From 3d1b519abb7e89593f2e9ad1b34aba2ffcf75718 Mon Sep 17 00:00:00 2001 From: SiboVG Date: Sun, 12 Feb 2023 23:39:19 +0000 Subject: [PATCH] Add RASAero motor files --- .../thrustcurves/RASAero/RASAero_Motors.eng | 21689 ++++++++++++++++ .../datafiles/thrustcurves/RASAero/README.txt | 2 + 2 files changed, 21691 insertions(+) create mode 100644 core/resources/datafiles/thrustcurves/RASAero/RASAero_Motors.eng create mode 100644 core/resources/datafiles/thrustcurves/RASAero/README.txt diff --git a/core/resources/datafiles/thrustcurves/RASAero/RASAero_Motors.eng b/core/resources/datafiles/thrustcurves/RASAero/RASAero_Motors.eng new file mode 100644 index 000000000..a5d937a21 --- /dev/null +++ b/core/resources/datafiles/thrustcurves/RASAero/RASAero_Motors.eng @@ -0,0 +1,21689 @@ +;Aerotech D9 RASP.ENG file made from NAR published data +;File produced July 4, 2000 +;Submitted to ThrustCurve.org by Chris Kobel (3/29/07) +;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. +D9W 24 70 4-7 0.0101001 0.045 AT +0.1 13.7 +0.15 15.4 +0.2 16.3 +0.25 16.8 +0.35 17.2 +0.4 17.2 +0.5 16.8 +0.65 15.9 +0.8 14.5 +1.1 9.2 +1.25 7 +1.4 4.8 +1.6 2.5 +1.9 0 +; +;Aerotech D13 RASP.ENG file made from NAR published data +;File produced July 4, 2000 +;Submitted to ThrustCurve.org by Chris Kobel (3/29/07) +;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. +D13W 18 70 4-7-10 0.0098 0.0326 AT +0.03 13.462 +0.061 21.171 +0.085 20.618 +0.127 21.605 +0.158 21.042 +0.182 22.306 +0.217 22.592 +0.227 23.61 +0.248 21.891 +0.279 23.155 +0.317 22.039 +0.366 21.338 +0.383 21.901 +0.449 20.648 +0.462 21.486 +0.48 19.947 +0.507 19.947 +0.521 20.509 +0.559 18.693 +0.58 19.118 +0.66 17.578 +0.743 15.337 +0.861 12.406 +0.947 9.329 +1.068 5.834 +1.155 4.158 +1.172 4.72 +1.231 2.762 +1.328 1.928 +1.404 1.093 +1.52 0 +; +;Aerotech D15 RASP.ENG file made from NAR published data +;File produced July 4, 2000 +;Submitted to ThrustCurve.org by Chris Kobel (3/29/07) +;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. +D15T 24 70 4-6-8 0.0089 0.044 AT +0.014 11.48 +0.049 26.272 +0.081 30.087 +0.107 31.261 +0.121 31.249 +0.159 31.36 +0.208 31.249 +0.283 29.583 +0.439 23.353 +0.551 18.484 +0.675 13.43 +0.863 6.422 +0.938 3.892 +1.01 2.335 +1.085 0.778 +1.142 0.389 +1.15 0 +; +;Aerotech D21 RASP.ENG file made from NAR published data +;File produced July 4, 2000 +;Submitted to ThrustCurve.org by Chris Kobel (3/29/07) +;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. +D21T 18 70 4-7 0.0096 0.025 AT +0.01 1.367 +0.021 19.367 +0.029 32.12 +0.037 31.667 +0.051 30.528 +0.094 30.074 +0.115 31.213 +0.133 30.074 +0.177 30.76 +0.189 29.842 +0.203 30.528 +0.226 29.842 +0.275 28.935 +0.296 29.389 +0.331 28.027 +0.421 25.971 +0.478 24.146 +0.579 20.728 +0.659 17.774 +0.739 14.356 +0.799 9.569 +0.852 4.557 +0.899 1.139 +0.94 0 +; +;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. +D7RC 24 70 1000 0.0105002 0.0422 AT +0.036 3.336 +0.084 9.326 +0.101 10.281 +0.143 10.827 +0.213 10.99 +0.271 10.887 +0.359 10.685 +0.471 10.13 +0.506 10.342 +0.535 9.929 +0.81 8.697 +1.226 6.713 +1.589 5.138 +1.8 4.861 +2.151 4.581 +2.649 4.57 +2.696 3.887 +2.748 2.388 +2.807 0.889 +2.842 0.207 +2.87 0 +; +;AeroTech D24T (Blue Thunder) RASP.ENG file made from +;manufacturers published data. +;File was produced May 07, 2004 by Stanley_Hemphill@Hotmail.com. +;The motor is listed in the www.thrustcurve.org database as an +;engine certified by NAR, but there is "no data" at the weblink +;to the NAR file database. +;The author has created this file by extracting the manufacturers +;Thrust-Time curve from The AeroTech-2002 Catalog, and then deploting +;32 points using the distance measuring tools in Paint Shop Pro 8. +;The file was then created in RockSim 7 and the motor and static values +;were read from the RockSim Engine Editor. +;Motor Dia Len Delay Propellant Total Manufacturer +D24BT_CO_SU 18 70 4-7-10 0.0087 0.032 AT +0.038 39.6 +0.055 36.5 +0.076 34.4 +0.122 32.4 +0.164 31.1 +0.219 30.3 +0.261 29.3 +0.308 28.7 +0.329 27.9 +0.358 26.9 +0.392 25.8 +0.434 25 +0.485 24 +0.539 23.2 +0.577 22.3 +0.62 20.9 +0.666 19.6 +0.695 18 +0.721 16.5 +0.75 15.5 +0.754 14.3 +0.759 12.4 +0.76 11 +0.763 9.1 +0.7634 7.5 +0.771 5.9 +0.792 4 +0.83 2.6 +0.868 1.8 +0.9 1.1 +0.94 0 +; +;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. +E15 24 70 4-7 0.0201 0.0501 AT +0.02 23.33 +0.036 27.318 +0.058 28.84 +0.079 27.171 +0.139 25.638 +0.183 24.263 +0.237 24.106 +0.297 22.426 +0.373 21.964 +0.4 20.894 +0.443 21.355 +0.487 20.442 +0.617 19.833 +0.742 18.457 +0.812 20 +0.85 18.006 +0.899 18.467 +1.035 17.711 +1.1 16.945 +1.16 16.945 +1.377 15.736 +1.426 14.656 +1.436 16.198 +1.463 14.813 +1.55 14.361 +1.572 15.432 +1.61 13.752 +1.827 12.839 +2.126 10.098 +2.337 6.116 +2.538 1.369 +2.64 0 +; +;Aerotech E6T single use from NAR cert data +E6T 24 70 2-4-8-0 0.0215 0.0463 AT +0.011 18.085 +0.109 19.681 +0.217 16.312 +0.315 13.475 +0.457 11.348 +0.63 9.043 +0.804 7.801 +0.989 6.738 +1.272 6.028 +2 5.851 +3 5.496 +4 5.496 +4.446 4.965 +5.011 4.965 +5.533 4.787 +5.609 6.56 +5.707 4.255 +6.033 0 +; +;Based On NAR Test Data +;12/23/93 +E11J 24 70 4 0.025 0.0624 AT +0.0725446 14.3704 +0.16183 17.6296 +0.206473 18.3704 +0.418527 19.2593 +0.731027 18.3704 +1.31696 14.2222 +1.91964 9.03704 +2.51116 2.22222 +2.83 0 +; +;E15W-4,7,P from NAR data +E15W 24 70 4-7-0 0.0201 0.0502 AT +0.012 9.918 +0.018 20.205 +0.027 25.257 +0.039 28.152 +0.055 28.768 +0.088 27.29 +0.197 24.517 +0.297 22.977 +0.467 20.945 +0.561 19.959 +0.679 20.021 +0.722 19.22 +0.761 18.789 +0.807 20.021 +0.84 18.234 +0.904 18.727 +0.995 17.926 +1.034 18.172 +1.104 16.756 +1.147 17.248 +1.256 16.386 +1.377 15.77 +1.411 14.846 +1.426 16.324 +1.45 15.031 +1.547 14.353 +1.559 16.016 +1.589 13.86 +1.62 14.23 +1.693 13.121 +1.72 13.429 +1.829 12.936 +1.866 11.951 +1.944 11.951 +2.005 10.965 +2.093 10.472 +2.236 8.316 +2.26 9.055 +2.278 7.207 +2.378 4.99 +2.442 2.71 +2.499 1.602 +2.548 1.047 +2.618 0 +; +;Aerotech E16 RASP.ENG file made from NAR published data +;File produced July 4, 2000 +;Submitted to ThrustCurve.org by Chris Kobel (3/30/07) +;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. +E16W 29 124 4-7-10 0.019 0.107 AT +0.132 32.223 +0.221 37.2 +0.255 36.699 +0.306 36.699 +0.371 35.357 +0.414 33.785 +0.437 34.906 +0.472 33.785 +0.53 32.894 +0.553 31.772 +0.576 32.443 +0.638 29.309 +0.72 27.296 +0.867 23.942 +1.083 19.245 +1.273 14.319 +1.458 9.397 +1.513 8.055 +1.524 8.279 +1.555 6.936 +1.656 4.474 +1.814 1.79 +2 0 +; +;Aerotech E18 RASP.ENG file made from NAR published data +;File produced July 4, 2000 +;Submitted to ThrustCurve.org by Chris Kobel (3/29/07) +;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. +E18W 24 70 4-8-10 0.0207 0.057 AT +0.016 6.586 +0.042 18.004 +0.073 27.138 +0.098 29.815 +0.134 30.357 +0.17 30.347 +0.195 31.08 +0.236 30.347 +0.287 30.878 +0.338 30.337 +0.368 30.878 +0.404 29.795 +0.424 30.688 +0.465 29.976 +0.526 29.785 +0.592 29.063 +0.669 28.341 +0.786 26.908 +0.908 23.85 +1.025 21.163 +1.157 17.905 +1.284 14.857 +1.462 11.338 +1.66 7.106 +1.838 3.47 +2.006 1.309 +2.083 0.588 +2.14 0 +; +;Aerotech E23 RASP.ENG file made from NAR published data +;File produced July 4, 2000 +;Submitted to ThrustCurve.org by Chris Kobel (3/30/07) +;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. +E23T 29 124 5-8 0.0174 0.1039 AT +0.024 16.299 +0.035 21.959 +0.067 30.785 +0.09 35.774 +0.153 37.577 +0.2 38.22 +0.24 37.357 +0.322 37.577 +0.393 35.093 +0.534 32.378 +0.727 27.168 +0.766 26.938 +0.798 25.125 +0.908 21.729 +1.057 16.98 +1.187 12.682 +1.336 7.471 +1.45 3.169 +1.497 1.584 +1.532 0.679 +1.57 0 +; +;Aerotech E28 RASP.ENG file made from NAR published data +;File produced July 4, 2000 +;Submitted to ThrustCurve.org by Chris Kobel (3/29/07) +;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. +E28T 24 70 2-5-8 0.0184 0.0545 AT +0.01 29.862 +0.018 45.139 +0.038 47.562 +0.081 50.52 +0.106 48.953 +0.146 48.263 +0.161 48.953 +0.197 48.953 +0.242 47.562 +0.313 46.18 +0.411 43.057 +0.494 40.624 +0.527 39.583 +0.542 40.274 +0.562 38.542 +0.633 36.46 +0.683 34.377 +0.743 31.244 +0.799 29.162 +0.877 26.038 +0.97 20.832 +1.006 17.359 +1.046 11.462 +1.089 6.943 +1.132 3.819 +1.172 1.735 +1.22 0 +; +;Aerotech E30 RASP.ENG file made from NAR published data +;File produced July 4, 2000 +;Submitted to ThrustCurve.org by Chris Kobel (3/30/07) +;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. +E30T 24 70 4-7 0.0193 0.0433 AT +0.013 38.847 +0.02 45.621 +0.041 48.27 +0.059 46.502 +0.11 46.502 +0.166 45.912 +0.184 46.792 +0.217 45.912 +0.265 45.912 +0.319 45.031 +0.383 44.15 +0.482 42.089 +0.594 38.847 +0.615 39.437 +0.628 37.376 +0.684 35.314 +0.742 33.263 +0.804 30.021 +0.88 25.607 +0.962 20.014 +1.038 12.949 +1.089 7.358 +1.151 3.237 +1.186 1.176 +1.2 0 +; +;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. +E7RC 24 70 1000 0.0171 0.0484 AT +0.038 6.636 +0.063 10.056 +0.087 11.019 +0.134 11.42 +0.206 11.58 +0.312 11.149 +0.466 10.738 +0.667 9.777 +0.94 8.132 +1.223 6.281 +1.484 5.182 +1.709 4.701 +2.112 4.423 +2.776 4.279 +3.31 4.205 +3.926 4.266 +4.401 4.192 +4.638 4.258 +4.744 4.119 +5.124 3.979 +5.219 3.977 +5.266 3.156 +5.313 1.992 +5.36 0.965 +5.43 0 +; +;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. +E6-RC 24 70 1000 0.0215 0.0527 AT +0.047 10.866 +0.127 11.693 +0.19 11.9 +0.316 11.622 +0.522 10.593 +0.743 9.287 +0.996 7.842 +1.249 6.19 +1.47 5.296 +1.787 4.747 +2.372 4.471 +3.02 4.403 +3.747 4.264 +4.49 4.403 +5.375 4.333 +6.087 4.264 +6.719 4.264 +6.877 4.196 +6.957 3.783 +7.004 2.614 +7.036 1.513 +7.083 0.55 +7.12 0 +; +;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. +E12JRC 24 70 1000 0.0303 0.0594 AT +0.054 16.764 +0.095 18.33 +0.197 16.545 +0.313 16.654 +0.36 17.211 +0.401 16.316 +0.442 17.55 +0.476 16.206 +0.578 16.316 +0.666 16.764 +0.7 15.649 +0.768 16.316 +0.89 16.097 +1.019 15.649 +1.162 14.983 +1.23 14.983 +1.25 13.968 +1.291 14.754 +1.332 13.749 +1.373 14.197 +1.434 13.53 +1.488 13.749 +1.597 12.635 +1.726 11.401 +1.828 10.615 +1.889 9.613 +1.957 9.613 +1.998 8.495 +2.093 8.607 +2.277 7.042 +2.487 5.813 +3.05 0 +; +; +F10 29 92 4-6-8 0.04 0.083 AT +0.01 16.81 +0.03 22.34 +0.11 22.23 +0.26 21.49 +0.37 20 +0.47 20.21 +0.67 18.09 +0.99 15.74 +1.31 13.4 +1.81 10.85 +2.49 10.21 +3.13 8.94 +3.6 8.83 +4.11 8.62 +4.95 8.62 +5.45 8.62 +5.58 8.51 +5.88 8.72 +6.22 8.51 +6.46 8.51 +6.6 7.77 +6.71 7.02 +6.79 5.64 +6.91 3.83 +6.95 2.23 +7 0.96 +7.05 0 +; +;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. +F22 29 125 4-7 0.0463 0.1342 AT +0.014 11.527 +0.075 20.126 +0.157 26.572 +0.293 29.113 +0.382 30.278 +0.45 29.69 +0.539 30.667 +0.614 30.089 +0.662 31.15 +0.771 30.478 +0.948 29.89 +0.996 28.714 +1.078 28.136 +1.187 27.738 +1.289 26.761 +1.337 26.96 +1.412 25.984 +1.474 25.008 +1.515 26.173 +1.542 24.808 +1.706 22.856 +1.938 20.903 +2.101 18.173 +2.129 19.338 +2.251 16.21 +2.402 13.48 +2.64 8.791 +2.961 3.32 +3.31 0 +; +;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. +F25 29 98 4-6-9 0.0388 0.0972 AT +0.039 57.631 +0.187 53.491 +0.342 51.239 +0.5 47.86 +1 33.806 +1.5 22.94 +2 10.135 +2.207 4.504 +2.69 0 +; +;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 +F27 29 83 4-8 0.0284 0.08 AT +0 4.84718 +0.0125 15.5374 +0.0175 18.8183 +0.025 22.5311 +0.0325 25.2547 +0.04 27.3204 +0.0575 30.3657 +0.0725 31.4597 +0.0975 32.2507 +0.265 35.0238 +0.295 35.9203 +0.4675 35.9684 +0.59 35.065 +0.8 32.0145 +0.825 31.2773 +0.8575 31.1102 +0.9025 29.9308 +0.955 29.7244 +1.045 27.2951 +1.085 27.2663 +1.1175 25.9881 +1.1475 26.0014 +1.235 23.2853 +1.28 22.9001 +1.3425 21.0771 +1.52 17.256 +1.8075 6.85478 +1.9175 4.16387 +2.05 1.78386 +2.1775 0.488016 +2.4225 0.44385 +2.425 0 +; +;Aerotech F32 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. +F32 24 124 5-10-15 0.0377 0.0814 AT +0.025 46.699 +0.031 51.846 +0.061 55.64 +0.085 52.868 +0.126 47.37 +0.245 45.637 +0.34 44.946 +0.394 42.873 +0.447 42.873 +0.572 41.14 +0.72 39.408 +0.744 40.78 +0.786 38.026 +1.041 35.592 +1.136 33.179 +1.177 34.541 +1.225 32.818 +1.379 31.436 +1.474 30.394 +1.635 28.311 +1.676 27.28 +1.694 29.683 +1.712 26.929 +1.854 25.537 +1.943 23.815 +2.092 21.051 +2.187 18.287 +2.276 13.82 +2.382 7.281 +2.525 2.457 +2.72 0 +; +;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. +F37 29 99 6-10-14 0.0282 0.1086 AT +0.018 7.251 +0.053 13.626 +0.088 22.331 +0.106 25.227 +0.141 26.385 +0.183 28.411 +0.26 37.685 +0.31 41.449 +0.422 44.035 +0.524 45.183 +0.59 46.47 +0.682 45.153 +0.864 43.386 +0.934 40.471 +1.042 35.23 +1.151 29.699 +1.246 25.037 +1.354 19.796 +1.445 13.397 +1.498 7.586 +1.54 3.226 +1.6 0 +; +;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. +F40 29 124 4-7-10 0.04 0.126 AT +0.015 17.776 +0.049 41.016 +0.089 58.793 +0.124 62.9 +0.148 65.173 +0.183 62.442 +0.242 68.07 +0.292 60.617 +0.321 61.524 +0.415 60.617 +0.524 58.334 +0.741 52.412 +0.87 48.314 +0.889 49.221 +0.914 47.397 +1.102 40.109 +1.285 33.728 +1.492 25.064 +1.665 15.952 +1.808 8.659 +1.942 3.19 +2.06 0 +; +;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. +F52 29 124 5-8-11 0.0366 0.1214 AT +0.012 46.899 +0.033 61.778 +0.056 69.441 +0.097 73.483 +0.115 76.636 +0.13 74.381 +0.153 74.82 +0.168 78.422 +0.182 78.95 +0.206 77.963 +0.238 77.504 +0.258 73.892 +0.314 72.974 +0.39 72.046 +0.428 70.679 +0.501 65.699 +0.565 62.975 +0.688 58.874 +0.749 56.15 +0.837 52.517 +0.901 49.793 +0.971 46.161 +1.088 39.365 +1.144 34.386 +1.173 29.417 +1.222 20.376 +1.275 13.151 +1.339 5.461 +1.389 1.838 +1.42 0 +; +;Aerotech F72 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. +F72 24 124 5-10-15 0.0368 0.0742 AT +0.012 62.586 +0.017 84.986 +0.02 98.78 +0.03 94.748 +0.05 90.152 +0.069 82.688 +0.089 85.556 +0.104 80.39 +0.136 83.255 +0.146 80.96 +0.176 82.688 +0.198 78.672 +0.213 80.96 +0.253 80.39 +0.315 80.96 +0.38 79.821 +0.429 79.241 +0.489 78.092 +0.523 78.672 +0.536 75.225 +0.675 73.496 +0.699 67.182 +0.719 68.331 +0.747 64.884 +0.769 66.033 +0.858 60.867 +0.923 52.824 +0.98 40.195 +1.012 29.864 +1.034 20.092 +1.089 11.48 +1.21 0 +; +;Aerotech F12 RASP.ENG file made from NAR published data +;File produced July 4, 2000 +;Submitted to ThrustCurve.org by Chris Kobel (4/6/07) +;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. +F12J 24 70 2-5 0.0303 0.0667 AT +0.037 20.894 +0.054 22.152 +0.101 22.152 +0.148 22.571 +0.165 23.409 +0.2 22.421 +0.281 22.142 +0.369 22.132 +0.474 22.271 +0.526 23.54 +0.549 21.982 +0.637 22.122 +0.724 21.842 +0.8 21.413 +0.823 22.251 +0.846 20.714 +0.881 21.553 +0.945 21.123 +1.021 20.704 +1.114 20.554 +1.213 19.296 +1.382 18.298 +1.481 18.019 +1.737 15.343 +1.79 17.3 +1.883 13.936 +2.051 11.26 +2.22 7.468 +2.447 3.671 +2.709 1.135 +2.93 0 +; +;Aerotech F24 RASP.ENG file made from NAR published data +;File produced July 4, 2000 +;Submitted to ThrustCurve.org by Chris Kobel (4/6/07) +;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. +F24W 24 70 4-7-10 0.0253 0.062 AT +0.033 16.442 +0.112 40.646 +0.125 41.45 +0.18 40.927 +0.245 40.626 +0.281 41.017 +0.355 40.024 +0.438 39.713 +0.543 38.227 +0.603 37.032 +0.658 33.779 +0.685 34.663 +0.726 29.934 +0.772 30.216 +0.951 26.953 +1.071 25.166 +1.107 