1075 Dark Matter Entered by Tim Van Milligan. Used John Coker's ThrustCurve Tracer software and data from TRA certification dated 10-14-08 98/10240 Super Thunder @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 AeroTech N2000W Copyright Tripoli Motor Testing 1997 (www.tripoli.org) provided by ThrustCurve.org (www.thrustcurve.org) AeroTech N4800T provided by ThrustCurve.org (www.thrustcurve.org) 38mm DMS Super Thunder data from TMT certification, tested April 22, 2020 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 AeroTech F52C, data from TMT test firing AeroTech H13ST, data from TMT test firing Aerotech K400C DMS Aerotech H219 BT DMS from TMT document and posted thrust curve rough average of TMT burns 1-3 with steps removed from TMT thrustcurve posted on TRF; average of TMT burns 1 and 2