23.088 +1.185 21.311 +1.383 17.144 +1.649 10.91 +1.828 5.869 +1.938 2.903 +1.988 2.306 +2.048 1.412 +2.13 0 +; +;Aerotech F39 RASP.ENG file made from NAR published data +;File produced July 4, 2000 +;Submitted to ThrustCurve.org by Chris Kobel (4/6/07) +;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. +F39T 24 70 3-6-9 0.0227 0.059 AT +0.01 45.057 +0.016 54.131 +0.046 58.321 +0.079 59.47 +0.103 58.311 +0.13 57.253 +0.172 55.491 +0.235 53.738 +0.321 51.271 +0.363 50.566 +0.387 49.509 +0.408 50.203 +0.426 48.804 +0.453 47.746 +0.48 47.041 +0.68 41.059 +0.716 39.649 +0.752 38.944 +0.809 36.487 +0.86 34.382 +0.893 33.324 +0.917 32.619 +1 28.752 +1.075 25.247 +1.105 22.095 +1.126 17.201 +1.144 13.001 +1.174 8.109 +1.219 4.606 +1.261 2.5 +1.33 0 +; +;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. +F42T 29 83 4-8 0.027 0.076 AT +0.01 68.694 +0.029 65.879 +0.202 62.5 +0.511 51.802 +0.739 43.356 +0.993 31.532 +1.02 29.279 +1.072 23.086 +1.199 9.572 +1.262 4.505 +1.319 2.815 +1.47 0 +; +;Aerotech F62T (Blue Thunder) +;AeroTech RMS-29/60 Easy Access Reloadable Motor Hardware. +;RASP.ENG file made from manufacturers catalog data. +;File produced May, 17 2004. +;The file was produced by scaling 16 data points off +;the thrust curves in the manufacturers catalog. +;The F62T cannot be found on thrustcurve.org. +;Hence the amateur file production. +;The file was created by Stan Hemphill. +;Contact at stanley_hemphill@hotmail.com. +;Motor Dia Len Delay Prop Gross Mfg +F62T 29 99 6-8-9-10-11-13-14-16-18 0.025 0.109 AT +0.0046 53.6364 +0.0416 55.2727 +0.0909 58.3636 +0.1356 61.6364 +0.1649 64.9091 +0.1864 67.6364 +0.5085 67.6364 +0.5701 64.7273 +0.6687 60 +0.7427 55.0909 +0.7982 49.6364 +0.9029 48.7273 +0.9492 24.7273 +0.9661 20.1818 +0.9985 0 +; +; +F20EJ 29 83 4-7 0.03 0.0746 AT +0.01 52.08 +0.03 49.81 +0.06 46.98 +0.1 45.56 +0.15 44.49 +0.18 45.55 +0.21 43.42 +0.24 43.78 +0.32 43.77 +0.36 44.11 +0.44 43.04 +0.45 40.58 +0.53 39.86 +0.62 38.08 +0.76 36.3 +0.8 37.35 +0.84 34.88 +0.89 36.99 +0.9 33.46 +1.03 30.61 +1.06 32.02 +1.09 29.55 +1.23 26 +1.32 22.45 +1.35 23.16 +1.36 21.39 +1.58 16.42 +1.8 11.1 +2.01 6.48 +2.19 3.63 +2.39 1.13 +2.68 0 +; +;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. +F26FJ 29 98 6-9 0.0431 0.1007 AT +0.041 38.289 +0.114 36.318 +0.293 34.347 +0.497 32.939 +0.774 32.376 +1 31.25 +1.254 28.716 +1.498 25.338 +1.743 22.241 +2.003 17.737 +2.077 15.484 +2.304 5.349 +2.484 1.689 +2.61 0 +; +;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. +F13RCJ 32 107 1000 0.0323 0.1105 AT +0.048 15.309 +0.084 18.629 +0.143 19.98 +0.311 18.968 +0.538 18.172 +0.729 17.138 +0.992 15.428 +1.279 13.828 +1.673 12.456 +1.984 11.879 +2.044 12.227 +2.139 11.313 +2.378 11.193 +2.51 11.084 +2.558 12.108 +2.641 10.855 +2.976 10.736 +3.49 10.627 +3.873 10.507 +3.992 10.965 +4.028 10.627 +4.41 10.507 +4.625 10.736 +4.769 9.941 +4.829 8.684 +4.865 6.742 +4.96 3.199 +5.02 1.485 +5.1 0 +; +;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. +F16RCJ 32 107 1000 0.0625 0.1404 AT +0.046 26.35 +0.116 22.388 +0.139 21.374 +0.185 21.886 +0.22 20.54 +0.301 19.696 +0.498 18.35 +0.579 19.194 +0.637 16.492 +0.718 18.35 +0.834 18.35 +0.95 18.35 +1.054 19.194 +1.147 17.848 +1.181 18.853 +1.263 17.336 +1.436 18.009 +1.633 17.165 +1.784 17.336 +1.865 18.682 +1.934 16.834 +1.981 17.336 +2.178 16.332 +2.375 16.332 +2.502 18.18 +2.664 15.659 +2.896 15.488 +3.29 13.8 +3.718 11.611 +4.181 9.426 +4.888 5.891 +5.69 0 +; +;Aerotech F21W (White Lightning) RASP.ENG file. +;File produced Jun 22 2004. +;The file was produced by scaling data points off the +;thrust curve in the Tripoli.org motor pdf file. +;The F21W cannot be found on thrustcurve.org. +;Hence the amateur file production. +;The file was created by Stan Hemphill +;Contact at stanley_hemphill@hotmail.com +;Motor ## Dia Len Delays Prop Motor Company +F21WL_CO_SU 24 96 6-8 0.03 0.064 AT +0.0045 37.2266 +0.009 42.1474 +0.018 42.504 +0.027 40.5071 +0.0337 38.8669 +0.0427 38.225 +0.0517 37.7258 +0.0607 36.87 +0.072 36.4422 +0.0877 36.4422 +0.1102 35.3724 +0.135 35.8716 +0.1552 35.4437 +0.1732 36.2282 +0.2025 35.6577 +0.2452 37.2979 +0.2835 36.5848 +0.3195 38.0111 +0.3375 37.4406 +0.3757 38.5816 +0.396 38.225 +0.4297 39.3661 +0.4454 38.0111 +0.4747 38.7242 +0.4882 37.7971 +0.5084 38.1537 +0.5354 38.5103 +0.5647 37.9398 +0.5849 37.2266 +0.6007 37.8685 +0.6389 36.87 +0.6704 37.1553 +0.7649 35.9429 +0.9201 32.9477 +1.0056 30.309 +1.0709 29.7385 +1.2643 24.0333 +1.2868 24.0333 +1.3723 20.8241 +1.3926 20.8241 +1.5883 15.4754 +1.6108 15.4754 +2.0112 5.0634 +2.1192 3.4231 +2.2407 2.4247 +2.378 1.4976 +2.4927 0.9271 +2.5152 0 +; +;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. +F23-RC-SK 32 107 1000 0.0378 0.1287 AT +0.042 22.644 +0.133 28.191 +0.161 27.261 +0.189 29.57 +0.252 31.419 +0.343 32.578 +0.399 32.348 +0.441 33.737 +0.476 30.729 +0.539 33.507 +0.609 34.197 +0.777 34.886 +0.826 34.656 +0.896 36 +0.938 34.656 +1.015 34.656 +1.071 34.197 +1.12 33.038 +1.218 32.578 +1.267 29.81 +1.351 29.34 +1.393 27.731 +1.54 26.802 +1.645 24.263 +1.799 21.255 +1.862 19.866 +2.051 15.479 +2.317 11.552 +2.618 6.7 +2.884 3.234 +3.185 1.386 +3.47 0 +; +;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. +G25 29 124 5-10-15 0.0625 0.1197 AT +0.035 30.499 +0.047 36.712 +0.059 41.18 +0.13 40.669 +0.177 38.969 +0.295 38.969 +0.343 40.947 +0.413 40.38 +0.437 38.69 +0.484 39.824 +0.532 37.845 +0.65 37.557 +0.721 38.969 +0.803 38.69 +0.85 37.279 +0.98 39.535 +1.063 36.434 +1.098 38.124 +1.252 37.845 +1.37 37.279 +1.583 37 +1.819 35.3 +1.984 33.61 +2.185 31.344 +2.315 28.809 +2.622 24.286 +3.024 18.917 +3.39 13.838 +3.839 7.624 +4.323 4.518 +4.783 2.541 +5.3 0 +; +;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. +G33 29 124 5-7 0.0722 0.1593 AT +0.027 22.642 +0.061 42.201 +0.117 47.354 +0.243 46.678 +0.34 46.339 +0.438 47.384 +0.48 50.92 +0.508 46.359 +0.543 47.732 +0.662 45.693 +0.851 42.28 +1.039 41.266 +1.116 42.987 +1.193 39.226 +1.221 42.31 +1.312 38.888 +1.326 40.609 +1.479 38.221 +1.675 35.157 +1.843 32.77 +1.878 36.888 +1.899 32.093 +1.997 30.382 +2.13 26.622 +2.263 23.547 +2.444 19.11 +2.591 13.977 +2.752 8.502 +2.892 4.743 +3.053 2.014 +3.27 0 +; +;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. +G54 29 124 6-10-14 0.046 0.1365 AT +0.018 10.953 +0.042 39.215 +0.083 66.888 +0.14 72.075 +0.223 74.958 +0.25 76.694 +0.282 80.156 +0.315 79.577 +0.336 79.577 +0.354 81.64 +0.365 77.841 +0.374 80.724 +0.389 76.694 +0.455 76.116 +0.523 74.39 +0.639 70.928 +0.722 67.467 +0.82 64.005 +0.897 58.817 +0.992 51.894 +1.084 43.824 +1.197 34.017 +1.268 28.251 +1.283 29.987 +1.295 27.104 +1.328 23.642 +1.366 16.719 +1.399 9.803 +1.435 4.612 +1.51 0 +; +;Aerotech G55 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. +G55 24 117 5-10-15 0.0625 0.1148 AT +0.009 81.136 +0.014 84.65 +0.034 80.557 +0.084 77.064 +0.13 71.823 +0.18 72.422 +0.206 68.919 +0.342 69.538 +0.483 68.989 +0.513 66.663 +0.543 68.42 +0.664 66.114 +0.876 66.164 +0.901 64.418 +0.997 65.026 +1.062 66.793 +1.088 63.879 +1.148 63.889 +1.158 66.813 +1.173 63.31 +1.209 62.741 +1.325 61.593 +1.395 59.277 +1.456 57.541 +1.486 58.129 +1.587 52.32 +1.708 40.094 +1.824 26.11 +1.95 15.63 +2.112 7.498 +2.258 3.446 +2.44 0 +; +;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. +G64 29 124 4-8-10 0.0625 0.1512 AT +0.014 54.325 +0.032 81.488 +0.059 98.31 +0.101 85.021 +0.165 83.847 +0.274 85.614 +0.37 87.39 +0.476 86.798 +0.503 91.516 +0.517 85.614 +0.585 83.847 +0.723 80.896 +0.745 82.07 +0.773 77.945 +0.883 75.576 +0.988 74.401 +1.093 69.673 +1.262 61.412 +1.28 61.994 +1.326 58.451 +1.372 54.907 +1.422 47.238 +1.505 34.841 +1.591 23.027 +1.701 13.581 +1.829 7.085 +1.902 4.133 +1.966 1.771 +2.09 0 +; +;Exported using ThrustCurveTool, www.ThrustGear.com +;NAR S&T Data, contributed by John DeMar +G72 29 124 4-7-10 0.06 0.144 AT +0.004 4.2403 +0.006 9.6831 +0.016 54.397 +0.03 98.17 +0.034 108.509 +0.04 121.159 +0.048 133.047 +0.058 142.348 +0.068 147.209 +0.082 149.393 +0.112 146.89 +0.15 138.783 +0.17 136.039 +0.376 112.222 +0.466 103.079 +0.482 104.438 +0.56 92.6523 +0.606 92.8669 +0.644 84.2058 +0.748 73.9389 +0.76 74.2841 +0.79 69.704 +0.804 70.6 +0.822 66.7591 +0.856 62.6853 +1.154 39.9972 +1.374 19.9105 +1.474 12.5198 +1.574 7.41771 +1.78 1.19026 +2 0 +; +;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 +G80 29 124 4-7-10 0.0574 0.1049 AT +0.006 101.291 +0.013 105.18 +0.031 103.473 +0.038 104.069 +0.067 99.803 +0.103 96.906 +0.181 94.733 +0.271 94.039 +0.303 96.985 +0.367 95.547 +0.428 94.842 +0.456 97.055 +0.463 92.65 +0.51 94.872 +0.596 93.444 +0.606 95.646 +0.624 91.985 +0.635 95.656 +0.646 91.995 +0.696 90.547 +0.846 85.477 +0.96 80.388 +1.071 74.564 +1.207 62.878 +1.296 52.639 +1.35 37.252 +1.382 20.397 +1.418 10.139 +1.457 4.281 +1.5 0 +; +;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. +G40W 29 124 4-7-10 0.0538 0.123 AT +0.024 74.325 +0.057 67.005 +0.252 65.879 +0.5 63.063 +0.765 60.248 +1 54.054 +1.25 47.298 +1.502 36.599 +1.751 25.338 +1.999 12.951 +2.121 3.941 +2.3 0 +; +;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 +G61W 38 106.7 6-10-14 0.0613 0.1904 AT +0.008 3.083 +0.054 71.348 +0.089 72.229 +0.174 75.312 +0.216 78.394 +0.247 79.716 +0.502 81.037 +0.753 77.073 +1.001 72.669 +1.132 66.944 +1.252 55.933 +1.503 38.316 +1.754 10.13 +1.905 3.523 +2.04 0 +; +;Aerotech G67R (Redline) +;AeroTech RMS-38/120 EZ Access Reloadable Motors (New! Hardware). +;New AeroTech Redline Motor. Just announced on AeroTech's Website! +;File produced 28 Feb 2005. +;The file was produced by scaling data points off the +;thrust curve in the manufacturers catalog sheet. +;The motor is not yet on www.thrustcurve.org. +;Hence the amateur file production. +;The file was created by Stan Hemphill. +;Contact at stanley_hemphill@hotmail.com. +;Motor Dia Len Delay Prop Gross Mfg +G67R 38 106 4-6-8-9-10-12-13-15-17 0.0576 0.191 AT +0.04 4.92 +0.05 6.56 +0.06 9.84 +0.07 16.41 +0.08 32.81 +0.1 49.22 +0.13 68.08 +0.15 76.29 +0.18 80.39 +0.24 82.85 +0.26 85.31 +0.31 87.77 +0.51 89.41 +0.53 91.05 +0.56 87.77 +0.6 86.95 +0.61 88.59 +0.67 86.95 +0.69 85.31 +0.71 86.95 +0.72 85.31 +0.74 86.13 +0.77 85.31 +0.81 82.03 +0.95 78.75 +1.05 73.82 +1.43 53.32 +1.5 52.5 +1.52 50.86 +1.54 45.94 +1.62 11.48 +1.64 0 +; +;Submitted to ThrustCurve.org by Chris Kobel (4/13/07) +;G69N based on Aerotech instruction sheet by C. Kobel 3/29/07 +G69N 38 106 0 0.0622 0.195 AT +0.02 51.972 +0.05 75.574 +0.1 76.709 +0.2 77.617 +0.3 79.206 +0.4 81.475 +0.5 84.425 +0.6 86.922 +0.7 88.737 +0.8 89.645 +0.9 91.688 +1 93.503 +1.1 94.411 +1.2 94.638 +1.3 93.957 +1.35 93.05 +1.4 89.418 +1.5 62.865 +1.6 33.362 +1.65 19.518 +1.7 12.028 +1.75 7.489 +1.8 4.539 +1.9 1.816 +2 0 +; +;G71R based on Aerotech instruction sheet by C. Kobel 3/29/07 +G71R 29 124 4-7-10 0.0569 0.147 AT +0 0.389 +0.05 109.714 +0.1 117.884 +0.2 113.216 +0.3 109.714 +0.4 105.045 +0.5 99.21 +0.6 92.207 +0.7 83.258 +0.8 75.477 +0.9 68.085 +1 57.97 +1.1 47.465 +1.2 33.848 +1.3 21.009 +1.4 11.283 +1.5 5.447 +1.6 2.334 +1.7 0 +; +;Aerotech G75J (Black Jack) +;AeroTech RMS-29/180 Easy Access Reloadable Motor Hardware. +;RASP.ENG file made from made from NAR or TMT published data. +;File produced May, 17 2004. +;The total impulse, peak thrust, average thrust and burn time are +;the same as the averaged static test data from NAR or TMT files. +;The curve drawn with these data points is as accurate as could +;could be made scaling the data from the curve on the TMT html +;page. The file is 63 data points. NOT wRASP v1.6 compatible. +;The file was created by Stan Hemphill. +;Contact at stanley_hemphill@hotmail.com. +;Motor Dia Len Delay Prop Gross Mfg +G75J 29 194 1-3-4-6-7-9-10 0.114 0.236 AT +0.0281 68.8604 +0.038 78.6517 +0.0561 75.923 +0.066 73.0337 +0.0776 70.4655 +0.1139 69.3419 +0.1403 68.6998 +0.1667 67.5762 +0.1881 70.305 +0.2013 69.0209 +0.2294 72.5522 +0.2541 76.4045 +0.2723 71.4286 +0.3102 76.244 +0.335 71.9101 +0.4208 75.6019 +0.4604 72.3917 +0.5215 79.2937 +0.5941 73.3547 +0.6436 80.0963 +0.7013 73.8363 +0.7393 76.4045 +0.7541 74.6388 +0.7657 77.3676 +0.7937 78.6517 +0.8036 77.0465 +0.8168 80.2568 +0.8267 75.2809 +0.8383 81.5409 +0.8581 75.7624 +0.8795 77.8491 +0.934 74.1573 +0.9868 79.9358 +1.038 76.7255 +1.0561 72.2311 +1.0941 78.8122 +1.1221 75.6019 +1.1502 80.8989 +1.1617 76.886 +1.1848 80.0963 +1.1997 76.7255 +1.2327 78.8122 +1.2508 76.4045 +1.2871 82.504 +1.3102 77.5281 +1.3267 81.862 +1.3564 75.2809 +1.3729 80.0963 +1.4076 75.7624 +1.4884 79.9358 +1.5116 73.6758 +1.5297 81.0594 +1.5512 74.6388 +1.5611 80.8989 +1.604 72.8732 +1.7211 75.6019 +1.7607 68.6998 +1.7789 70.1445 +1.8119 66.9342 +1.8267 70.7865 +1.8482 70.7865 +2.3878 0 +; +;Aerotech G77R (Redline) +;AeroTech RMS-29/120 EZ Access Reloadable Motors (New! Hardware). +;New AeroTech Redline Motor. Just announced on AeroTech's Website! +;File produced 28 Feb 2005. +;The file was produced by scaling data points off the +;thrust curve in the manufacturers catalog sheet. +;The motor is not yet on www.thrustcurve.org. +;Hence the amateur file production. +;The file was created by Stan Hemphill. +;Contact at stanley_hemphill@hotmail.com. +;Motor Dia Len Delay Prop Gross Mfg +G77R 29 150 4-6-8-9-10-12-13-15-17 0.0554 0.155 AT +0.0132 14.8333 +0.0243 32.4479 +0.0331 46.3542 +0.0375 52.8438 +0.0463 56.5521 +0.0617 59.3333 +0.258 73.2396 +0.6548 87.1458 +0.8709 89 +0.8885 85.2917 +1.0252 86.2188 +1.0472 84.3646 +1.0715 86.2188 +1.1002 84.3646 +1.1332 85.2917 +1.195 76.9479 +1.2104 76.0208 +1.2369 65.8229 +1.2611 43.5729 +1.2898 27.8125 +1.3317 12.0521 +1.3625 4.6354 +1.4 0 +; +;@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 +G78G 29 146 4-7-10 0.0597 0.125 AT +0.004 2.76203 +0.006 34.7707 +0.008 44.326 +0.01 41.2789 +0.012 28.5933 +0.014 27.3926 +0.016 38.0574 +0.02 47.7036 +0.022 48.2012 +0.03 56.4344 +0.042 61.4034 +0.06 65.883 +0.212 84.526 +0.266 88.9218 +0.404 95.5932 +0.43 98.9746 +0.466 100.536 +0.58 102.242 +0.694 101.319 +0.86 95.4526 +1.1 90.4186 +1.132 82.5618 +1.156 72.6383 +1.168 64.903 +1.194 42.3389 +1.216 28.3424 +1.226 24.9802 +1.2559 17.4005 +1.2859 13.0465 +1.3819 5.05295 +1.4719 0 +; +;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 +G79W 29 149.86 6-10-14 0.0609 0.154 AT +0.015 7.157 +0.074 91.937 +0.09 91.387 +0.114 84.781 +0.145 84.23 +0.201 89.185 +0.291 94.69 +0.4 98.544 +0.6 99.645 +0.708 96.892 +0.8 93.038 +0.915 85.331 +1 77.624 +1.085 71.017 +1.175 68.265 +1.199 44.59 +1.28 22.021 +1.36 4.955 +1.42 0 +; +;Aerotech G80T 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 G80T motors. +G80T 29 124 4-7-10 0.0479 0.1161 AT +0.016 110.761 +0.049 100.648 +0.195 98.537 +0.472 96.425 +0.635 90.091 +0.798 82.348 +0.99 63.345 +1.121 38.711 +1.215 18.3 +1.287 5.56 +1.41 0 +; +; +G101T 29 114.3 5-8-12 0.046 0.136 AT +0.01 35.29 +0.02 63.97 +0.02 78.09 +0.03 84.71 +0.04 89.96 +0.06 93.96 +0.12 97.26 +0.17 99.14 +0.21 101.73 +0.27 104.09 +0.31 104.56 +0.36 103.62 +0.4 103.38 +0.45 101.03 +0.51 99.27 +0.53 94.41 +0.56 93.09 +0.64 87.35 +0.76 78.53 +0.8 75.88 +0.88 68.82 +0.89 65.73 +0.9 61.32 +0.91 55.15 +0.93 35.73 +0.94 32.65 +0.95 22.5 +0.98 10.59 +1 5.29 +1.05 0 +; +;Aerotech G104T (Blue Thunder) +;AeroTech RMS-29/100 EZ Access Reloadable Motors. +;File produced 28 Feb 2005. +;The file was produced by scaling data points off the +;thrust curve in the manufacturers catalog sheet. +;The motor is not yet on www.thrustcurve.org. +;Hence the amateur file production. +;The file was created by Stan Hemphill. +;Contact at stanley_hemphill@hotmail.com. +;Motor Dia Len Delay Prop Gross Mfg +G104T 29 124 6-8-9-10-11-13-14-16-18 0.0408 0.136 AT +0.0067 125.343 +0.0471 123.542 +0.0856 121.967 +0.1019 121.405 +0.1462 121.18 +0.1837 120.842 +0.2029 120.504 +0.2385 118.817 +0.2644 117.242 +0.2798 116.904 +0.3279 116.679 +0.3923 116.679 +0.4298 116.116 +0.4615 114.091 +0.5067 110.153 +0.5404 104.64 +0.576 96.201 +0.6067 89.5626 +0.6817 78.8736 +0.7692 67.9595 +0.7865 64.9216 +0.799 62.5588 +0.8058 58.0582 +0.8192 50.5196 +0.8385 39.043 +0.8625 27.5664 +0.8769 16.6523 +0.9019 0 +; +;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. +G12RC 32 107 1000 0.0511 0.131 AT +0.03 18.549 +0.117 19.96 +0.239 20.64 +0.362 20.111 +0.519 18.982 +0.694 17.138 +0.886 15.02 +1.131 13.186 +1.375 11.915 +1.689 11.069 +2.021 10.363 +2.422 10.232 +3.172 9.677 +4.114 9.267 +5.039 8.857 +6.137 8.733 +7.132 8.607 +7.795 8.335 +7.952 8.196 +8.074 8.055 +8.179 6.924 +8.319 4.661 +8.476 1.973 +8.55 0 +; +;38-120 +;Created from TRA Certification Record issued 23 Nov 2006 +;Bill Wagstaff - 04/30/07 +G339N 38 97 0 0.049 0.19 AT +0.009 371 +0.05 375 +0.1 375 +0.15 364 +0.2 349 +0.25 310 +0.3 264 +0.324 257 +0.342 39 +0.359 0 +; +; +G35EJ 29 98 4-7 0.05 0.1005 AT +0.01 39.14 +0.02 76.22 +0.05 64.46 +0.13 57.54 +0.21 57.53 +0.24 64.43 +0.25 57.06 +0.35 56.12 +0.43 55.2 +0.48 57.49 +0.51 52.41 +0.55 53.33 +0.76 50.54 +0.91 50.06 +1.11 44.96 +1.32 41.24 +1.55 35.68 +1.6 36.13 +1.63 33.36 +1.67 34.28 +1.8 30.12 +2 25.02 +2.14 21.32 +2.23 19.46 +2.3 15.77 +2.41 9.76 +2.53 6.52 +2.65 3.74 +2.74 1.88 +2.91 0 +; +;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. +G38FJ 29 124 4-7 0.0597 0.1264 AT +0.024 52.928 +0.171 48.424 +0.497 45.045 +1 42.23 +1.279 39.978 +1.498 36.599 +1.783 30.406 +2.011 23.086 +2.272 10.135 +2.467 3.941 +2.64 0 +; +;G53FJ based on Aerotech instruction sheet by C. Kobel 12/9/07 +G53FJ 29 124 5-7-10 0.06 0.152 AT +0.012 44.898 +0.031 71.504 +0.064 80.234 +0.081 83.976 +0.1 86.47 +0.15 84.599 +0.2 81.897 +0.3 78.571 +0.4 76.493 +0.5 73.583 +0.6 70.881 +0.7 67.347 +0.8 63.813 +0.9 60.072 +1 54.667 +1.1 47.392 +1.2 39.909 +1.3 32.426 +1.4 25.983 +1.5 20.578 +1.6 10.601 +1.7 3.949 +1.8 1.247 +1.85 0 +; +;AeroTech H45W +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +H45W 38 194 0 0.193984 0.294784 AT +0.141 62.554 +0.424 63.504 +0.707 65.913 +0.992 68.37 +1.276 69.315 +1.559 68.523 +1.843 67.231 +2.127 65.705 +2.411 63.154 +2.695 59.21 +2.979 55.6 +3.264 50.79 +3.547 45.237 +3.83 39.835 +4.115 34.562 +4.399 29.213 +4.682 24.72 +4.967 20.616 +5.251 17.475 +5.534 14.498 +5.818 12.697 +6.102 10.792 +6.386 9.229 +6.67 7.754 +6.954 6.075 +7.239 0 +; +;AeroTech H55W +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +H55W 29 191 0 0.09856 0.18816 AT +0.052 92.752 +0.159 98.019 +0.268 95.821 +0.375 96.162 +0.482 97.146 +0.591 96.927 +0.699 95.915 +0.806 94.447 +0.914 92.001 +1.022 88.756 +1.129 86.97 +1.236 84.072 +1.345 80.172 +1.453 74.343 +1.56 64.99 +1.668 46.38 +1.776 32.835 +1.883 25.734 +1.991 19.92 +2.099 16.229 +2.207 13.059 +2.315 10.451 +2.422 7.7 +2.53 5.696 +2.639 3.979 +2.747 0 +; +;AeroTech H70W +;Copyright Tripoli Motor Testing 1997 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +H70W 29 229 0 0.11648 0.224 AT +0.055 114.847 +0.169 131.427 +0.283 126.879 +0.397 127.136 +0.51 127.254 +0.625 125.894 +0.739 124.917 +0.852 122.031 +0.967 119.032 +1.08 115.071 +1.194 108.446 +1.308 102.273 +1.422 96.098 +1.535 86.953 +1.65 75.702 +1.764 62.402 +1.877 48.132 +1.992 36.862 +2.105 28.065 +2.219 21.592 +2.333 16.894 +2.447 12.686 +2.56 9.681 +2.675 6.818 +2.79 4.488 +2.904 0 +; +;AeroTech H73J +;Copyright Tripoli Motor Testing 1997 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +H73J 38 152 6 0.14784 0.30912 AT +0.056 49.252 +0.172 82.004 +0.287 82.13 +0.403 84.596 +0.52 86.883 +0.635 88.888 +0.751 89.652 +0.867 91.342 +0.982 92.98 +1.099 94.571 +1.215 94.641 +1.33 93.549 +1.446 91.447 +1.561 88.189 +1.678 82.436 +1.794 77.397 +1.909 70.772 +2.025 61.173 +2.141 51.161 +2.257 38.54 +2.373 21.562 +2.489 12.213 +2.604 7.327 +2.72 3.706 +2.836 1.777 +2.953 0 +; +;AeroTech H97J +;Copyright Tripoli Motor Testing 1997 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +H97J 29 238 6 0.1344 0.27776 AT +0.045 89.405 +0.136 100.289 +0.228 100.463 +0.32 102.019 +0.411 102.813 +0.503 103.55 +0.595 101.701 +0.686 103.056 +0.778 103.331 +0.87 102.613 +0.961 103.394 +1.053 100.963 +1.145 101.226 +1.236 99.864 +1.328 98.42 +1.42 96.827 +1.511 95.034 +1.603 93.241 +1.695 93.485 +1.786 88.068 +1.878 64.358 +1.97 30.264 +2.061 8.691 +2.153 1.399 +2.245 0.525 +2.336 0 +; +;AeroTech H112J +;Copyright Tripoli Motor Testing 1999 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +H112J 38 202 0 0.187712 0.379456 AT +0.064 85.431 +0.194 101.938 +0.324 101.897 +0.454 102.839 +0.584 104.479 +0.715 103.845 +0.845 103.439 +0.975 104.286 +1.106 104.922 +1.236 104.39 +1.367 102.768 +1.497 102.237 +1.627 100.032 +1.757 98.345 +1.888 94.56 +2.018 89.018 +2.148 82.857 +2.279 77.685 +2.409 72.373 +2.54 67.041 +2.67 59.764 +2.8 37.616 +2.93 14.457 +3.06 4.642 +3.192 1.818 +3.323 0 +; +;AeroTech H123W +;Copyright Tripoli Motor Testing 1999 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +H123W 38 154 0 0.126336 0.278656 AT +0.047 96.764 +0.143 146.256 +0.239 150.699 +0.334 152.496 +0.43 151.248 +0.526 149.875 +0.622 150.2 +0.718 149.176 +0.814 144.858 +0.909 143.536 +1.005 141.414 +1.101 135.125 +1.198 125.288 +1.295 114.035 +1.391 101.556 +1.486 90.175 +1.582 78.694 +1.678 66.364 +1.774 54.26 +1.87 46.872 +1.966 38.186 +2.061 22.737 +2.157 13.478 +2.253 7.587 +2.35 5.252 +2.447 0 +; +;AeroTech H125W +;Copyright Tripoli Motor Testing 1997 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +H125W-29mm 29 330 14 0.18816 0.32256 AT +0.053 275.994 +0.161 241.473 +0.27 216.283 +0.378 199.482 +0.488 188.758 +0.597 182.349 +0.705 175.862 +0.814 169.365 +0.922 162.281 +1.031 154.276 +1.141 143.915 +1.249 133.48 +1.357 123.007 +1.466 113.058 +1.575 101.801 +1.684 88.423 +1.793 73.53 +1.901 60.425 +2.009 46.643 +2.119 36.785 +2.228 29.546 +2.336 23.641 +2.445 18.794 +2.553 14.728 +2.663 10.97 +2.772 0 +; +; +H125W-38mm 38 191 6-10-14 0.1462 0.225 AT +0.05 100 +0.5 167 +1.53 129 +2 145 +2.56 0 +; +; +H128W 29 195 6-10-14 0.0922 0.2145 AT +0 0.62 +0.1 157.28 +0.2 129.75 +0.3 129.75 +0.4 125.26 +0.5 125.26 +0.9 125.26 +1 120.81 +1.2 102.93 +1.3 44.75 +1.4 8.94 +1.5 0 +; +;AeroTech H148R +;provided by ThrustCurve.org (www.thrustcurve.org) +H148R 38 152 0 0.14784 0.30912 AT +0.027 77.232 +0.088 174.296 +0.148 185.046 +0.208 190.458 +0.268 192.497 +0.327 191.996 +0.388 188.79 +0.448 187.548 +0.509 182.697 +0.57 178.151 +0.63 172.906 +0.69 169.607 +0.75 164.51 +0.81 158.375 +0.87 153.019 +0.93 146.81 +0.991 139.443 +1.053 132.001 +1.112 123.271 +1.173 112.559 +1.233 104.737 +1.292 97.657 +1.353 94.932 +1.413 60.644 +1.474 13.007 +1.535 0 +; +;AeroTech H165R +;provided by ThrustCurve.org (www.thrustcurve.org) +H165R 29 194 0 0.0896 0.2016 AT +0.018 55.047 +0.059 157.258 +0.101 168.509 +0.144 173.219 +0.186 179.237 +0.229 183.947 +0.271 187.872 +0.314 188.134 +0.356 188.919 +0.399 190.488 +0.441 187.349 +0.484 189.18 +0.525 186.547 +0.566 185.517 +0.609 180.807 +0.651 177.667 +0.694 170.602 +0.736 167.201 +0.779 158.828 +0.821 155.688 +0.864 153.333 +0.906 136.325 +0.949 73.526 +0.991 20.671 +1.034 4.448 +1.076 0 +; +;AeroTech H180W +;Copyright Tripoli Motor Testing 1997 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +H180W 29 238 6 0.12096 0.2464 AT +0.024 149.374 +0.075 222.273 +0.127 222.339 +0.178 227.835 +0.229 234.963 +0.281 238.162 +0.333 240.252 +0.384 243.126 +0.435 240.757 +0.487 240.724 +0.539 236.311 +0.59 236.799 +0.642 234.897 +0.694 232.763 +0.745 229.198 +0.796 228.816 +0.848 231.906 +0.899 225.853 +0.95 188.285 +1.002 134.679 +1.054 78.94 +1.105 34.557 +1.156 15.482 +1.208 7.279 +1.26 3.585 +1.313 0 +; +;AeroTech H210R +;provided by ThrustCurve.org (www.thrustcurve.org) +H210R 29 238 0 0.12096 0.2464 AT +0.019 105.923 +0.059 211.29 +0.099 219.77 +0.139 229.639 +0.179 235.082 +0.22 241.594 +0.26 242.706 +0.3 245.347 +0.341 249.1 +0.381 253.41 +0.421 258.553 +0.461 260.221 +0.502 257.997 +0.543 259.248 +0.583 256.607 +0.623 252.436 +0.663 245.056 +0.704 219.909 +0.744 209.344 +0.784 200.587 +0.824 193.565 +0.865 184.323 +0.905 153.881 +0.945 58.244 +0.986 13.21 +1.027 0 +; +; +H220T 29 239 6-10-14 0.1064 0.2386 AT +0 314.1 +0.1 236.61 +0.2 269.23 +0.3 261.06 +0.4 252.9 +0.72 252.9 +0.8 112.58 +0.9 9.78 +0.96 0 +; +;AeroTech H238T +;Copyright Tripoli Motor Testing 1997 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +H238T 29 194 6 0.08064 0.18816 AT +0.019 173.1 +0.059 206.876 +0.1 211.036 +0.141 214.353 +0.181 217.113 +0.222 219.343 +0.263 221.034 +0.303 224.951 +0.344 229.324 +0.384 229.308 +0.425 228.558 +0.466 226.573 +0.506 222.365 +0.547 219.205 +0.588 217.75 +0.628 213.35 +0.669 208.07 +0.709 200.966 +0.75 196.988 +0.791 151.387 +0.831 96.273 +0.872 59.475 +0.912 18.621 +0.953 7.986 +0.995 3.697 +1.036 0 +; +;AeroTech H242T +;Copyright Tripoli Motor Testing 1997 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +H242T 38 152 10 0.11648 0.2688 AT +0.03 164.06 +0.093 197.516 +0.155 204.324 +0.218 208.97 +0.28 211.481 +0.343 211.261 +0.405 209.291 +0.468 208.438 +0.531 206.707 +0.595 203.967 +0.657 198.175 +0.72 192.137 +0.782 186.84 +0.845 180.802 +0.907 174.635 +0.97 165.581 +1.033 159.726 +1.097 151.69 +1.159 144.167 +1.222 138.55 +1.284 119.114 +1.347 69.055 +1.409 21.396 +1.472 3.473 +1.535 0.594 +1.599 0 +; +;I don't know that +;these ejection +;delays are correct. +;This was made +;using the Aerotech +;test thrust curves. +;By Tobin Yehle, +;11/11/07. +H250G 29 228.93 0-6-10-14 0.1163 0.256 AT +0.00250627 88.6915 +0.0125313 177.383 +0.0300752 279.719 +0.0726817 311.103 +0.145363 320.654 +0.24812 311.103 +0.308271 297.458 +0.398496 282.448 +0.45614 270.168 +0.593985 238.785 +0.691729 221.047 +0.799499 218.318 +0.83208 210.131 +0.844612 189.663 +0.907268 13.6449 +0.92 0 +; +;AeroTech H268R +;provided by ThrustCurve.org (www.thrustcurve.org) +H268R 29 333 0 0.18368 0.3584 AT +0.022 268.095 +0.069 332.446 +0.116 312.429 +0.164 306.81 +0.211 305.757 +0.259 306.576 +0.306 312.546 +0.354 319.687 +0.401 321.234 +0.448 320.974 +0.495 321.208 +0.542 321.794 +0.59 323.315 +0.638 322.847 +0.685 307.044 +0.732 291.593 +0.779 277.713 +0.826 267.127 +0.874 257.529 +0.921 252.846 +0.969 222.645 +1.016 159.668 +1.064 108.747 +1.111 52.091 +1.159 15.569 +1.207 0 +; +;38-240 +;Greg Gardner - 09/15/06 +H669N 38 152 0 0.096 0.252 AT +0.003 141 +0.006 523 +0.009 934 +0.012 1178 +0.016 926 +0.019 684 +0.022 487 +0.025 415 +0.028 622 +0.031 801 +0.0325 906 +0.034 866 +0.037 755 +0.04 737 +0.043 666 +0.047 737 +0.0485 802 +0.05 755 +0.053 791 +0.056 765 +0.059 755 +0.062 747 +0.069 737 +0.075 761 +0.082 755 +0.088 729 +0.093 741 +0.1 751 +0.2 703 +0.25 640 +0.3 586 +0.306 584 +0.309 576 +0.312 506 +0.318 292 +0.325 93 +0.329 0 +; +;38-360 +;Greg Gardner - 09/15/06 +H999N 38 203 0 0.144 0.331 AT +0.003 204 +0.006 757 +0.009 1357 +0.012 1710 +0.016 1345 +0.019 995 +0.022 710 +0.025 606 +0.028 905 +0.031 1165 +0.0325 1311 +0.034 1258 +0.037 1098 +0.04 1072 +0.043 969 +0.047 1072 +0.0485 1166 +0.05 1098 +0.053 1160 +0.056 1117 +0.059 1103 +0.062 1093 +0.069 1076 +0.075 1110 +0.082 1105 +0.088 1065 +0.093 1082 +0.1 1092 +0.2 1022 +0.25 931 +0.3 853 +0.306 850 +0.309 838 +0.312 735 +0.318 435 +0.325 161 +0.329 0 +; +;AeroTech I65W +;Copyright Tripoli Motor Testing 1997 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +I65W 54 235 0 0.41216 0.7616 AT +0.18 125.414 +0.544 139.304 +0.908 145.369 +1.273 148.283 +1.638 146.745 +2.002 139.049 +2.367 131.2 +2.731 123.276 +3.096 113.454 +3.46 102.368 +3.825 90.21 +4.19 78.084 +4.554 66.812 +4.919 55.78 +5.283 47.281 +5.648 39.154 +6.012 32.528 +6.377 27.069 +6.742 22.099 +7.106 18.095 +7.471 14.819 +7.835 12.097 +8.2 9.763 +8.565 7.875 +8.929 5.999 +9.294 0 +; +;Aerotech I115W from TRA Cert Data +I115W 54 156 6-10-14-0 0.229 0.58 AT +0.034 12.095 +0.177 105.225 +0.206 113.087 +1.017 163.281 +1.166 161.466 +1.257 162.676 +1.343 166.909 +1.417 160.862 +1.514 162.676 +1.617 163.885 +1.686 160.257 +1.977 142.719 +2.497 106.435 +2.68 91.316 +2.994 72.569 +3.103 67.126 +3.189 65.917 +3.24 59.265 +3.291 42.937 +3.331 30.237 +3.377 20.561 +3.429 12.7 +3.491 7.257 +3.514 0 +; +;AeroTech I132W +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +I132W 38 335 0 0.365568 0.512064 AT +0.096 204.011 +0.29 174.236 +0.484 168.865 +0.679 170.783 +0.874 173.028 +1.069 174.287 +1.264 174.647 +1.458 174.364 +1.652 174.645 +1.847 173.002 +2.042 169.209 +2.236 164.309 +2.431 157.149 +2.626 149.58 +2.821 138.36 +3.016 124.171 +3.21 107.626 +3.404 89.785 +3.599 71.747 +3.794 55.124 +3.989 42.264 +4.183 31.373 +4.378 21.98 +4.573 14.389 +4.768 8.794 +4.962 0 +; +;AeroTech I154J +;Copyright Tripoli Motor Testing 1999 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +I154J 38 250 0 0.25088 0.491904 AT +0.066 120.409 +0.199 150.638 +0.332 151.666 +0.466 156.806 +0.599 150.331 +0.732 150.602 +0.866 145.101 +0.999 144.469 +1.133 145.159 +1.268 145.912 +1.401 141.71 +1.534 142.828 +1.668 141.187 +1.801 140.97 +1.934 137.832 +2.068 128.417 +2.202 122.339 +2.336 111.986 +2.47 105.295 +2.603 96.602 +2.736 90.469 +2.87 57.427 +3.003 20.489 +3.136 4.707 +3.271 2.966 +3.405 0 +; +;AeroTech I161W +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +I161W 38 191 0 0.189952 0.370048 AT +0.043 178.9 +0.131 206.77 +0.221 206.101 +0.31 205.175 +0.4 206.924 +0.49 210.603 +0.579 210.475 +0.669 211.555 +0.758 212.379 +0.848 212.096 +0.938 209.06 +1.027 202.345 +1.116 192.439 +1.204 179.499 +1.294 162.159 +1.383 148.446 +1.473 135.222 +1.563 120.095 +1.652 104.041 +1.742 87.962 +1.831 74.789 +1.921 54.362 +2.01 23.386 +2.1 7.332 +2.19 5.171 +2.279 0 +; +;AeroTech I195J +;Copyright Tripoli Motor Testing 1996 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +I195J 38 298 10 0.3136 0.59136 AT +0.05 258.67 +0.152 353.638 +0.254 300.655 +0.356 265.354 +0.458 266.338 +0.56 283.233 +0.662 332.442 +0.765 283.04 +0.867 230.795 +0.969 222.867 +1.071 217.091 +1.173 210.6 +1.275 202.722 +1.377 192.671 +1.479 182.571 +1.581 171.964 +1.683 162.238 +1.785 148.138 +1.888 130.259 +1.99 107.022 +2.092 80.23 +2.194 51.074 +2.296 26.313 +2.398 10.397 +2.5 3.977 +2.602 0 +; +;AeroTech I200W +;Copyright Tripoli Motor Testing 1999 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +I200W 29 333 0 0.181888 0.357504 AT +0.033 303.951 +0.103 273.452 +0.174 276.061 +0.245 271.625 +0.316 268.233 +0.386 258.449 +0.457 252.48 +0.528 246.642 +0.599 242.304 +0.67 237.737 +0.741 234.769 +0.811 233.171 +0.882 230.66 +0.953 224.985 +1.024 221.658 +1.095 214.548 +1.166 177.365 +1.236 154.208 +1.307 119.146 +1.378 91.586 +1.449 65.33 +1.52 32.877 +1.591 28.702 +1.661 22.211 +1.732 15.558 +1.803 0 +; +;AeroTech I211W +;Copyright Tripoli Motor Testing 1999 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +I211W 38 240 0 0.247296 0.466368 AT +0.044 257.326 +0.134 295.533 +0.226 296.087 +0.318 298.204 +0.408 295.082 +0.499 287.669 +0.591 282.578 +0.682 272.875 +0.773 266.997 +0.864 257.602 +0.955 250.495 +1.047 238.574 +1.138 228.571 +1.228 215.135 +1.32 198.047 +1.411 180.631 +1.502 161.261 +1.593 146.708 +1.684 134.484 +1.776 101.241 +1.867 52.688 +1.957 35.461 +2.049 24.321 +2.141 11.165 +2.232 4.587 +2.324 0 +; +;Aerotech I215R from TRA Cert Data +I215R 54 156 6-10-14-0 0.208 0.527 AT +0.049 88.39 +0.089 154.683 +0.094 206.914 +0.178 245.083 +0.251 255.127 +0.325 259.145 +0.404 249.1 +0.582 257.136 +0.631 253.118 +0.7 253.118 +0.774 245.083 +1.001 239.056 +1.509 192.852 +1.681 178.79 +1.716 180.799 +1.746 190.843 +1.775 178.79 +1.8 90.399 +1.82 34.151 +1.859 0 +; +;AeroTech I218R +;provided by ThrustCurve.org (www.thrustcurve.org) +I218R 38 191 0 0.19264 0.37184 AT +0.027 136.078 +0.088 275.03 +0.148 280.998 +0.208 284.371 +0.268 284.037 +0.327 279.311 +0.388 277.791 +0.448 276.309 +0.509 269.384 +0.57 266.041 +0.63 261.907 +0.69 256.366 +0.75 250.565 +0.81 242.206 +0.87 234.607 +0.93 225.488 +0.991 216.166 +1.053 205.415 +1.112 193.238 +1.173 177.206 +1.233 161.304 +1.292 139.118 +1.353 96.082 +1.413 38.848 +1.474 5.978 +1.535 0 +; +; +I229T 54 156 6-10-14 0.206 0.52 AT +0.01 44.73 +0.02 216.65 +0.19 244.72 +0.4 266.64 +0.49 266.64 +0.52 273.66 +0.59 271.9 +0.75 272.78 +0.84 268.4 +0.88 271.9 +0.97 262.26 +1 265.76 +1.07 255.24 +1.21 249.1 +1.51 219.28 +1.6 230.68 +1.63 191.21 +1.64 132.44 +1.66 86.83 +1.7 44.73 +1.71 21.05 +1.73 0 +; +;Ejection delays may not be corrrect. +;From Aerotech pre-cert data. +;Created 11/11/07 by Jim Yehle. +I245G 38 192.532 0-6-10-14 0.1813 0.365 AT +0.0244989 234.061 +0.0550162 257.888 +0.0868597 368.567 +0.106904 382.335 +0.13363 390.808 +0.200445 405.635 +0.262806 410.931 +0.302895 411.99 +0.363029 408.813 +0.401294 398.43 +0.501114 363.271 +0.594655 320.907 +0.68932 278.355 +0.797327 212.879 +0.893204 181.477 +1.00647 154.187 +1.09061 133.72 +1.16036 120.737 +1.1804 122.856 +1.23625 106.43 +1.30421 75.0467 +1.3608 36.0094 +1.40312 19.0638 +1.43875 5.2955 +1.46325 0 +; +;AeroTech I284W +;Copyright Tripoli Motor Testing 1997 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +I284W 38 298 10 0.3136 0.55552 AT +0.033 370.682 +0.103 483.606 +0.174 483.282 +0.245 486.856 +0.316 490.842 +0.386 499.428 +0.457 508.8 +0.528 506.326 +0.599 485.287 +0.67 481.043 +0.741 455.776 +0.811 426.92 +0.882 393.422 +0.953 367.404 +1.024 347.49 +1.095 325.191 +1.166 304.064 +1.236 284.158 +1.307 271.165 +1.378 228.579 +1.449 130.521 +1.52 57.212 +1.591 29.552 +1.661 16.413 +1.732 10.365 +1.803 0 +; +;AeroTech I285R +;provided by ThrustCurve.org (www.thrustcurve.org) +I285R 38 250 0 0.25088 0.4928 AT +0.027 171.405 +0.088 325.573 +0.148 341.697 +0.208 358.916 +0.268 373.706 +0.327 373.966 +0.388 368.442 +0.448 367.497 +0.507 361.9 +0.568 351.928 +0.628 346.109 +0.687 340.993 +0.749 329.382 +0.81 321.625 +0.87 310.856 +0.93 295.955 +0.99 283.704 +1.05 269.655 +1.11 253.419 +1.17 240.222 +1.23 224.116 +1.29 204.118 +1.35 118.73 +1.41 23.483 +1.471 2.046 +1.532 0 +; +; +I300T 38 250 6-10-14 0.2216 0.4405 AT +0 473.17 +0.1 395.68 +0.2 375.31 +0.3 367.14 +0.4 358.97 +0.5 346.72 +0.6 338.56 +0.7 318.19 +0.8 305.94 +0.9 295.35 +1.07 269.23 +1.1 258.01 +1.2 246.79 +1.3 179.49 +1.4 48.95 +1.5 13.91 +1.6 0 +; +;AeroTech I357T +;Copyright Tripoli Motor Testing 1997 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +I357T 38 203 14 0.1792 0.34944 AT +0.028 311.629 +0.087 351.768 +0.147 349.074 +0.206 346.175 +0.266 341.229 +0.325 336.857 +0.384 333.748 +0.444 326.96 +0.503 319.679 +0.563 312.533 +0.622 300.79 +0.681 292.787 +0.741 283.766 +0.8 274.578 +0.859 264.915 +0.919 254.273 +0.978 241.755 +1.037 229.02 +1.097 216.238 +1.156 187.776 +1.216 109.94 +1.275 56.459 +1.334 24.476 +1.394 10.977 +1.454 3.45 +1.515 0 +; +;AeroTech I366R +;provided by ThrustCurve.org (www.thrustcurve.org) +I366R 38 298 0 0.3136 0.55552 AT +0.027 323.256 +0.088 485.393 +0.148 483.744 +0.208 479.926 +0.268 473.365 +0.327 466.192 +0.388 457.444 +0.448 448.751 +0.509 441.477 +0.57 430.236 +0.63 421.524 +0.69 411.757 +0.75 398.876 +0.81 387.496 +0.87 375.43 +0.93 361.325 +0.991 345.057 +1.053 330.392 +1.112 312.636 +1.173 293.508 +1.233 275.085 +1.292 262.408 +1.353 230.881 +1.413 118.008 +1.474 23.611 +1.535 0 +; +;AeroTech I435T +;Copyright Tripoli Motor Testing 1996 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +I435T 38 298 6 0.28672 0.52864 AT +0.026 684.626 +0.08 702.334 +0.134 655.13 +0.19 638.942 +0.245 624.098 +0.299 611.802 +0.354 602.601 +0.409 590.237 +0.464 575.712 +0.519 563.654 +0.574 548.912 +0.628 527.885 +0.683 504.211 +0.739 480.412 +0.793 459.219 +0.848 436.771 +0.903 414.493 +0.957 392.151 +1.012 366.634 +1.068 299.67 +1.122 182.639 +1.177 106.457 +1.232 55.447 +1.286 23.628 +1.342 11.052 +1.397 0 +; +;Aerotech I599N from TRA Cert Data +I599N 54 156 100 0.195 0.520051 AT +0.007 179.424 +0.01 495.908 +0.012 578.144 +0.014 647.92 +0.017 797.44 +0.024 593.096 +0.032 647.92 +0.045 677.824 +0.051 702.744 +0.055 677.824 +0.062 720.188 +0.076 707.728 +0.12 752.584 +0.202 757.568 +0.225 755.076 +0.241 735.14 +0.25 720.188 +0.263 730.156 +0.329 722.68 +0.399 697.76 +0.45 667.856 +0.501 618.016 +0.536 585.62 +0.55 580.636 +0.564 585.62 +0.578 632.968 +0.581 555.716 +0.584 426.132 +0.589 299.04 +0.595 176.932 +0.598 112.14 +0.604 57.316 +0.608 24.92 +0.619 12.46 +0.623 0 +; +;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 +I600R 38 344.68 10 0.3237 0.617 AT +0.005 40.438 +0.046 817.754 +0.059 813.261 +0.1 772.822 +0.2 736.877 +0.4 696.439 +0.5 669.48 +0.6 620.055 +0.796 539.178 +0.894 485.261 +0.951 453.809 +0.964 435.836 +1 274.082 +1.052 152.767 +1.106 62.904 +1.144 13.48 +1.18 0 +; +;Aerotech I117FJ from TRA Cert Data +I117FJ 54 156 6-10-14-0 0.253 0.58 AT +0.014 65.9 +0.021 94.456 +0.055 120.816 +0.089 107.636 +0.179 107.636 +0.344 124.111 +0.385 133.996 +0.447 123.013 +0.509 138.389 +0.564 131.799 +0.646 146.077 +0.708 144.979 +0.736 127.406 +0.75 149.372 +0.798 141.684 +0.825 164.749 +0.866 152.667 +1.004 158.159 +1.141 155.962 +1.224 154.864 +1.492 155.962 +2.304 121.914 +2.407 118.619 +2.482 117.521 +2.544 128.504 +2.599 112.029 +2.654 75.784 +2.695 45.031 +2.75 16.475 +2.771 8.787 +2.806 0 +; +;Entered by Jim Yehle +;from TRA cert document +I1299N 38 249 1000 0.192 0.422 AT +0 15.7171 +0.00361 222.5 +0.0115 1112 +0.0134228 1237.11 +0.02 1287 +0.04 1359 +0.1 1451 +0.12 1470 +0.18 1491 +0.2 1483 +0.22 1462 +0.24 1399 +0.28 1208 +0.294743 1131.63 +0.3 1065 +0.304251 974.46 +0.32 305 +0.330537 55.0098 +0.333893 11.7878 +0.34 0 +; +;AeroTech I225FJ +;Curvefit to instruction sheet on Aerotech website (12/27/06) +;by Chris Kobel +;burn time: 1.8 seconds +;total impulse: 350.5 newton-seconds +;average thrust: 43.8 pounds +I225FJ 38 202 6-10-14 0.2417 0.486 AT +0.04 213.6 +0.1 213.6 +0.2 218.1 +0.28 235.9 +0.3 249.2 +0.4 262.6 +0.5 267 +0.6 271.5 +0.7 275.9 +0.8 275.9 +0.87 271.5 +0.9 258.1 +1 240.3 +1.1 218.1 +1.2 200.3 +1.3 178 +1.4 160.2 +1.5 97.9 +1.6 40.1 +1.7 13.4 +1.8 0 +; +;I305FJ based on Aerotech instruction sheet by C. Kobel 3/30/07 +I305FJ 38 298 6-10-14 0.302 0.581 AT +0.02 341.398 +0.1 365.497 +0.2 383.571 +0.3 403.653 +0.4 405.662 +0.5 405.662 +0.6 404.657 +0.7 374.534 +0.8 342.402 +0.9 309.267 +1 272.115 +1.1 238.979 +1.15 224.921 +1.2 194.798 +1.3 119.489 +1.4 62.255 +1.45 33.136 +1.5 23.095 +1.6 0 +; +;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 +I364FJ 38 345 6-10-14 0.3625 0.678 AT +0.02 356 +0.1 373.8 +0.2 387.2 +0.3 400.5 +0.4 400.5 +0.5 409.4 +0.6 413.9 +0.7 409.4 +0.8 382.7 +0.9 373.8 +1 351.6 +1.1 333.8 +1.2 320.4 +1.3 311.5 +1.4 244.8 +1.5 178 +1.6 80.1 +1.7 0 +; +;AeroTech J125 +;Copyright Tripoli Motor Testing 1997 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +J125 54 368 0 0.63392 1.288 AT +0.174 223.931 +0.525 254.842 +0.877 275.347 +1.229 285.163 +1.581 280.333 +1.933 264.476 +2.285 244.373 +2.638 223.774 +2.99 204.72 +3.342 185.434 +3.694 166.807 +4.046 147.653 +4.398 127.914 +4.75 108.483 +5.102 92.582 +5.454 77.817 +5.806 63.844 +6.158 53.017 +6.51 44.507 +6.862 37.543 +7.215 32.205 +7.567 27.212 +7.919 22.847 +8.271 18.596 +8.623 14.79 +8.975 0 +; +;AeroTech J90W +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +J90W 54 243 0 0.427392 0.852544 AT +0.143 116.187 +0.43 165.444 +0.718 176.536 +1.005 184.645 +1.293 187.242 +1.58 183.651 +1.868 175.492 +2.155 167.687 +2.443 156.858 +2.73 143.514 +3.018 128.856 +3.305 110.879 +3.593 94.003 +3.88 79.657 +4.168 67.472 +4.455 57.268 +4.743 48.008 +5.03 40.523 +5.318 33.901 +5.605 28.248 +5.893 23.334 +6.18 19.275 +6.468 15.923 +6.755 12.727 +7.044 9.903 +7.332 0 +; +; +J125W 54 368 100 0.6433 1.115 AT +1 214 +3 200 +4.01 142 +7 120 +10.24 0 +; +;AeroTech J135W +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +J135W 54 368 0 0.62272 1.14106 AT +0.147 226.295 +0.444 243.688 +0.742 250.916 +1.04 257.345 +1.338 259.308 +1.635 253.727 +1.933 246.071 +2.231 235.78 +2.529 221.775 +2.827 205.143 +3.125 183.57 +3.423 161.103 +3.72 140.983 +4.017 122.984 +4.315 106.605 +4.612 91.959 +4.91 77.693 +5.208 65.304 +5.506 54.347 +5.804 44.246 +6.102 35.395 +6.4 27.716 +6.698 21.121 +6.996 14.939 +7.294 9.737 +7.592 0 +; +;AeroTech J145H +;Copyright Tripoli Motor Testing 1999 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +J145H 54 709 0 0.410816 1.79738 AT +0.113 253.118 +0.34 293.672 +0.567 300.149 +0.794 289.519 +1.021 253.366 +1.248 251.809 +1.476 246.042 +1.704 236.553 +1.931 229.907 +2.158 222.55 +2.385 211.12 +2.612 201.066 +2.841 191.143 +3.069 139.197 +3.296 79.889 +3.523 63.9 +3.75 51.048 +3.977 40.565 +4.205 31.71 +4.433 24.429 +4.66 19.95 +4.887 15.256 +5.115 12.412 +5.342 10.212 +5.57 9.135 +5.798 0 +; +;AeroTech J180T +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +J180T 54 230 0 0.429184 0.809088 AT +0.093 301.634 +0.281 313.236 +0.47 313.71 +0.658 308.334 +0.847 300.1 +1.035 290.743 +1.224 278.867 +1.412 263.823 +1.601 245.974 +1.79 226.651 +1.978 207.345 +2.167 187.053 +2.355 168.339 +2.544 149.993 +2.732 133.094 +2.921 116.33 +3.109 100.088 +3.298 84.507 +3.486 70.453 +3.675 57.263 +3.864 44.453 +4.052 33.34 +4.241 24.654 +4.429 17.964 +4.619 12.391 +4.808 0 +; +; +J210H 54 609.6 1000 0.471 1.497 AT +0.00772798 651.819 +0.0695518 528.502 +0.200927 488.864 +0.502318 409.589 +0.996909 374.355 +1.4915 312.697 +1.59196 286.272 +2.00927 167.359 +2.43431 88.0836 +2.50386 101.296 +2.55023 74.8711 +3.02164 57.2543 +4 0 +; +;AeroTech J275W +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +J275W 54 230 0 0.468608 0.864192 AT +0.075 239.74 +0.227 289.133 +0.38 299.773 +0.533 312.721 +0.686 323.878 +0.84 332.165 +0.992 336.422 +1.145 335.11 +1.298 329.538 +1.451 325.343 +1.604 309.98 +1.756 292.901 +1.909 275.732 +2.063 257.341 +2.216 234.891 +2.369 213.102 +2.521 182.501 +2.674 167.853 +2.827 153.041 +2.98 138.115 +3.133 105.605 +3.285 67.369 +3.439 29.239 +3.592 14.599 +3.745 6.662 +3.898 0 +; +;AeroTech J315R +;provided by ThrustCurve.org (www.thrustcurve.org) +J315R 54 243 0 0.42112 0.8512 AT +0.051 189.719 +0.154 337.529 +0.259 354.534 +0.363 364.111 +0.468 371.479 +0.572 373.222 +0.676 376.062 +0.78 372.962 +0.884 368.988 +0.989 366.978 +1.093 358.752 +1.197 351.302 +1.301 339.336 +1.406 325.202 +1.51 311.322 +1.614 300.496 +1.718 288.598 +1.822 278.279 +1.927 270.538 +2.031 262.127 +2.136 245.027 +2.239 236.238 +2.344 188.308 +2.448 63.668 +2.552 18.746 +2.657 0 +; +;AeroTech J415W +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +J415W 54 314 0 0.686336 1.15718 AT +0.065 431.3 +0.196 452.427 +0.327 489.904 +0.458 513.542 +0.591 523.192 +0.723 531.44 +0.854 542.165 +0.985 542.731 +1.118 549.788 +1.25 553.889 +1.381 537.331 +1.512 512.126 +1.645 517.338 +1.777 498.098 +1.908 473.365 +2.04 444.157 +2.172 413.187 +2.304 384.854 +2.435 360.556 +2.567 297.571 +2.699 178.288 +2.831 89.889 +2.962 43.066 +3.094 19.126 +3.226 8.995 +3.358 0 +; +;AeroTech J420R +;provided by ThrustCurve.org (www.thrustcurve.org) +J420R 38 337 0 0.37632 0.6496 AT +0.031 61.083 +0.095 563.47 +0.16 525.283 +0.224 521.242 +0.288 527.371 +0.352 537.088 +0.418 535.138 +0.481 534.623 +0.545 530.245 +0.61 526.447 +0.674 517.203 +0.738 510.279 +0.802 500.887 +0.868 479.45 +0.931 460.675 +0.995 438.594 +1.06 409.647 +1.124 383.454 +1.188 361.024 +1.252 339.741 +1.318 319.194 +1.381 296.714 +1.445 195.191 +1.51 61.984 +1.575 7.22 +1.64 0 +; +;AeroTech J460T +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +J460T 54 230 0 0.413504 0.801024 AT +0.041 500.927 +0.125 509.423 +0.209 516.357 +0.294 527.752 +0.379 535.135 +0.464 541.858 +0.548 545.793 +0.633 545.678 +0.718 544.832 +0.802 540.278 +0.887 533.698 +0.972 526.34 +1.056 511.003 +1.141 492.475 +1.225 474.977 +1.31 457.021 +1.395 437.203 +1.479 418.093 +1.565 403.24 +1.649 339.173 +1.733 203.861 +1.819 102.62 +1.903 49.295 +1.987 9.538 +2.073 2.155 +2.158 0 +; +;Delays are speculation. +;Taken from Aerotech curves, not cert docs. +;Jim Yehle 15 Nov 07 +J500G 38 335.407 0-6-10-14 0.3626 0.654 AT +0.0134378 40.2458 +0.0335946 724.425 +0.0403135 781.616 +0.0604703 787.971 +0.0895857 711.716 +0.134378 686.297 +0.394177 637.578 +0.575588 588.86 +0.606943 622.751 +0.633819 620.633 +1.20045 360.094 +1.24076 345.267 +1.31019 182.165 +1.38186 65.6642 +1.43337 23.3002 +1.45 0 +; +;AeroTech J540R +;provided by ThrustCurve.org (www.thrustcurve.org) +J540R 54 314 0 0.61376 1.08416 AT +0.044 498.757 +0.134 639.617 +0.224 649.317 +0.314 657.966 +0.404 664.02 +0.494 666.924 +0.584 663.699 +0.675 658.398 +0.765 651.232 +0.855 638.505 +0.945 626.396 +1.035 612.557 +1.126 590.09 +1.216 562.391 +1.306 536.875 +1.396 511.607 +1.486 490.354 +1.576 468.978 +1.667 451.342 +1.758 430.18 +1.847 414.549 +1.937 398.116 +2.027 305.877 +2.118 55.541 +2.208 1.523 +2.299 0 +; +;AeroTech J570W +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +J570W 38 479 0 0.547904 0.886144 AT +0.039 1149.8 +0.119 1042.85 +0.199 960.891 +0.279 900.02 +0.36 837.772 +0.441 792.834 +0.521 735.51 +0.602 685.857 +0.682 649.599 +0.762 608.757 +0.844 597.35 +0.924 568.934 +1.004 548.552 +1.084 505.08 +1.165 484.626 +1.246 452.328 +1.326 362.439 +1.406 297.973 +1.487 262.381 +1.568 195.696 +1.648 156.733 +1.729 124.649 +1.809 113.749 +1.89 69.812 +1.971 46.023 +2.052 0 +; +;AeroTech J800T +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +J800T 54 314 0 0.613312 1.08595 AT +0.04 841.341 +0.121 818.497 +0.203 776.386 +0.285 784.308 +0.367 785.314 +0.449 783.315 +0.531 782.539 +0.612 779.977 +0.695 773.68 +0.777 765.307 +0.858 755.517 +0.941 744.777 +1.023 733.131 +1.105 719.947 +1.187 702.235 +1.269 685.369 +1.351 668.265 +1.433 650.327 +1.515 630.472 +1.597 615.483 +1.679 470.262 +1.76 256.617 +1.843 108.716 +1.925 15.005 +2.007 1.249 +2.09 0 +; +;Aerotech J825R +J825R 38 479 10 0.53 0.88 AT +0 11.504 +0.048913 1069.87 +0.100155 977.842 +0.118789 1035.36 +0.652174 897.314 +0.801242 839.794 +0.899068 782.274 +0.999224 586.705 +1.09938 103.536 +1.14363 23.008 +1.18 0 +; +;AeroTech 54-852 +;Greg Gardner - 09/15/06 +J1299N 54 230 0 0.3716 0.834 AT +0.01 548 +0.02 1152 +0.03 1232 +0.04 1277 +0.05 1272 +0.06 1288 +0.07 1333 +0.08 1347 +0.09 1378 +0.1 1383 +0.12 1405 +0.14 1410 +0.16 1440 +0.18 1444 +0.2 1446 +0.25 1449 +0.3 1452 +0.35 1448 +0.4 1440 +0.45 1405 +0.5 1320 +0.55 1248 +0.57 1224 +0.59 1210 +0.6 1180 +0.61 1188 +0.615 1195 +0.62 1188 +0.63 510 +0.64 220 +0.65 96 +0.66 46 +0.67 26 +0.678 0 +; +;AeroTech 54-1280 +;Greg Gardner - 09/15/06 +J1999N 54 314 0 0.5574 1.111 AT +0.01 830 +0.02 1716 +0.03 1787 +0.04 1873 +0.05 1896 +0.06 1918 +0.07 1984 +0.08 2007 +0.09 2051 +0.1 2058 +0.12 2090 +0.14 2098 +0.16 2135 +0.18 2138 +0.2 2142 +0.25 2146 +0.3 2150 +0.35 2146 +0.4 2138 +0.45 2096 +0.5 1974 +0.55 1864 +0.57 1829 +0.59 1815 +0.6 1762 +0.61 1673 +0.62 1085 +0.63 490 +0.64 190 +0.65 81 +0.66 31 +0.67 0 +; +;Aerotech J250FJ from TRA Cert Data +J250FJ 54 241 6-10-14-18 0.511 0.92 AT +0.011 132.176 +0.021 263.335 +0.084 236.899 +0.168 252.151 +0.294 238.933 +0.494 261.301 +0.715 285.703 +0.993 295.87 +1.177 306.038 +1.267 305.021 +1.498 301.971 +1.64 292.82 +2.002 253.167 +2.344 224.699 +2.391 225.715 +2.502 233.849 +2.57 185.046 +2.659 116.925 +2.685 76.255 +2.738 32.536 +2.77 17.285 +2.796 0 +; +; +J260HW 54 708.66 1000 0.558 1.574 AT +0.00772798 598.969 +0.0386399 475.651 +0.108192 506.481 +0.463679 493.268 +0.780526 475.651 +1.01236 427.205 +2.00155 330.314 +2.48841 193.784 +2.99073 114.509 +4.01082 57.2543 +4.5 0 +; +; +J575FJ 38 478.79 6-10-14 0.576 0.91424 AT +0.0156556 656.682 +0.0195695 840.689 +0.037182 840.689 +0.0606654 839.001 +0.101761 839.001 +0.162427 839.001 +0.228963 839.001 +0.315068 839.001 +0.399217 837.312 +0.459883 837.312 +0.547945 822.119 +0.60274 801.862 +0.700587 742.777 +0.802348 685.381 +0.841487 646.554 +0.902153 573.964 +0.949791 483.69 +1 319.581 +1.05365 220.66 +1.12916 153.62 +1.19961 99.5997 +1.27593 43.8914 +1.34 0 +; +; +J350W-L 38 337 0 0.361 0.651 AT +0.041 841.443 +0.051 767.077 +0.088 698.219 +0.173 644.51 +0.256 621.098 +0.298 564.635 +0.547 543.977 +0.783 487.514 +0.989 418.656 +1.16 359.438 +1.192 340.158 +1.213 320.878 +1.287 216.214 +1.319 179.031 +1.342 126.699 +1.386 84.007 +1.427 53.709 +1.48 45.446 +1.591 20.657 +1.695 0 +; +; +J390HW-TURBO 54 708.66 1000 0.69 1.74 AT +0.015456 440.418 +0.100464 550.523 +0.193199 546.118 +0.301391 656.223 +0.502318 647.414 +0.973725 581.352 +1.48377 471.247 +1.98609 378.759 +2.17929 334.718 +2.30294 255.442 +2.49614 158.55 +3.01391 57.2543 +3.5 0 +; +;AeroTech K185W +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +K185W 54 437 0 0.827008 1.43405 AT +0.15 279.128 +0.452 308.22 +0.754 328.435 +1.056 338.929 +1.359 339.677 +1.663 333.166 +1.965 321.891 +2.267 309.687 +2.57 293.26 +2.873 271.536 +3.175 247.174 +3.477 216.883 +3.78 186.951 +4.083 161.096 +4.385 138.113 +4.688 117.749 +4.991 99.372 +5.294 82.759 +5.596 68.426 +5.898 55.126 +6.201 44.162 +6.504 34.209 +6.806 25.064 +7.108 16.88 +7.411 9.2 +7.715 0 +; +;AeroTech K250W +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +K250W 54 673 0 1.52902 2.21133 AT +0.199 365.33 +0.599 403.324 +0.999 418.669 +1.4 409.813 +1.801 408.949 +2.201 412.146 +2.602 411.952 +3.003 409.488 +3.403 393.214 +3.804 373.599 +4.205 348.913 +4.605 328.463 +5.006 307.163 +5.407 281.467 +5.807 249.011 +6.208 217.159 +6.609 185.908 +7.009 149.19 +7.41 119.808 +7.811 92.096 +8.211 69.726 +8.613 52.613 +9.014 35.876 +9.414 16.727 +9.815 4.086 +10.216 0 +; +;Aerotech K270W-P Moon Burner from TRA Certification Data +K270W 54 579 0 1.188 2.1 AT +0.046 177.061 +0.062 292.932 +0.092 425.727 +0.154 414.01 +0.277 389.273 +0.446 377.556 +0.585 381.462 +0.738 372.349 +1 377.556 +1.154 376.254 +1.231 378.858 +1.308 395.783 +1.4 380.16 +1.569 399.689 +1.615 381.462 +1.846 381.462 +2.369 368.443 +2.415 381.462 +2.554 360.631 +3.015 350.216 +3.354 328.083 +3.723 300.743 +4 273.403 +4.6 225.232 +5.262 175.759 +5.677 144.513 +6 124.984 +6.538 89.832 +7.015 66.398 +8 22.133 +8.323 10.415 +8.508 5.208 +8.692 0 +; +;AeroTech K458W +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +K458W 98 275 0 1.42778 3.16378 AT +0.133 294.911 +0.403 404.808 +0.674 462.021 +0.944 515.863 +1.214 555.072 +1.484 583.153 +1.755 600.299 +2.025 610.254 +2.295 618.543 +2.566 623.155 +2.835 618.885 +3.105 589.082 +3.376 546.307 +3.647 505.042 +3.917 451.412 +4.186 391.651 +4.457 338.409 +4.727 288.429 +4.997 245.814 +5.268 208.209 +5.539 178.153 +5.808 149.825 +6.078 62.931 +6.349 8.427 +6.62 2.562 +6.891 0 +; +;AeroTech K550W +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +K550W 54 410 0 0.919744 1.48736 AT +0.065 604.264 +0.196 642.625 +0.327 682.197 +0.458 732.995 +0.591 758.236 +0.723 780.289 +0.854 794.452 +0.985 797.939 +1.117 797.601 +1.249 773.842 +1.381 711.608 +1.512 646.522 +1.644 590.724 +1.775 537.505 +1.907 491.012 +2.04 445.836 +2.171 401.461 +2.302 364.291 +2.433 319.614 +2.566 255.577 +2.698 172.573 +2.829 103.501 +2.96 51.795 +3.092 26.814 +3.224 15.203 +3.356 0 +; +;AeroTech K560W +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +K560W 75 396 0 1.40806 2.71354 AT +0.096 552.123 +0.29 645.403 +0.484 681.109 +0.679 716.167 +0.874 742.678 +1.069 764.778 +1.264 775.71 +1.458 785.859 +1.653 789.305 +1.848 789.077 +2.043 744.622 +2.237 676.886 +2.432 614.711 +2.627 557.908 +2.822 503.641 +3.017 455.504 +3.211 412.045 +3.406 372.963 +3.601 335.987 +3.796 307.346 +3.991 279.856 +4.185 223.491 +4.38 70.441 +4.575 10.028 +4.77 2.445 +4.965 0 +; +;AeroTech K650T +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +K650T 98 289 0 1.27008 2.9353 AT +0.079 514.338 +0.24 594.264 +0.401 618.849 +0.563 641.658 +0.723 665.057 +0.884 686.488 +1.046 704.685 +1.206 720.215 +1.368 730.072 +1.529 736.891 +1.69 743.109 +1.851 747.503 +2.013 747.557 +2.174 744.081 +2.335 732.294 +2.496 710.412 +2.657 682.67 +2.819 653.246 +2.979 627.02 +3.141 595.456 +3.302 563.844 +3.463 551.08 +3.624 236.059 +3.785 1.383 +3.947 1.234 +4.108 0 +; +;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. +K680R 98 289 1000 1.316 3.035 AT +0.085 629.798 +0.494 717.881 +0.996 797.157 +1.29 819.178 +1.506 819.178 +2.001 775.136 +2.519 673.84 +2.99 563.735 +3.137 541.714 +3.176 532.906 +3.238 563.735 +3.276 563.735 +3.408 52.85 +3.431 22.02 +3.49 0 +; +;AeroTech K695R +;provided by ThrustCurve.org (www.thrustcurve.org) +K695R 54 410 0 0.9184 1.48736 AT +0.044 618.611 +0.134 727.84 +0.224 751.996 +0.314 812.48 +0.404 900.125 +0.495 884.763 +0.585 873.457 +0.675 864.561 +0.765 849.672 +0.856 838.886 +0.946 822.55 +1.036 806.24 +1.126 781.342 +1.216 753.973 +1.307 728.472 +1.398 697.629 +1.487 672.979 +1.578 646.66 +1.667 620.897 +1.758 595.574 +1.849 571.72 +1.939 546.822 +2.029 272.824 +2.119 57.95 +2.209 4.509 +2.3 0 +; +;AeroTech K700W +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +K700W 54 568 0 1.29158 2.03526 AT +0.069 1005.47 +0.209 1018.92 +0.35 1026.61 +0.491 1028.64 +0.632 1029.34 +0.773 1004.2 +0.914 970.694 +1.055 946.516 +1.196 918.437 +1.336 873.783 +1.478 821.276 +1.619 773.27 +1.759 735.553 +1.9 692.732 +2.041 658.984 +2.182 626.737 +2.323 591.431 +2.464 508.666 +2.605 420.175 +2.746 328.309 +2.886 202.409 +3.028 121.672 +3.169 80.453 +3.309 50.873 +3.451 31.548 +3.593 0 +; +;AeroTech K780R +;provided by ThrustCurve.org (www.thrustcurve.org) +K780R 75 289 0 1.26784 2.9344 AT +0.053 383.29 +0.173 718.241 +0.292 849.343 +0.413 885.503 +0.533 903.243 +0.652 924.403 +0.772 938.825 +0.892 938.623 +1.013 947.13 +1.133 953.578 +1.253 944.001 +1.373 935.448 +1.495 929.447 +1.617 920.379 +1.737 897.293 +1.857 888.917 +1.977 861.127 +2.098 840.971 +2.217 812.36 +2.337 779.614 +2.457 747.866 +2.578 726.819 +2.697 729.258 +2.817 279.891 +2.94 10.969 +3.063 0 +; +;AeroTech K1050W +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +K1050W 54 676 0 1.34714 2.12845 AT +0.049 1305.65 +0.149 1270.39 +0.249 1288.92 +0.349 1327.06 +0.449 1345.72 +0.549 1359.79 +0.649 1364.45 +0.749 1365.49 +0.849 1377.19 +0.949 1379.52 +1.049 1346.59 +1.149 1286.74 +1.249 1232.1 +1.349 1186.48 +1.449 1156.52 +1.549 1120.05 +1.649 1098.71 +1.749 1070.19 +1.849 889.885 +1.949 646.691 +2.049 441.213 +2.149 302.245 +2.249 155.001 +2.349 52.187 +2.449 43.415 +2.549 0 +; +;AeroTech K1100T +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +K1100T 54 398 0 0.7616 1.32518 AT +0.034 1234.65 +0.105 1233.43 +0.176 1192.39 +0.247 1163.04 +0.318 1147.96 +0.389 1146.32 +0.46 1140.96 +0.532 1132.64 +0.603 1123.82 +0.674 1108.92 +0.745 1090.97 +0.816 1073.94 +0.887 1049.13 +0.959 1021.22 +1.03 994.559 +1.101 966.571 +1.172 940.194 +1.243 909.792 +1.315 880.264 +1.386 844.477 +1.457 643.599 +1.528 401.861 +1.599 145.498 +1.67 28.372 +1.742 0 +; +;AeroTech K1275R +;provided by ThrustCurve.org (www.thrustcurve.org) +K1275R 54 569 0 1.29024 2.03392 AT +0.039 1282.62 +0.119 1557.99 +0.199 1540.2 +0.279 1526.78 +0.359 1500.69 +0.44 1456.58 +0.52 1425.79 +0.6 1390.42 +0.68 1355.11 +0.761 1323.31 +0.841 1282.83 +0.921 1247.8 +1.001 1194.42 +1.081 1150.98 +1.162 1108.22 +1.242 1068.75 +1.322 1036.92 +1.403 997.444 +1.482 964.569 +1.563 933.305 +1.644 889.992 +1.724 599.467 +1.804 134.559 +1.884 5.63 +1.964 0.205 +2.045 0 +; +;Entered by Jim Yehle +;from TRA cert document +K1499N 75 260 1000 0.604 1.741 AT +0.01 1450 +0.2 1720.12 +0.35 1700 +0.5 1600 +0.6 1575 +0.7 1500 +0.82 1400 +0.84 250 +0.88 0 +; +;AeroTech K1999N +;Curvefit to instruction sheet on Aerotech website (1/29/07) +;by Chris Kobel +;burn time: 1.4 seconds +;total impulse: 2522 newton-seconds +;average thrust: 405 pounds +K1999N 98 289 6-10-14-18 1.195 2.989 AT +0.02 1557.5 +0.08 1780 +0.1 1913.5 +0.12 1869 +0.18 2002.5 +1.08 2002.5 +1.1 1958 +1.2 1780 +1.25 1557.5 +1.27 1335 +1.31 890 +1.33 667.5 +1.35 222.5 +1.4 0 +; +;AeroTech K485HW +;Copyright Tripoli Motor Testing 1999 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +K485HW 54 699 0 0.910784 2.22029 AT +0.075 454.453 +0.227 568.735 +0.38 831.332 +0.533 825.584 +0.686 795.935 +0.84 759.473 +0.992 727.238 +1.145 680.051 +1.298 653.091 +1.451 627.316 +1.604 601.548 +1.756 576.27 +1.909 542.033 +2.063 479.078 +2.216 394.184 +2.369 346.719 +2.521 307.435 +2.674 276.291 +2.827 216.608 +2.98 146.021 +3.133 106.838 +3.285 81.226 +3.439 52.105 +3.592 37.385 +3.745 29.462 +3.898 0 +; +; +K828FJ 54 579 6-10-14-18 1.45 2.255 AT +0.01 1112.06 +0.02 1238.6 +0.04 1303.79 +0.06 1135.06 +0.08 1077.54 +0.13 1031.53 +0.2 1016.19 +0.5 993.18 +0.65 1004.68 +1 985.51 +1.08 974.01 +1.19 974.01 +1.42 954.83 +1.51 935.66 +1.69 912.65 +1.75 885.81 +1.83 893.48 +1.89 843.63 +1.95 774.6 +2 667.23 +2.15 444.82 +2.2 364.29 +2.23 260.76 +2.27 184.06 +2.33 111.21 +2.39 49.85 +2.5 0 +; +;AeroTech L1150 +;provided by ThrustCurve.org (www.thrustcurve.org) +L1150 75 531 0 2.06528 3.6736 AT +0.053 935.855 +0.175 1292.64 +0.3 1260.93 +0.425 1241.48 +0.55 1257.06 +0.675 1272.29 +0.8 1287.61 +0.925 1301.01 +1.048 1309.71 +1.17 1308.42 +1.295 1304.83 +1.42 1285.27 +1.545 1267.66 +1.67 1255.62 +1.795 1227.21 +1.92 1202.44 +2.043 1182.62 +2.165 1150.71 +2.29 1117.91 +2.415 1081.74 +2.54 1037.55 +2.665 1007.09 +2.79 1008.91 +2.915 643.124 +3.04 64.371 +3.165 0 +; +;AeroTech L850W +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +L850W 75 531 0 2.06528 3.67315 AT +0.091 1015.93 +0.274 1064.94 +0.458 1101.37 +0.643 1143.36 +0.827 1170.93 +1.011 1184.8 +1.196 1178.04 +1.38 1177.6 +1.564 1174.91 +1.748 1170.02 +1.932 1113.72 +2.117 1042.59 +2.301 972.795 +2.485 908.071 +2.67 844.471 +2.854 773.595 +3.039 714.046 +3.222 649.095 +3.406 597.341 +3.591 557.444 +3.775 422.233 +3.959 200.739 +4.144 79.411 +4.328 43.959 +4.513 14.862 +4.697 0 +; +;AeroTech L952W +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +L952W 98 427 0 2.73011 5.01222 AT +0.141 679.073 +0.425 801.562 +0.709 848.474 +0.994 913.345 +1.278 981.614 +1.562 1043.69 +1.847 1088.11 +2.131 1112.56 +2.416 1121.54 +2.7 1118.57 +2.984 1100.66 +3.269 1039.14 +3.553 965.784 +3.837 876.793 +4.122 780.693 +4.406 693.903 +4.691 608.03 +4.975 528.335 +5.259 463.528 +5.544 405.769 +5.828 358.367 +6.112 279.009 +6.397 99.897 +6.681 20.108 +6.967 3.317 +7.252 0 +; +;AeroTech L1120W +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +L1120W 75 665 0 2.75699 4.65786 AT +0.097 1377.21 +0.293 1442.67 +0.489 1496.99 +0.685 1537.06 +0.882 1554.96 +1.078 1554.13 +1.275 1547.97 +1.472 1533.46 +1.668 1510.34 +1.865 1472.28 +2.061 1362.53 +2.257 1245.42 +2.454 1148.86 +2.651 1062.68 +2.847 984.952 +3.044 916.169 +3.241 831.929 +3.436 766.45 +3.633 698.978 +3.83 562.966 +4.026 384.579 +4.223 227.654 +4.42 105.078 +4.616 56.339 +4.813 21.712 +5.009 0 +; +; +L1300R 98 443 1000 2.508 4.884 AT +0.0231839 1299.23 +0.502318 1332.26 +0.996909 1497.42 +1.49923 1552.47 +1.99382 1508.43 +2.49614 1354.29 +2.99845 1101.05 +3.12983 1090.03 +3.21484 1145.09 +3.3694 176.167 +3.5 0 +; +; +L1420R 75 443 1000 2.56 4.562 AT +0.0386399 1332.26 +0.123648 1563.48 +0.502318 1519.44 +0.996909 1574.49 +1.49923 1662.58 +2.00155 1574.49 +2.48068 1409.34 +2.92117 1299.23 +2.99073 1167.11 +3.11437 187.178 +3.24 0 +; +;AeroTech L1500T +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +L1500T 98 443 0 2.464 4.6592 AT +0.073 1320.33 +0.222 1454.82 +0.372 1508.99 +0.522 1556.78 +0.672 1602.41 +0.822 1642 +0.971 1670.1 +1.12 1694.8 +1.27 1701.3 +1.42 1704.29 +1.57 1701.01 +1.72 1694.55 +1.869 1683.86 +2.018 1659.69 +2.168 1620.16 +2.318 1570.03 +2.468 1517.93 +2.618 1463.32 +2.767 1400.99 +2.916 1331.42 +3.066 1279.48 +3.216 1108.99 +3.366 217.788 +3.516 10.579 +3.666 3.245 +3.816 0 +; +;75-6400 case +;Greg Gardner - 10/25/07 +M650W 75 801 1000 3.351 5.125 AT +0.08 1240 +0.12 1328 +0.25 1230 +0.5 1142 +1 1071 +1.5 1048 +2 1018 +2.5 982 +3 950 +3.5 853 +4 781 +5 595 +6 443 +7 297 +8 155 +9 88 +10 32 +10.5 12 +11 4 +11.5 0 +; +;98-10240 case +;Greg Gardner - 10/25/07 +M750W 98 732 1000 5.3 8.776 AT +0.1 1032 +0.2 992 +0.3 974 +0.48 966 +1 1055 +1.5 1152 +2 1192 +2.5 1218 +4 1103 +6 818 +8 561 +10 318 +11 216 +12 125 +13 76 +14 47 +15 23 +15.5 9 +16 0 +; +;Aerotech M1297W +;Greg Gardner - 12/20/04 +M1297W 75 665 0 2.722 4.637 AT +0.1 1433.4 +0.15 1789.3 +0.2 1922.8 +0.25 1869.4 +0.3 1856 +0.35 1833.8 +0.4 1767 +0.5 1722.6 +0.6 1709.2 +0.9 1700.3 +1 1688.1 +1.5 1678.7 +1.75 1634.6 +1.85 1622.3 +1.95 1572.8 +2 1554 +2.5 1346.5 +3 1136 +3.2 1053.3 +3.25 1044.1 +3.35 1032 +3.38 1020 +3.4 937 +3.5 738 +3.6 545 +3.75 393 +4 226 +4.25 94 +4.35 45 +4.4 0 +; +;AeroTech M1315W +;Copyright Tripoli Motor Testing 1999 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +M1315W 75 801 0 3.4496 5.6448 AT +0.116 1728.68 +0.349 1673.34 +0.582 1686.81 +0.816 1696.07 +1.049 1663.17 +1.282 1631.24 +1.516 1620.47 +1.749 1619.7 +1.982 1621.04 +2.216 1615.32 +2.449 1567.09 +2.682 1493.72 +2.916 1420.08 +3.149 1358.66 +3.382 1292.51 +3.616 1224.81 +3.849 1171.99 +4.082 928.809 +4.316 577.949 +4.549 395.445 +4.782 314.006 +5.016 228.273 +5.249 159.803 +5.482 118.348 +5.716 109.782 +5.949 0 +; +;AeroTech M1419W +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +M1419W 98 579 0 4.032 6.91622 AT +0.154 1154.9 +0.465 1241.15 +0.776 1300.22 +1.087 1358.36 +1.399 1411.03 +1.71 1461.03 +2.022 1485.75 +2.333 1503.65 +2.644 1513.11 +2.955 1511.95 +3.267 1492.44 +3.578 1418.37 +3.89 1326.61 +4.201 1219.22 +4.513 1087.65 +4.824 937.068 +5.135 810.066 +5.446 709.13 +5.757 624.701 +6.069 557.223 +6.38 437.806 +6.692 252.076 +7.003 107.741 +7.315 19.973 +7.626 0.515 +7.937 0 +; +;AeroTech M1550R +;provided by ThrustCurve.org (www.thrustcurve.org) +M1550R 75 800 0 3.4496 5.6448 AT +0.069 1720.76 +0.212 2125.33 +0.358 1995.95 +0.501 1908.44 +0.645 1868.71 +0.79 1835.5 +0.935 1808.66 +1.079 1796.3 +1.222 1785.42 +1.368 1773.15 +1.511 1746.59 +1.655 1715.71 +1.8 1689.63 +1.945 1660.72 +2.089 1633.28 +2.232 1606.04 +2.378 1570.22 +2.521 1534.71 +2.665 1503.35 +2.81 1461.32 +2.955 1427.57 +3.099 1393.23 +3.242 939.955 +3.388 268.504 +3.532 4.985 +3.677 0 +; +;AeroTech M1600R +;provided by ThrustCurve.org (www.thrustcurve.org) +M1600R 98 579 0 4.032 6.91712 AT +0.088 1370.36 +0.268 1626.63 +0.448 1672.65 +0.628 1720.6 +0.808 1763.29 +0.987 1801.28 +1.167 1829.83 +1.348 1845.15 +1.529 1856.37 +1.71 1850.09 +1.89 1847.37 +2.07 1829.45 +2.25 1810.98 +2.43 1784.91 +2.61 1754.27 +2.79 1726.9 +2.971 1689.29 +3.152 1641.58 +3.332 1581.59 +3.513 1511.04 +3.692 1431.4 +3.872 1361.03 +4.053 1234.57 +4.232 621.206 +4.414 42.471 +4.595 0 +; +;75-7680 case +;Greg Gardner - 10/25/07 +M1850W 75 935 0 3.979 6.871 AT +0.1 2411 +0.2 2135 +0.3 2015 +0.4 2000 +0.5 2055 +1 2098 +1.5 1860 +2 1788 +2.5 1659 +3 1468 +3.25 1423 +3.35 1334 +3.5 1201 +3.75 934 +3.8 930 +4 881 +4.25 600 +4.5 468 +4.75 400 +5 290 +5.5 85 +6 23 +6.5 0 +; +;AeroTech M1939W +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +M1939W 98 732 0 5.656 8.98822 AT +0.134 1905.18 +0.406 2021.15 +0.679 2095.9 +0.952 2158.09 +1.225 2198.21 +1.498 2219.69 +1.77 2228.64 +2.042 2229.88 +2.315 2225.64 +2.587 2211.71 +2.86 2164.72 +3.133 2047.01 +3.405 1916.24 +3.677 1805.66 +3.95 1658.49 +4.223 1497.7 +4.496 1339.45 +4.769 1213.06 +5.041 1102.13 +5.313 966.508 +5.585 670.253 +5.858 443.975 +6.131 155.355 +6.404 41.358 +6.677 5.775 +6.95 0 +; +;AeroTech M2000R +;provided by ThrustCurve.org (www.thrustcurve.org) +M2000R 98 732 0 5.65824 8.98688 AT +0.091 1530.96 +0.279 2186.27 +0.466 2166.7 +0.655 2187.24 +0.844 2219.07 +1.031 2248.07 +1.22 2273.74 +1.409 2298.31 +1.596 2309.75 +1.785 2315.71 +1.974 2316.16 +2.161 2306.31 +2.35 2282.23 +2.539 2252.1 +2.726 2209.64 +2.915 2168.8 +3.104 2117.18 +3.291 2067.53 +3.48 2004.51 +3.669 1934.44 +3.856 1831.48 +4.045 1745.63 +4.234 1504.27 +4.421 649.796 +4.61 58.178 +4.799 0 +; +;Took this data from the Aerotech Typical Time-Thrust Curve that comes with the M2030G motor. +M2030G 75 653 1000 2.663 4.906 AT +0.00776398 1342.14 +0.0776398 2147.42 +0.15528 1840.64 +0.496894 2224.11 +0.784161 2607.58 +1.00155 2645.93 +1.3587 2530.88 +1.49068 2415.84 +1.99534 1802.3 +2.3913 1418.83 +2.5 805.282 +2.56211 191.734 +2.675 0 +; +;AeroTech M2400T +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +M2400T 98 597 0 3.65254 6.4512 AT +0.07 2441.95 +0.211 2495.46 +0.353 2556.13 +0.495 2601.6 +0.636 2637.66 +0.778 2660.8 +0.92 2676.49 +1.061 2687.08 +1.203 2695.81 +1.345 2694.49 +1.486 2684.27 +1.628 2667.29 +1.771 2629.96 +1.914 2578.92 +2.055 2522.07 +2.197 2461.7 +2.339 2393.52 +2.48 2303.94 +2.622 2201.61 +2.764 2097.46 +2.905 2010.41 +3.047 1275.78 +3.189 418.836 +3.33 17.586 +3.473 3.669 +3.616 0 +; +;AeroTech M2500T +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +M2500T 98 751 0 4.6592 8.064 AT +0.082 2651.86 +0.249 2780.28 +0.416 2820.73 +0.583 2843.01 +0.751 2847.76 +0.918 2851.22 +1.084 2854.74 +1.252 2861.69 +1.42 2858.09 +1.586 2851.09 +1.754 2844.62 +1.922 2830.86 +2.089 2804.71 +2.255 2765.8 +2.423 2710.51 +2.591 2648.26 +2.757 2586.91 +2.925 2520.79 +3.093 2462.22 +3.259 2419.94 +3.426 1894.94 +3.594 808.043 +3.761 282.403 +3.928 97.876 +4.096 24.492 +4.264 0 +; +; +M845HW 98 795.02 1000 3.569 6.833 AT +0.015456 1332.26 +0.0463679 1706.62 +0.0772798 1178.12 +0.185471 1310.24 +0.973725 1222.16 +1.51468 1200.14 +1.97836 1123.07 +3.97218 1057 +4.20402 880.836 +6.01236 627.596 +6.495 418.397 +7.017 99.0941 +7.5 0 +; +;AeroTech N2000W +;Copyright Tripoli Motor Testing 1997 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +N2000W 98 1046 0 7.66707 12.2828 AT +0.146 2775.07 +0.446 2831.81 +0.746 2834.35 +1.046 2829.56 +1.346 2777.65 +1.646 2688.25 +1.95 2597.97 +2.254 2501.04 +2.554 2415.75 +2.854 2343.62 +3.154 2262.58 +3.454 2178.18 +3.758 2104.16 +4.062 2024.47 +4.362 1935.62 +4.663 1839.78 +4.962 1756.91 +5.262 1351.81 +5.567 954.556 +5.871 681.831 +6.171 475.91 +6.471 361.124 +6.771 194.633 +7.071 44.938 +7.375 6.03 +7.679 0 +; +;AeroTech N4800T +;provided by ThrustCurve.org (www.thrustcurve.org) +N4800T 98 1194 0 9.7664 14.784 AT +0.098 4752.72 +0.301 6007.53 +0.506 5594.23 +0.71 5270.36 +0.914 5150.12 +1.119 5108.05 +1.324 5086.21 +1.528 5031.65 +1.731 4941.81 +1.936 4800.4 +2.14 4664.88 +2.344 4527.84 +2.549 4401 +2.754 4263.56 +2.958 4120.41 +3.161 3971.14 +3.366 3876.42 +3.57 3916.23 +3.774 3913.51 +3.979 3312.76 +4.184 1649.27 +4.388 523.361 +4.591 327.209 +4.796 251.041 +5.001 128.177 +5.206 0 +; +;Apogee A2 RASP.ENG file made from NAR published data +;File produced September 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. +A2 11 58 0-3-5-7 0.00300006 0.00670001 AP +0.014 0.241 +0.036 0.895 +0.064 2.618 +0.1 4.82 +0.111 4.133 +0.125 2.687 +0.139 2.307 +0.185 2.031 +0.296 1.928 +0.481 1.825 +0.517 1.722 +0.538 1.791 +0.649 1.688 +0.748 1.757 +0.869 1.825 +1.04 1.894 +1.101 1.894 +1.119 1.825 +1.144 1.928 +1.229 1.859 +1.265 1.894 +1.283 1.757 +1.29 1.412 +1.293 0.688 +1.3 0.275 +1.31 0 +; +;Apogee B2 RASP.ENG file made from NAR published data +;File produced September 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. +B2 11 88 0-3-5-7-9 0.006 0.0106 AP +0.057 1.637 +0.093 4.091 +0.121 5.48 +0.143 4.787 +0.157 3.478 +0.207 2.578 +0.328 2.087 +0.371 2.087 +0.406 1.882 +0.641 1.841 +0.869 1.841 +1.283 1.882 +1.361 1.882 +1.397 1.718 +1.439 1.841 +1.532 1.718 +1.71 1.841 +1.888 1.882 +2.095 1.8 +2.23 1.8 +2.295 1.677 +2.423 1.759 +2.444 1.637 +2.466 0.982 +2.494 0.327 +2.53 0 +; +;Apogee B7 RASP.ENG file made from NAR published data +;File produced September 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. +B7 13 50 4-6-8-10 0.0028 0.0091 AP +0.007 5.708 +0.013 7.211 +0.032 6.111 +0.045 8.116 +0.056 7.717 +0.069 9.02 +0.078 12.122 +0.087 14.76 +0.106 13.832 +0.117 13.733 +0.125 12.636 +0.155 12.438 +0.168 11.836 +0.2 11.243 +0.209 11.737 +0.219 10.739 +0.266 9.846 +0.29 9.849 +0.299 8.949 +0.367 7.456 +0.393 7.159 +0.429 5.761 +0.487 4.567 +0.571 2.975 +0.607 2.178 +0.669 1.084 +0.708 0.489 +0.74 0 +; +;Apogee C4 RASP.ENG file made from NAR published data +;File produced September 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. +C4 18 50 3-5-7 0.0045 0.017 AP +0.018 3.23 +0.041 6.874 +0.147 8.779 +0.294 10.683 +0.365 11.31 +0.388 10.521 +0.412 8.779 +0.441 7.04 +0.465 4.555 +0.529 3.479 +0.629 2.981 +0.653 3.23 +0.718 2.816 +0.853 2.733 +1.065 2.65 +1.253 2.567 +1.453 2.401 +1.694 2.484 +1.794 2.484 +1.812 2.733 +1.841 2.401 +1.947 2.401 +2.112 2.401 +2.235 2.401 +2.282 2.236 +2.312 1.656 +2.329 0.662 +2.35 0 +; +;Apogee C6 RASP.ENG file made from NAR published data +;File produced September 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. +C6 13 83 4-7-10 0.007 0.0151 AP +0.008 13.958 +0.016 21.1 +0.022 15.511 +0.03 12.831 +0.052 14.8 +0.081 15.927 +0.092 14.658 +0.114 16.069 +0.125 14.658 +0.136 15.369 +0.168 14.8 +0.214 13.816 +0.225 12.973 +0.247 13.958 +0.252 12.831 +0.285 12.547 +0.307 12.405 +0.317 12.831 +0.328 11.562 +0.347 11.988 +0.393 11.42 +0.442 10.719 +0.464 11.136 +0.488 9.164 +0.545 8.459 +0.624 7.754 +0.716 6.485 +0.838 5.075 +0.977 3.102 +1.096 1.833 +1.207 0.986 +1.32 0 +; +;Apogee C10 RASP.ENG file made from NAR published data +;File produced September 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. +C10 18 50 4-7-10 0.0049 0.0176 AP +0.01 2.712 +0.019 5.842 +0.029 17.116 +0.037 25.72 +0.051 22.535 +0.07 20.446 +0.106 18.983 +0.164 17.085 +0.188 17.085 +0.2 15.824 +0.216 16.036 +0.255 15.602 +0.293 14.35 +0.343 13.503 +0.394 12.655 +0.41 11.605 +0.434 11.605 +0.521 9.287 +0.631 6.34 +0.741 4.021 +0.851 2.119 +0.911 1.48 +0.945 1.264 +0.96 0 +; +;Apogee D3 RASP.ENG file made from NAR published data +;File produced September 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. +D3 18 77 3-5-7 0.0098 0.0249 AP +0.05 6.79 +0.168 8.788 +0.318 10.46 +0.385 10.07 +0.402 7.909 +0.469 5.432 +0.486 3.914 +0.687 3.115 +1.122 2.876 +2.06 2.636 +3.349 2.397 +4.639 2.156 +5.727 1.997 +6.163 1.837 +6.263 3.994 +6.347 2.317 +6.364 0.719 +6.39 0 +; +;Apogee D10 RASP.ENG file made from NAR published data +;File produced September 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. +D10 18 70 3-5-7 0.0098 0.0259 AP +0.011 14.506 +0.018 25.13 +0.032 20.938 +0.079 19.065 +0.122 21.139 +0.136 19.686 +0.169 21.139 +0.201 20.728 +0.223 21.76 +0.233 20.938 +0.255 21.97 +0.276 20.938 +0.352 20.728 +0.402 20.107 +0.42 20.728 +0.459 20.107 +0.488 20.517 +0.556 18.243 +0.671 15.959 +0.707 14.717 +0.729 15.127 +0.779 12.853 +0.793 13.474 +0.836 11.401 +0.904 10.158 +0.926 10.569 +0.99 8.083 +1.026 8.498 +1.123 6.011 +1.231 2.487 +1.342 0.829 +1.4 0 +; +;Aerotech E6 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. +E6 24 70 2-4-6-8-100 0.0215 0.0463 AT +0.056 18.59 +0.112 20.12 +0.168 17.575 +0.307 14.38 +0.531 10.45 +0.894 7.696 +1.146 6.244 +1.691 5.808 +2.836 5.663 +3.898 5.517 +4.275 5.227 +4.415 4.937 +5.058 5.082 +5.519 5.227 +5.603 6.679 +5.729 3.921 +5.882 2.323 +5.966 1.016 +6.06 0 +; +; +G100 38 406 0 0.093 0.511 Contrail +0 182.756 +0.199105 177.584 +0.606264 132.757 +0.986577 53.4476 +1.43 0 +; +; +G123 38 406 0 0.0830001 0.511 Contrail +0.00223714 217.239 +0.00671141 399.995 +0.0201342 220.687 +0.914989 72.4129 +0.955257 37.9306 +1.15 0 +; +; +G130 38 406 1000 0.093 0.516 Contrail +0 662.061 +0.0145414 448.27 +0.0234899 241.376 +0.642058 41.3788 +0.86 0 +; +;G-234-HP Reload +;38mm/16 Inch Hardware +;Fast Nozzle +G234 38 406.4 0 0.498 0.544 Contrail +0.00169492 245.419 +0.0973154 540.63 +0.183445 526.943 +0.202461 191.616 +0.237136 143.712 +0.260626 136.868 +0.533 0 +; +;G-300 PVC Motor for 38mm/16 Inch Case. +;Motor uses Fast Nozzle +;90cc's of Nitrous Oxide Used +G300 38 406.4 0 0.0229999 0.544 Contrail +0.00111857 602.221 +0.0497763 814.367 +0.100671 670.655 +0.114094 266.893 +0.158837 239.52 +0.25 0 +; +; +H121 38 516 1000 0.11 0.612 Contrail +0.00223714 251.721 +0.0402685 265.514 +0.0738255 203.446 +0.400447 179.308 +0.60179 134.481 +1.08949 127.585 +1.40268 93.1023 +1.61969 37.9306 +1.85 0 +; +; +H141 38 516 0 0.125 0.612 Contrail +0.00223714 265.514 +0.111857 262.066 +1.20134 106.895 +1.25951 55.1717 +1.3557 27.5859 +1.7 0 +; +; +H211 38 516 0 0.125 0.612 Contrail +0.00111857 531.028 +0.0190157 634.475 +0.0223714 593.096 +0.033557 544.821 +0.296421 317.238 +0.313199 186.205 +0.743848 96.5506 +0.97 0 +; +;H-222-HP Reload +;38mm/16 inch Case Used +;Medium Nozzle Used For Reload +;140cc of Nitrous Oxide Used +H222 38 406.4 1000 0.0220001 0.52 Contrail +0 684.342 +0.0302013 656.968 +0.0525727 574.847 +0.0581655 349.014 +0.346756 260.05 +0.364653 191.616 +0.7 0 +; +;H-246 HP Reload +;38mm/20 Inch Case Used +;Medium Nozzle Used +;185cc Nitrous Oxide Used +H246 38 508 0 0.0220001 0.598 Contrail +0.00111857 609.064 +0.0123043 499.57 +0.502237 253.206 +0.514541 157.399 +0.9 0 +; +;H-248-PVC Reload +;38mm/28 Inch Hardware +;Fast Nozzle +H248 38 711.2 0 0.0350001 0.794 Contrail +0.00223714 465.352 +0.082774 698.029 +0.111857 342.171 +0.536913 266.893 +0.639821 191.616 +0.700224 184.772 +0.738255 164.242 +1.1 0 +; +; +H277 38 719 1000 0.11 0.71 Contrail +0 765.508 +0.0738255 703.44 +0.118568 337.927 +0.917226 179.308 +0.957494 75.8612 +0.995526 41.3788 +1.02908 48.2753 +1.15 0 +; +; +H300 38 516.001 0 0.11 0.612 Contrail +0 558.614 +0.115213 717.233 +0.12528 268.962 +0.214765 248.273 +0.286353 241.376 +0.334452 227.583 +0.62 0 +; +;H-303-PVC Hybrid Motor +;Uses Fast Nozzle +;38mm/20 Inch Hardware +;Uses 185cc Nitrous Oxide +H303 38 508 0 0.0229999 0.589 Contrail +0 663.812 +0.0447427 780.15 +0.108501 704.872 +0.111857 342.171 +0.176734 328.484 +0.196868 307.954 +0.6 0 +; +; +H340 38 711.2 1000 0.024 0.816 Contrail +0 920.322 +0.0847458 715.806 +0.101695 345.121 +0.683051 332.338 +0.740678 255.645 +0.766102 153.387 +0.95 0 +; +; +I155 38 711.2 0 0.045 0.725 Contrail +0.0111857 222.411 +2.71253 150.555 +2.82998 82.121 +2.96421 58.1691 +3.5 0 +; +; +I210 38 922 0 0.125 0.87 Contrail +0 468.96 +0.464206 386.202 +0.497763 206.894 +2.25391 110.343 +2.34899 41.3788 +2.40492 13.7929 +2.72 0 +; +; +I221 38 719 1000 0.125 0.71 Contrail +0 482.753 +0.503356 358.616 +0.519016 179.308 +1.49217 103.447 +1.53691 27.5859 +1.74 0 +; +;I-250-HP +;38mm/28 Inch Hardware +;430cc +;Medium Nozzle +I250 38 711.2 0 0.066 0.724 Contrail +0.00447427 622.751 +0.0246085 437.979 +1.00447 273.737 +1.02237 171.085 +1.20134 157.399 +1.23937 136.868 +1.7 0 +; +; +I290 38 914.4 0 0.0679998 0.884 Contrail +0 521.516 +0.0847458 337.451 +0.138983 357.903 +0.19661 398.806 +0.308475 490.838 +0.40339 449.935 +0.589831 357.903 +0.762712 419.258 +0.932203 265.871 +1.08814 163.613 +1.24068 81.8064 +1.5 0 +; +; +I307 38 922 1000 0.11 0.81 Contrail +0.00223714 551.717 +0.199105 717.233 +0.210291 386.202 +0.756152 620.682 +0.834452 455.167 +0.941834 310.341 +1.09172 199.998 +1.22371 117.24 +1.85 0 +; +;I-333-PVC Reload +;38mm/36 Inch Hardware +;Uses Fast Nozzle +;460cc Nitrous Oxide +I333 38 914.4 0 0.0679998 0.929 Contrail +0.00894855 855.427 +0.0290828 881.09 +0.0536913 504.702 +0.604027 342.171 +0.796421 461.931 +1.7 0 +; +;I-400-HP +;38mm/36 Inch Hardware +;Uses Fast/X-Fast Nozzle +;460cc Nitrous Oxide +I400 38 914.4 0 0.0860002 0.925 Contrail +0.00447427 667.233 +0.0782998 898.199 +0.116331 598.799 +0.297539 521.811 +0.420582 410.605 +0.559284 487.594 +0.738255 367.834 +1 0 +; +; +I500 38 719 1000 0.748 0.8 Contrail +0.00111857 1155.16 +0.0201342 706.888 +0.0313199 999.988 +0.574944 103.447 +0.623043 120.688 +0.7 0 +; +; +I727 38 914.4 0 0.0220001 0.929 Contrail +0.00847458 1278.22 +0.0355932 1661.69 +0.0983051 1508.31 +0.144068 1482.74 +0.171186 1175.97 +0.218644 1022.58 +0.422034 792.499 +0.75 0 +; +; +I747 38 711.2 0 0.0679998 0.839 Contrail +0 1917.34 +0.45 0 +; +;J-150-HP +;38mm/36 Inch +;550cc +;Slow Nozzle +J150 38 914.4 1000 0.0910002 0.839 Contrail +0 266.893 +2.00224 184.772 +2.75727 150.555 +3.00895 92.3861 +4.1 0 +; +;J-222-HP Reload +;Medium Nozzle +;38mm/48 Inch Hardware +;830cc +J222 38 1219.2 0 0.0910002 1.043 Contrail +0.00559284 547.473 +0.167785 355.858 +2.86353 191.616 +2.95861 143.712 +3.08725 130.025 +3.46756 95.8079 +4.3 0 +; +;J-234-BG Reload +;Slow Nozzle +;54mm/36 Inch Hardware +J234 54 914.4 0 0.177 1.764 Contrail +0.00559284 229.255 +0.503356 349.014 +3.47875 208.724 +3.62416 116.338 +3.75839 78.6993 +4.3 0 +; +; +J242 38 1227 0 0.11 1.065 Contrail +0.0111857 448.27 +1.73937 268.962 +1.76174 165.515 +2.97539 48.2753 +3.1 0 +; +;J-245-BG Reload +;Slow Nozzle +;54mm/28 Inch Hardware +J245 54 711.2 0 0.1 1.55 Contrail +0 444.822 +0.139821 355.858 +1.05145 307.954 +2.06376 184.772 +2.15884 102.651 +2.28188 68.4342 +2.62 0 +; +;J-246-HP Reload +;38mm/36 Inch Hardware +;550cc +;Medium Nozzle +J246 38 914.4 0 0.0679998 0.861 Contrail +0.0167785 492.726 +0.0279642 328.484 +0.134228 526.943 +0.341163 403.762 +0.520134 349.014 +2.00224 191.616 +2.12528 116.338 +2.8 0 +; +; +J272 54 914.4 0 0.114 1.746 Contrail +0.00847458 398.806 +0.169492 572.645 +0.533898 460.161 +0.872881 388.58 +1.05932 357.903 +2.91525 204.516 +3.19492 71.5806 +3.51695 40.9032 +3.63559 51.129 +3.86 0 +; +; +J292 54 711.2 0 0.136 1.542 Contrail +0.00847458 552.193 +0.262712 480.612 +0.423729 419.258 +0.762712 337.451 +1.97458 245.419 +2.07627 143.161 +2.53 0 +; +; +J333 38 1227 0 0.11 1.064 Contrail +0 717.233 +0.204139 799.99 +0.752237 448.27 +0.763423 268.962 +2.16443 62.0682 +2.23714 27.5859 +2.4 0 +; +;J-345-PVC +;38mm/48 Inch Hardware +;735cc +;Fast Nozzle +J345 38 1219.2 0 0.098 1.118 Contrail +0.00559284 881.09 +0.0782998 667.233 +1.21924 376.388 +1.26398 359.279 +2.7 0 +; +; +J355 54 711.2 0 0.09 1.564 Contrail +0 562.419 +0.176271 501.064 +0.2 286.322 +0.433898 286.322 +0.688136 337.451 +0.701695 501.064 +0.80678 490.838 +1.00339 521.516 +1.21695 419.258 +1.31186 429.484 +1.37627 460.161 +1.49831 429.484 +1.54576 224.968 +1.64068 122.71 +1.91 0 +; +; +J358 54 914.4 0 0.111 1.743 Contrail +0.00847458 726.032 +0.0932203 726.032 +0.110169 501.064 +0.483051 480.612 +0.550847 398.806 +2.23729 286.322 +2.32203 153.387 +2.44915 112.484 +2.69 0 +; +; +J416 54 914.4 0 0.158 1.7 Contrail +0 787.386 +0.0762712 777.161 +0.211864 572.645 +0.432203 531.741 +0.864407 511.29 +1.26271 480.612 +1.82203 470.387 +2.00847 347.677 +2.13559 276.097 +2.24576 184.064 +2.40678 81.8064 +2.75 0 +; +; +J555 38 1227 0 0.166 1.132 Contrail +0 931.023 +0.0581655 1344.81 +0.277405 810.335 +1.17226 241.376 +1.2774 68.9647 +1.31767 51.7235 +1.6 0 +; +; +J642 54 914.4 0 0.159 1.791 Contrail +0.00677966 1482.74 +0.0779661 997.015 +0.471186 1303.79 +0.542373 818.064 +0.633898 741.37 +0.742373 587.983 +1.25085 485.725 +1.29831 332.338 +1.39661 178.951 +1.47458 51.129 +1.72 0 +; +;J-800-HP +;38mm/48 Inch +;685cc +;XXF Nozzle (Short Nozzle) +J800 38 1219.2 0 0.105 1.148 Contrail +0.00223714 1830.61 +0.52349 889.644 +0.639821 650.125 +0.740492 444.822 +0.823266 273.737 +0.90604 153.977 +0.997763 136.868 +1.2 0 +; +;K-234-BG Reload +;Slow Nozzle +;54mm/48 Inch Hardware +K234 54 1219.2 0 0.385 2.063 Contrail +0 92.3861 +0.234899 396.918 +0.973154 338.749 +5.97315 171.085 +6.05145 106.073 +6.19687 78.6993 +6.37584 54.7473 +7.05 0 +; +; +K265 54 1219.2 0 0.271 2.085 Contrail +0 470.387 +2.44068 347.677 +3.91525 224.968 +4.77966 173.839 +5.13559 112.484 +5.33898 51.129 +6.26 0 +; +;K-300-BS +;75mm/40 Inch Hardware +;2050cc +;Slow Nozzle +K300 75 1016 0 0.181 4.059 Contrail +0 431.135 +0.324385 526.943 +0.98434 479.039 +1.1745 369.545 +5 280.58 +5.19016 171.085 +5.35794 102.651 +5.6264 54.7473 +5.79418 27.3737 +6.5 0 +; +;K-321-BG Reload +;54mm/48 Inch Hardware +;Medium Nozzle +K321 54 1219.2 0 0.183 2.043 Contrail +0.00559284 218.989 +0.218121 410.605 +0.973154 718.559 +0.989933 732.246 +1.05705 444.822 +1.4877 403.762 +3.97092 232.676 +4.11633 88.9644 +4.23378 54.7473 +4.34564 54.7473 +4.9 0 +; +;K-404-Sparky +;75mm/40 Inch Hardware +;2050cc +;Slow Nozzle +K404 75 1016 0 0.318 4.15 Contrail +0.0111857 670.655 +4.63087 335.328 +4.80984 205.303 +4.9217 130.025 +5.0783 82.121 +5.26846 41.0605 +6.4 0 +; +; +K456 75 813.001 0 0.58 3.704 Contrail +0.00559284 681.026 +0.212528 896.541 +0.503356 775.853 +1.36465 577.579 +1.52685 525.856 +2.51119 370.685 +2.66779 129.309 +3.7 0 +; +;Contrail Rockets Hybrid Rocket Motor (K543) +;75mm-1400cc Motor Hardware w/ Slow Injector Kit and Nozzle +;Black Smoke Reload +;Data Input By Tom R. Sanders of Contrail Rockets LLC +K543 75 787.4 0 1.5 3.6 Contrail +0 900 +2.98992 472.868 +3.1243 108.527 +3.6 0 +; +;K-555-BG Reload +;54mm/48 Inch Case +;XF Nozzle +K555 54 1219.2 0 0.156 2.038 Contrail +0.0503356 769.885 +0.33557 889.644 +0.559284 1385.79 +0.844519 872.536 +1.0123 581.691 +2.48881 342.171 +2.56711 222.411 +2.63982 136.868 +2.74049 51.3256 +2.8132 17.1085 +3.04 0 +; +;K-630-Sparky Reload +;75mm/41 Inch Hardare +;1400cc +;Medium Nozzle +K630 75 1041.4 0 0.075 3.55 Contrail +0.00559284 307.954 +0.0978747 573.136 +0.500559 889.644 +1.75336 667.233 +1.85403 410.605 +1.93792 239.52 +2.04978 128.314 +2.2 0 +; +;K-678-Sparky +;75mm/40 Inch Hardware +;2050cc +;Medium Nozzle +K678 75 1016 0 0.827 4.05 Contrail +0.00559284 1163.38 +2.21477 444.822 +2.32103 256.628 +2.38814 102.651 +2.8 0 +; +;K-707-BG Reload +;Medium Nozzle +;1400cc +K707 75 1041.4 0 0.136 3.674 Contrail +0.0111857 684.342 +0.195749 1351.58 +0.288031 1180.49 +0.369128 1129.16 +1.50168 496.148 +1.566 307.954 +1.63591 171.085 +1.68345 119.76 +2 0 +; +; +K777 75 1016 0 0.645 4.05 Contrail +0 931.023 +0.0950783 965.506 +0.111857 1793.08 +0.167785 1741.36 +0.206935 1344.81 +0.727069 1137.92 +1.00112 810.335 +1.97427 413.788 +2.04698 172.412 +2.6 0 +; +;Contrail Rockets Hybrid Rocket Motor (K888) +;75mm-2000cc Hardware with Medium Injector Kit and Nozzle +;Black Smoke Reload +;Data Input By Tom R. Sanders of Contrail Rockets LLC. +K888 75 990.6 0 2.1 4.1 Contrail +0 1365 +0.5 1365 +1.04143 1069.77 +2.4972 434.109 +2.54199 124.031 +2.7 0 +; +;L-369-Sparky +;Slow nozzle +;75mm/54 Inch Hardware +;3200cc +L369 75 1371.6 0 0.514 4.8 Contrail +0.0223714 540.63 +1.45414 533.787 +8.92617 260.05 +9.08277 130.025 +9.28412 68.4342 +10.6 0 +; +;L-800-Sparky +;75mm/54 Inch Hardware +;3200cc +;Medium Nozzle +L800 75 1371.6 0 0.988 4.726 Contrail +0.00559284 1351.58 +0.167785 1129.16 +0.329978 1266.03 +0.553691 1248.92 +0.665548 1129.16 +3.48434 821.21 +3.5962 496.148 +3.69687 273.737 +3.83669 153.977 +4.6 0 +; +;Contrail Rockets LLC Hybrid Rocket Motor (L1222) +;75mm-3200cc Motor System +;Sparky Hybrid Fuel +;Data Input By Tom R. Sanders of Contrail Rockets +L1222 75 1339.85 0 3.9 4.989 Contrail +0 455 +0.25 455 +0.5 2725 +0.75 1816 +2.75 680 +3.1 0 +; +;Contrail Rockets LLC. Hybrid Rocket Motor (L1428) +;75mm-3200cc Motor Using Fast Injector Kit and Nozzle +;Data Input By Tom R. Sanders of Contrail Rockets +L1428 75 1492.25 0 3.5 5.738 Contrail +0 1425 +0.403135 2751.94 +0.8 2725 +1.20941 1511.63 +2.65 800 +3 800 +3.1 0 +; +; +L2525 75 1492.25 0 3.5 5.579 Contrail +0 4200 +0.754759 3294.57 +1.9 0 +; +;Contrail Rockets LLC Hybrid Rocket Motor. (M-711) +;75-3200cc Hardware Set +;Black Smoke Fuel +M711 75 1340 0 4.2 4.9 Contrail +0 1140 +1.46697 1069.77 +4 680 +6.47256 589.147 +6.67413 279.07 +7.22 0 +; +;Contrail Rockets LLC. Hybrid Rocket Motor (M1491 +;75mm-3200cc Motor Using Medium Injector Kit and Nozzle +;Data Input By Tom R. Sanders of Contrail Rockets +M1491 75 1339.85 0 3.85 4.876 Contrail +0 2725 +0.481523 2635.66 +0.81187 2286.82 +1.33259 1860.47 +3 900 +3.09071 503.876 +3.35 0 +; +;M-1575-Black Gold Reload +;5300cc +;98mm/60 Inch Hardware +M1575 98 1524 0 0.726 10.863 Contrail +0.139821 2429.41 +0.503356 2976.89 +2.95302 1402.9 +3.06488 923.861 +3.21029 376.388 +3.31096 205.303 +4.2 0 +; +;Contrail Rockets LLC. Hybrid Rocket Motor (M2281) +;75mm-3200cc Motor Using Fast Injector Kit and Nozzle +;Data Input By Tom R. Sanders of Contrail Rockets +M2281 75 1492.25 0 3.95 5.579 Contrail +0 2725 +0.2 4550 +0.6 4550 +0.8 4550 +0.9 4000 +0.95 2725 +1.98768 116.279 +2.14 0 +; +; +M2700 98 1524 0 0.412 10.432 Contrail +0.00847458 2965.48 +0.0508475 3272.26 +0.105932 5930.96 +0.347458 5828.7 +0.504237 6442.25 +0.512712 5726.45 +0.601695 5112.9 +0.745763 3681.29 +0.902542 3067.74 +1.06356 2454.19 +1.18644 1942.9 +1.34322 1738.39 +1.75 715.806 +1.95763 102.258 +2.3 0 +; +;M-2800-Black Gold Reload +;5300cc +;98mm/60 inch Hardware +M2800 98 1524 0 0.476 10.704 Contrail +0.00838926 2395.2 +0.251678 2805.8 +0.545302 3695.45 +0.75783 5611.6 +0.911633 4311.35 +1.1745 3558.58 +1.4094 2258.33 +1.70861 1505.55 +2.3 0 +; +; +O6300 152 1828.8 0 3.175 28.576 Contrail +0.0338983 12271 +0.728814 9714.51 +1.65254 9203.22 +2.37288 8947.57 +2.51695 6646.77 +2.78814 4601.61 +2.99153 4857.25 +3.27966 3579.03 +3.61017 1278.22 +4.29 0 +; +;Apogee 1/4A2 RASP.ENG file made from NAR published data +;File produced September 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. +1/4A2 11 38 2-4 0.000800137 0.00360016 AP +0.007 0.162 +0.023 0.65 +0.041 1.463 +0.058 2.519 +0.074 3.738 +0.079 3.9 +0.088 4.915 +0.097 5.119 +0.106 5.4 +0.11 5.119 +0.118 3.981 +0.125 3.656 +0.132 3.453 +0.136 3.209 +0.151 3.169 +0.156 2.966 +0.168 2.884 +0.18 2.397 +0.194 1.625 +0.207 1.056 +0.218 0.406 +0.23 0 +; +;Estes 1/4A3T RASP.ENG file made from NAR published data +;File produced October 3, 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. +1/4A3T 13 45 3 0.000830074 0.00609991 ES +0.016 0.243 +0.044 1.164 +0.08 2.698 +0.088 2.851 +0.096 3.312 +0.105 3.804 +0.116 4.325 +0.129 4.754 +0.131 4.754 +0.135 4.95 +0.139 4.815 +0.143 4.814 +0.149 4.66 +0.157 4.289 +0.173 3.548 +0.187 2.808 +0.194 2.592 +0.197 2.13 +0.202 1.913 +0.206 1.512 +0.213 1.389 +0.218 1.112 +0.227 0.802 +0.236 0.493 +0.241 0.277 +0.25 0 +; +;Apogee 1/2A2 RASP.ENG file made from NAR published data +;File produced September 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. +1/2A2 11 57 2-4-6 0.0015 0.0044 AP +0.007 0.19 +0.045 1.494 +0.078 3.152 +0.088 3.805 +0.093 3.805 +0.1 3.97 +0.105 3.696 +0.11 3.071 +0.117 2.554 +0.123 2.582 +0.132 2.31 +0.163 2.146 +0.2 1.984 +0.242 1.902 +0.253 2.01 +0.275 1.929 +0.342 1.929 +0.403 1.929 +0.41 1.848 +0.42 1.902 +0.467 1.902 +0.528 1.929 +0.565 1.929 +0.58 1.902 +0.593 1.848 +0.603 1.657 +0.61 1.141 +0.615 0.597 +0.622 0.244 +0.63 0 +; +;Estes 1/2A3T RASP.ENG file made from NAR published data +;File produced October 3, 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. +1/2A3T 13 45 2-4 0.002 0.0066 ES +0.024 0.501 +0.042 1.454 +0.064 3.009 +0.076 4.062 +0.088 4.914 +0.093 5.065 +0.103 6.068 +0.112 6.87 +0.117 7.021 +0.126 7.62 +0.137 7.472 +0.146 6.87 +0.153 6.118 +0.159 5.065 +0.166 4.363 +0.179 3.66 +0.197 2.908 +0.222 2.256 +0.25 2.156 +0.277 2.106 +0.294 2.056 +0.304 2.156 +0.316 1.955 +0.326 1.554 +0.339 1.053 +0.35 0.651 +0.36 0 +; +;Estes 1/2A6 RASP.ENG file made from NAR published data +;File produced October 3, 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. +1/2A6 18 70 2 0.0026 0.0138 ES +0.031 0.404 +0.064 1.258 +0.096 2.263 +0.124 3.467 +0.149 4.72 +0.172 6.023 +0.196 7.027 +0.21 7.528 +0.225 7.86 +0.235 7.482 +0.244 6.683 +0.254 5.685 +0.263 4.487 +0.269 4.087 +0.279 3.039 +0.29 1.79 +0.297 1.042 +0.306 0.593 +0.314 0.344 +0.33 0 +; +;Estes A3T RASP.ENG file made from NAR published data +;File produced October 3, 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. +A3T 13 45 4 0.0033 0.0085 ES +0.024 0.195 +0.048 0.899 +0.086 2.658 +0.11 4.183 +0.14 5.83 +0.159 5.395 +0.18 4.301 +0.199 3.635 +0.215 2.736 +0.234 2.267 +0.258 2.15 +0.315 2.072 +0.441 1.993 +0.554 2.033 +0.605 2.072 +0.673 1.954 +0.764 1.954 +0.874 2.072 +0.931 2.15 +0.953 2.072 +0.966 1.719 +0.977 1.173 +0.993 0.547 +1.01 0 +; +;Estes A8 RASP.ENG file made from NAR published data +;File produced October 3, 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. +A8 18 70 3-5 0.0033 0.01635 ES +0.041 0.512 +0.084 2.115 +0.127 4.358 +0.166 6.794 +0.192 8.588 +0.206 9.294 +0.226 9.73 +0.236 8.845 +0.247 7.179 +0.261 5.063 +0.277 3.717 +0.306 3.205 +0.351 2.884 +0.405 2.499 +0.467 2.371 +0.532 2.307 +0.589 2.371 +0.632 2.371 +0.652 2.243 +0.668 1.794 +0.684 1.153 +0.703 0.448 +0.73 0 +; +;Estes A10T RASP.ENG file made from NAR published data +;File produced October 3, 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. +A10T 13 45 3-100 0.0038 0.00525 ES +0.026 0.478 +0.055 1.919 +0.093 4.513 +0.124 8.165 +0.146 10.956 +0.166 12.64 +0.179 11.046 +0.194 7.966 +0.203 6.042 +0.209 3.154 +0.225 1.421 +0.26 1.225 +0.333 1.41 +0.456 1.206 +0.575 1.195 +0.663 1.282 +0.76 1.273 +0.811 1.268 +0.828 0.689 +0.85 0 +; +;Estes B4 RASP.ENG file made from NAR published data +;File produced October 3, 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. +B4 18 70 2-4 0.006 0.0189 ES +0.02 0.418 +0.04 1.673 +0.065 4.076 +0.085 6.69 +0.105 9.304 +0.119 11.496 +0.136 12.75 +0.153 11.916 +0.173 10.666 +0.187 9.304 +0.198 7.214 +0.207 5.645 +0.226 4.809 +0.258 4.182 +0.326 3.763 +0.422 3.554 +0.549 3.345 +0.665 3.345 +0.776 3.345 +0.863 3.345 +0.94 3.449 +0.991 3.449 +1.002 2.404 +1.01 1.254 +1.03 0 +; +;Estes C5 RASP.ENG file made from NAR published data +;File produced October 3, 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. +C5 18 70 3 0.0113 0.0248 ES +0.042 2.195 +0.107 9.118 +0.159 16.213 +0.21 21.85 +0.233 18.407 +0.27 13.677 +0.289 9.793 +0.303 7.092 +0.326 5.065 +0.401 4.39 +0.55 3.883 +0.802 3.714 +1.026 3.883 +1.291 3.883 +1.524 4.221 +1.683 4.221 +1.702 2.195 +1.73 0 +; +;Estes C6 RASP.ENG file made from NAR published data +;File produced October 3, 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. +C6 18 70 0-3-5-7 0.0108 0.0231 ES +0.031 0.946 +0.092 4.826 +0.139 9.936 +0.192 14.09 +0.209 11.446 +0.231 7.381 +0.248 6.151 +0.292 5.489 +0.37 4.921 +0.475 4.448 +0.671 4.258 +0.702 4.542 +0.723 4.164 +0.85 4.448 +1.063 4.353 +1.211 4.353 +1.242 4.069 +1.303 4.258 +1.468 4.353 +1.656 4.448 +1.821 4.448 +1.834 2.933 +1.847 1.325 +1.86 0 +; +;ESTES C11 RASP.ENG file made from NAR published data +;File produced JANUARY 1, 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. +C11 24 70 0-3-5-7 0.012 0.0353 ES +0.034 1.692 +0.066 3.782 +0.107 7.566 +0.145 10.946 +0.183 14.832 +0.214 17.618 +0.226 18.213 +0.256 20.107 +0.281 21.208 +0.298 21.73 +0.306 20.206 +0.323 17.321 +0.337 14.931 +0.358 13.236 +0.385 11.947 +0.413 11.65 +0.468 10.946 +0.539 10.45 +0.619 10.648 +0.683 10.648 +0.715 10.648 +0.726 10.053 +0.74 8.163 +0.758 5.773 +0.778 3.185 +0.795 1.394 +0.81 0 +; +;Estes D11 RASP.ENG file made from NAR published data +;File produced October 3, 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. +D11 24 70 100 0.0245 0.0448 ES +0.033 2.393 +0.084 5.783 +0.144 12.17 +0.214 20.757 +0.261 24.35 +0.289 26.01 +0.311 23.334 +0.325 18.532 +0.338 14.536 +0.356 12.331 +0.398 10.72 +0.48 9.303 +0.618 8.676 +0.761 8.247 +0.955 8.209 +1.222 7.955 +1.402 8.319 +1.54 8.291 +1.701 8.459 +1.784 8.442 +1.803 6.239 +1.834 3.033 +1.86 0 +; +;Estes D12 RASP.ENG file made from NAR published data +;File produced October 3, 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. +D12 24 70 0-3-5-7 0.0211 0.0426 ES +0.049 2.569 +0.116 9.369 +0.184 17.275 +0.237 24.258 +0.282 29.73 +0.297 27.01 +0.311 22.589 +0.322 17.99 +0.348 14.126 +0.386 12.099 +0.442 10.808 +0.546 9.876 +0.718 9.306 +0.879 9.105 +1.066 8.901 +1.257 8.698 +1.436 8.31 +1.59 8.294 +1.612 4.613 +1.65 0 +; +;Estes B6-0 from NAR data by Mark Koelsch +B6-0 18 70 0 0.0056 0.0156 ES +0.036 1.364 +0.064 2.727 +0.082 4.215 +0.111 6.694 +0.135 9.05 +0.146 9.545 +0.172 11.901 +0.181 12.149 +0.191 11.901 +0.211 9.174 +0.239 7.314 +0.264 6.074 +0.275 5.95 +0.333 5.207 +0.394 4.835 +0.445 4.835 +0.556 4.339 +0.667 4.587 +0.723 4.339 +0.78 4.339 +0.793 4.091 +0.812 2.603 +0.833 1.24 +0.857 0 +; +;Estes E9-0 by Mark Koelsch from NAR data +E9-0 24 95 0 0.0358 0.0568 ES +0.046 1.913 +0.235 16.696 +0.273 18.435 +0.326 14.957 +0.38 12.174 +0.44 10.435 +0.835 9.043 +1.093 8.87 +1.496 8.696 +1.997 8.696 +2.498 8.696 +3.014 9.217 +3.037 5.043 +3.067 1.217 +3.09 0 +; 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+;Pro 150 O5800 White Thunder +O5800 150 754 0 13.95 26.368 CTI +0.069 6337.62 +0.103 5700.97 +0.218 5874.6 +0.378 6135.05 +0.561 6337.62 +0.745 6221.86 +0.985 6221.86 +1.18 6192.93 +1.455 6308.68 +1.753 6366.56 +1.994 6337.62 +2.269 6395.5 +2.509 6308.68 +2.83 6192.93 +3.14 6048.23 +3.426 5874.6 +3.69 5729.9 +3.965 5585.21 +4.263 5382.64 +4.572 5295.82 +4.939 5180.06 +5.053 5035.37 +5.11 4717.04 +5.133 4225.08 +5.145 3675.24 +5.156 3038.59 +5.179 2344.05 +5.214 1475.88 +5.259 607.717 +5.294 57.878 +5.295 0 +; +;Pro 150 O8000 White Thunder +O8000 150 957 0 18.61 32.672 CTI +0.045 3964.63 +0.046 6742.77 +0.047 8623.79 +0.125 7929.26 +0.239 8160.77 +0.364 8392.28 +0.489 8508.04 +0.614 8536.98 +0.773 8392.28 +0.989 8421.22 +1.273 8479.1 +1.602 8623.79 +2.011 8565.92 +2.33 8565.92 +2.682 8479.1 +3.102 8276.53 +3.568 8045.02 +3.886 7900.32 +4.239 7668.81 +4.591 7524.12 +4.739 7524.12 +4.909 7263.67 +4.955 7003.22 +4.977 6540.19 +4.989 5845.66 +5 5006.43 +5.023 4051.45 +5.034 3067.52 +5.045 1996.79 +5.08 1012.86 +5.114 318.328 +5.17 0 +; +; +A6Q 18 70 4 0.00349992 0.0153001 QU +0.1 4.8 +0.2 11.82 +0.23 7.9 +0.3 4.8 +0.41 0 +; +; +B6Q 18 70 4 0.00649998 0.0162001 QU +0.1 7 +0.18 14.38 +0.2 10.2 +0.24 6.6 +0.3 6 +0.4 6.1 +0.5 6.2 +0.6 6.3 +0.65 6.6 +0.7 3 +0.75 0 +; +; +C6 18 70 0-3-5 0.0110001 0.0203999 QU +0.05 3.8 +0.1 6.5 +0.15 11.75 +0.2 13.4 +0.25 9.25 +0.3 7 +0.4 5.6 +0.5 5.2 +0.6 5.05 +0.7 4.8 +0.8 4.5 +0.9 4.6 +1 4.45 +1.2 4.2 +1.35 4 +1.62 4 +1.63 0 +; +;Quest C6-0 from NAR data +C6-0 18 70 0 0.0083 0.0216 QU +0.02 0.497 +0.057 2.539 +0.089 5.132 +0.129 7.947 +0.159 9.437 +0.171 21.247 +0.181 23.234 +0.194 22.958 +0.204 22.185 +0.218 19.592 +0.233 17.881 +0.258 10.486 +0.308 2.428 +0.338 2.539 +0.385 2.98 +0.412 3.091 +0.442 3.422 +0.459 2.98 +0.536 3.256 +0.732 3.311 +0.747 2.483 +0.78 2.98 +1.323 3.587 +1.365 2.815 +1.887 3.808 +1.974 3.256 +2.1 3.532 +2.227 3.201 +2.247 0 +; +;Quest D5-0 by Mark Koelsch from NAR data +D5-0 20 88 0 0.025 0.0384 QU +0.096 1.241 +0.252 5.897 +0.304 8.586 +0.357 10.552 +0.391 11.483 +0.435 9.828 +0.557 6.103 +0.583 5.172 +0.67 5.172 +1.078 4.966 +1.2 4.345 +1.73 4.759 +1.8 4.759 +1.887 4.138 +2.391 5.069 +2.626 4.966 +3.009 5.379 +3.357 5.276 +3.661 5.69 +3.835 3.103 +3.887 1.655 +3.983 0 +; +;Sky Ripper Systems 29/75 G63 +G63 29 304.8 1000 0.0649998 0.236 SRS +0.01 121.91 +0.03 142.66 +0.07 156.57 +0.09 133.6 +0.13 100.62 +0.18 114.82 +0.2 105.21 +0.27 104.91 +0.35 93.38 +0.41 83.85 +0.5 67.95 +0.65 61.99 +0.83 61.99 +0.93 40.14 +1.09 17.09 +1.18 13.78 +1.29 5.56 +1.3 0 +; +;Sky Ripper Systems 29/125 G69 +G69 29 406.4 1000 0.107 0.333 SRS +0.01 99.8 +0.04 137.51 +0.07 103.01 +0.13 94.13 +0.3 80.09 +0.49 72.2 +0.57 70.72 +0.65 71.96 +0.74 80.83 +0.81 81.81 +0.94 73.43 +1.01 74.42 +1.06 85.02 +1.11 83.78 +1.19 62.1 +1.24 60.62 +1.32 65.3 +1.37 64.81 +1.43 52.98 +1.49 48.55 +1.55 44.85 +1.64 28.59 +1.85 17.74 +1.99 14.29 +2 0 +; +; +G125 38 408 1000 0.158 0.537 SRS +0.01 346.87 +0.04 325.72 +0.07 324.57 +0.08 415.57 +0.09 219.61 +0.13 194.84 +0.2 177.77 +0.4 157.13 +0.6 131.89 +0.8 88.31 +1 42.44 +1.09 14.64 +1.2 0 +; +;Sky Ripper Systems 29/185 H78 +H78 29 520.7 1000 0.158 0.418 SRS +0.01 138.21 +0.08 150.1 +0.12 142.67 +0.15 132.27 +0.22 130.49 +0.29 90.3 +0.34 88.27 +0.4 86.81 +0.61 86.52 +0.72 81.59 +0.76 71.72 +0.86 64.46 +1.01 63.3 +1.18 62.42 +1.28 60.39 +1.5 57.49 +1.8 58.36 +1.89 59.23 +2.01 55.46 +2.21 36.29 +2.36 22.94 +2.54 13.36 +2.72 9.58 +2.75 0 +; +;Sky Ripper Systems 38mm hybrid motors +;prepared by Andrew MacMillen NAR 77472 8/10/04 +;based on TMT thrust data & cert docs +;NOX weight calc'd at 90 deg. F; 0.5469 gm/cc; 984 psi +;compiled with RockSim6 EngEdit +;SRS H155 38/220 PP +H155_pp 38 508 0 0.142 0.664 SRS +0.03 308.75 +0.05 362.22 +0.09 252.41 +1.02 102.11 +1.08 119.98 +1.45 33.45 +1.66 19.06 +1.68 12.59 +1.69 0 +; +;Sky Ripper Systems 38mm hybrid motors +;prepared for SRS by Andrew MacMillen NAR 77472 8/10/04 +;based on TMT thrust data & cert docs +;NOX weight calc'd at 90 deg. F; 0.5469 gm/cc; 984 psi +;compiled with RockSim6 EngEdit +;SRS H124 38/220 PVC +H124_pvc 38 508 0 0.142 0.664 SRS +0.01 198.24 +0.02 300.84 +0.03 314.34 +0.03 316 +0.04 305.39 +0.08 280.35 +0.11 221.43 +0.69 168.38 +0.78 180.85 +0.81 158.64 +0.84 167.59 +0.89 152.32 +0.92 120.7 +0.95 123.55 +1.06 82.23 +1.35 48.36 +1.55 25.63 +1.6 21.88 +1.62 23.66 +1.66 18.58 +1.67 12.46 +1.68 0 +; +;Sky Ripper Systems 38mm hybrid motors +;prepared by Andrew MacMillen NAR 77472 8/10/04 +;based on TMT thrust data & cert docs +;NOX weight calc'd at 90 deg. F; 0.5469 gm/cc; 984 psi +;compiled with RockSim6 EngEdit +;SRS I147 38/400 PP +I147_pp 38 711 0 0.264 0.967 SRS +0 194.47 +0.02 366.71 +0.03 390.09 +0.03 392.3 +0.05 359.02 +0.07 217.4 +0.1 207.68 +0.38 241.52 +1.07 183.8 +2.33 141.34 +2.51 100.04 +2.75 71.51 +3.32 34.49 +3.89 17.18 +4.43 7.17 +4.45 0 +; +;Sky Ripper Systems 38mm hybrid motors +;prepared by Andrew MacMillen NAR 77472 8/10/04 +;based on TMT thrust data & cert docs +;NOX weight calc'd at 90 deg. F; 0.5469 gm/cc; 984 psi +;compiled with RockSim6 EngEdit +;SRS I117 38/580 PVC +I117_pvc 38 914 0 0.37 1.133 SRS +0.01 203.36 +0.02 339.95 +0.02 358.77 +0.03 367.94 +0.03 361.47 +0.06 277.4 +0.08 277.11 +0.15 250.99 +0.27 256.14 +0.3 248.56 +0.42 194.78 +0.47 222.59 +1.35 174.82 +1.39 184.03 +1.79 150.12 +2.12 156.59 +3.42 54.16 +3.8 40 +4.2 17.22 +4.23 0 +; +;Sky Ripper Systems 38mm hybrid motors +;prepared by Andrew MacMillen NAR 77472 8/10/04 +;based on TMT thrust data & cert docs +;NOX weight calc'd at 90 deg. F; 0.5469 gm/cc; 984 psi +;compiled with RockSim6 EngEdit +;SRS I119 38/400 PVC +I119_pvc 38 711 0 0.264 0.967 SRS +0 192.14 +0.01 262.2 +0.02 341.53 +0.03 338.42 +0.06 221.25 +0.07 195.93 +0.11 189.23 +0.15 202.2 +0.18 233.36 +0.47 230.26 +0.99 200.9 +1.18 165.36 +1.27 172.11 +1.48 162.61 +2.18 74.18 +2.92 24.69 +2.97 10.98 +3.1 10.06 +3.12 0 +; +;Sky Ripper Systems 54/830 J261 Gold Insert +J261 54 731.5 0 0.5647 1.9025 SRS +0.02 1303.39 +0.09 903.88 +0.21 591.22 +0.42 349.57 +0.61 304.62 +0.81 329.59 +1.01 277.16 +1.21 294.64 +1.39 232.21 +1.61 197.26 +1.82 255.99 +2 274.66 +2.2 269.67 +2.41 189.77 +2.61 294.64 +2.82 212.24 +3.01 254.69 +3.21 225.29 +3.41 194.76 +3.59 156.32 +3.74 229.72 +3.85 237.71 +3.9 156.32 +4 112.76 +4.2 140.19 +4.4 192.26 +4.48 106.66 +4.61 54.86 +4.76 33.52 +4.95 0 +; +;Sky Ripper Systems 54/550 J263 Gold Insert +J263 54 606.5 0 0.3742 1.5983 SRS +0.01 1359.46 +0.09 794.32 +0.15 559.93 +0.21 419.3 +0.4 296.89 +0.61 286.48 +0.81 265.64 +1.01 244.81 +1.2 247.41 +1.4 244.81 +1.6 231.79 +1.81 200.53 +2.01 205.74 +2.21 205.74 +2.41 195.32 +2.6 174.49 +2.8 166.68 +2.91 161.47 +3 138.03 +3.08 98.96 +3.21 62.5 +3.41 28.74 +3.6 0 +; +;Sky Ripper Systems 54/830 J337 Black Insert +J337 54 731.5 0 0.5647 1.9025 SRS +0 8.88 +0.01 1521.03 +0.1 585.29 +0.2 651.28 +0.41 589.45 +0.5 548.23 +0.6 539.99 +0.99 461.67 +1.4 416.33 +1.6 391.59 +1.8 387.47 +1.91 364.9 +2.01 239.43 +2.2 171.02 +2.4 119.72 +2.6 72.68 +2.8 42.76 +3 21.68 +3.1 0 +; +;Sky Ripper Systems 54/550 J348 Black Insert +J348 54 606.5 0 0.3742 1.5983 SRS +0 8.88 +0.02 451.8 +0.13 557.6 +0.14 1203.84 +0.2 617.65 +0.4 549.02 +0.6 494.69 +0.79 406.05 +1.01 354.57 +1.2 334.56 +1.31 303.1 +1.4 237.34 +1.6 148.69 +1.8 82.92 +2 37.17 +2.2 0 +; +;Sky Ripper Systems 38mm hybrid motors +;prepared by Andrew MacMillen NAR 77472 8/10/04 +;based on TMT thrust data & cert docs +;NOX weight calc'd at 90 deg. F; 0.5469 gm/cc; 984 psi +;compiled with RockSim6 EngEdit +;SRS J144 38/580 PP +J144_pp 38 914 0 0.37 1.133 SRS +0.01 301.25 +0.03 376.44 +0.03 376.86 +0.08 247.31 +0.22 273.45 +0.45 263.59 +0.79 231.99 +1.09 175.69 +1.21 185.68 +2.05 149.6 +2.86 127.64 +3.42 69.07 +3.88 42.69 +4.59 20.49 +5.2 10 +5.8 6.12 +5.8 0 +; +;Sky Ripper Systems 54/1130 K257 Gold Insert +K257 54 911.4 0 0.7688 2.3107 SRS +0.07 1133.08 +0.2 529.98 +0.4 333.69 +0.59 363.13 +0.8 347.18 +0.98 366.4 +1.2 356.59 +1.4 310.79 +1.6 274.8 +1.81 337.71 +2 356.59 +2.2 294.43 +2.4 314.06 +2.6 294.43 +2.81 333.69 +3 340.23 +3.22 319.78 +3.41 292.68 +3.59 249.32 +3.79 278.07 +4 243.9 +4.21 281.35 +4.41 235.54 +4.6 251.9 +4.81 211.38 +5.01 222.22 +5.2 189.7 +5.41 153.23 +5.6 81.4 +5.8 23.94 +6.1 0 +; +;Sky Ripper Systems 54/1130 K347 Black Insert +K347 54 911.4 0 0.7688 2.3107 SRS +0 8.88 +0.03 1474.51 +0.11 972.2 +0.19 737.25 +0.4 697.22 +0.61 673.87 +0.81 653.85 +1.01 600.4 +1.2 550.44 +1.4 530.42 +1.6 533.76 +1.8 517.08 +1.89 396.98 +1.95 493.19 +2.06 393.65 +2.13 443.69 +2.3 365.38 +2.3 292.31 +2.4 257.92 +2.6 184.84 +2.79 124.66 +3 81.67 +3.21 51.58 +3.41 21.49 +3.58 0 +; +;RATT Works H70H +;Copyright Tripoli Motor Testing 2002 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +H70H 29 457 0 0.106176 0.348992 RTW +0.051 124.137 +0.156 134.902 +0.261 127.047 +0.367 115.87 +0.473 110.286 +0.578 108.63 +0.683 105.741 +0.789 104.108 +0.894 101.515 +1 98.471 +1.105 93.809 +1.21 90.543 +1.316 85.219 +1.421 74.353 +1.527 57.739 +1.632 44.019 +1.738 34.554 +1.843 27.992 +1.948 22.691 +2.054 19.064 +2.159 15.665 +2.265 12.897 +2.37 11.332 +2.475 10.107 +2.581 8.591 +2.688 0 +; +;RATT Works I80H +;Copyright Tripoli Motor Testing 2002 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +I80H 29 730 0 0.21952 0.549248 RTW +0.093 84.101 +0.28 102.075 +0.469 118.708 +0.657 117.13 +0.846 114.829 +1.034 112.225 +1.222 109.818 +1.41 107.622 +1.599 105.945 +1.787 102.168 +1.976 100.449 +2.164 99.265 +2.352 96.272 +2.541 91.951 +2.729 89.38 +2.918 86.43 +3.105 54.544 +3.294 41.902 +3.482 33.368 +3.671 26.516 +3.859 21.324 +4.047 16.951 +4.235 14.387 +4.424 13.456 +4.612 12.777 +4.801 0 +; +;RATT Works I90LH +;Copyright Tripoli Motor Testing 2002 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +I90LH 29 921 0 0.285376 0.684544 RTW +0.127 137.737 +0.383 121.431 +0.64 117.048 +0.897 121.354 +1.154 118.436 +1.41 116.538 +1.668 114.826 +1.925 112.358 +2.181 110.303 +2.439 107.768 +2.696 105.749 +2.952 104.733 +3.209 102.802 +3.467 95.41 +3.723 68.281 +3.98 55 +4.237 43.62 +4.494 33.784 +4.751 31.704 +5.008 27.714 +5.265 24.875 +5.522 22.93 +5.779 21.379 +6.035 20.884 +6.293 18.637 +6.55 0 +; +;RATT Works K240H +;Copyright Tripoli Motor Testing 2002 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +K240H 64 908 0 1.29338 2.81434 RTW +0.164 413.978 +0.493 392.975 +0.822 370.841 +1.151 362.058 +1.48 337.839 +1.809 321.401 +2.139 285.118 +2.468 280.031 +2.798 275.06 +3.128 278.392 +3.457 274.394 +3.786 252.302 +4.116 272.858 +4.445 264.671 +4.774 255.572 +5.103 210.314 +5.433 163.955 +5.764 126.239 +6.093 98.015 +6.422 74.491 +6.751 55.617 +7.08 40.778 +7.409 29.618 +7.739 21.915 +8.069 17.214 +8.399 0 +; +;ROADRUNNER F35 RASP.ENG FILE +;File produced April 5, 2006 +;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. +F35 29 112 6-10 0.04 0.111 RR +0.023 33.7 +0.04 44.462 +0.081 47.206 +0.121 48.579 +0.166 49.27 +0.242 49.55 +0.315 51.01 +0.411 50.111 +0.528 49.71 +0.664 48.208 +0.791 47.256 +0.896 46.986 +1 45.484 +1.097 44.943 +1.194 42.338 +1.277 40.4 +1.323 40.706 +1.356 37.691 +1.402 35.637 +1.451 32.753 +1.505 29.467 +1.578 25.491 +1.675 20.833 +1.75 17.137 +1.828 13.021 +1.907 8.638 +1.984 5.075 +2.049 2.61 +2.13 0 +; +;ROADRUNNER F45R RASP ENG FILE +F45R 29 93 5-8-14 0.03 0.093 RR +0 4.1971 +0.019 45.5 +0.038 53.07 +0.057 52.402 +0.095 54.741 +0.113 55.298 +0.132 56.744 +0.151 57.19 +0.227 60.419 +0.284 61.754 +0.416 62.422 +0.491 60.753 +0.51 61.42 +0.567 60.307 +0.624 58.414 +0.662 58.08 +0.737 55.298 +0.775 52.959 +0.813 51.513 +0.888 46.169 +0.983 34.701 +1.002 31.807 +1.096 23.902 +1.134 21.453 +1.21 14.106 +1.229 12.992 +1.285 8.4282 +1.342 5.5328 +1.361 5.4218 +1.418 2.9723 +1.42 0 +; +;ROADRUNNER F60 RASP.ENG FILE +;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. +F60R 29 112 4-7-10 0.038 0.109 RR +0.013 45.86 +0.021 63.937 +0.029 72.291 +0.041 75.214 +0.061 74.374 +0.087 76.872 +0.155 83.122 +0.231 86.44 +0.309 88.088 +0.329 90.07 +0.345 88.33 +0.395 87.9 +0.454 87.208 +0.514 87.188 +0.616 82.141 +0.699 77.105 +0.765 70.4 +0.807 61.611 +0.859 51.983 +0.926 42.355 +0.978 33.556 +1.022 21.43 +1.061 13.056 +1.101 6.776 +1.133 3.423 +1.19 0 +; +;ROADRUNNER G80 RASP.ENG FILE +;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. +G80R 29 140 4-7-10 0.055 0.133 RR +0.012 63.563 +0.028 84.077 +0.057 89.563 +0.119 96.03 +0.206 102.518 +0.242 104.42 +0.297 106.923 +0.356 109.826 +0.422 111.829 +0.483 111.328 +0.558 112.632 +0.622 112.75 +0.683 112.129 +0.739 109.125 +0.796 102.017 +0.863 90.494 +0.901 82.75 +0.935 72.41 +0.976 59.869 +1.018 49.826 +1.028 44.321 +1.042 39.805 +1.073 28.272 +1.113 18.231 +1.17 11.176 +1.218 4.636 +1.31 0 +; +;Rocketvision F32 +;from NAR data sheet updated 11/2000 +;created by John Coker 5/2006 +F32 24 124 5-10-15 0.0377 0.0695 RV +0.01 50 +0.05 56 +0.1 48 +2 24 +2.2 19 +2.45 5 +2.72 0 +; +;Same motor as the Aerotech F72T single use from NAR cert data +F72T 24 124 5-10-15 0.0368 0.0746 RV +0.004 37.671 +0.01 78.082 +0.017 97.26 +0.027 91.781 +0.043 89.726 +0.06 80.822 +0.087 84.932 +0.101 78.767 +0.132 81.507 +0.143 78.767 +0.171 81.507 +0.192 78.082 +0.215 80.822 +0.24 78.082 +0.264 81.507 +0.279 78.767 +0.298 80.137 +0.517 76.027 +0.68 70.548 +0.855 58.219 +0.934 49.315 +0.961 43.151 +0.996 31.507 +1.025 21.233 +1.054 14.384 +1.103 7.534 +1.147 3.425 +1.196 0 +; +;Same motor as the Aerotech G55W single use from NAR cert data +G55W 24 177 5-10-15 0.0625 0.115 RV +0.004 74.648 +0.012 85.211 +0.054 81.69 +0.128 73.239 +0.182 73.944 +0.231 69.718 +0.508 69.014 +0.868 67.606 +1.037 65.493 +1.07 67.606 +1.091 64.085 +1.14 63.38 +1.161 66.901 +1.19 62.676 +1.269 62.676 +1.397 59.155 +1.496 57.042 +1.583 52.113 +1.653 45.07 +1.719 38.028 +1.76 31.69 +1.831 24.648 +1.901 19.014 +1.988 12.676 +2.083 9.155 +2.169 5.634 +2.252 3.521 +2.36 0 +; +;West Coast Hybrid motor +;prepared for WestCoast/Scott Harrison by +;Andrew MacMillen NAR 77472 9/13/02 +;based on CAR thrust curves & cert letters +;since the cert letters and test curves don't agree +;the data is hand entered data points from CAR thrust curves +;NOX weight calc'd at 90 deg. F; 0.5469 gm/cc; 984 psi +;compiled with RockSim5 EngEdit +;within 2-3 percent for total impulse, peak and average thrust +;accurate thrust profile +;NOTE: NOT WCH, CAR, TMT OR NAR APPROVED +;West Coast Hybrids I110 +I110H 38 606 0 0.327 0.824 WCH +0.05 240 +0.38 200 +0.76 182 +1.14 160 +1.52 142 +1.9 125 +2.23 113 +2.66 71 +3.04 44 +3.42 29 +3.78 22 +4 0 +; +;Animal Motor Works 38-640 +I375GG 38 369 20 0.3936 0.7338 AMW +0.013 223.878 +0.045 273.929 +0.092 312.421 +0.14 334.383 +0.219 357.983 +0.298 381.992 +0.377 410.267 +0.457 431.141 +0.536 454.458 +0.615 476.825 +0.694 495.473 +0.773 504.665 +0.852 510.942 +0.931 511.972 +1.011 489.639 +1.09 441.35 +1.169 392.762 +1.248 354.753 +1.327 292.385 +1.406 177.309 +1.486 63.879 +1.565 14.901 +1.583 0 +; +;Animal Motor Works 38-640 +I315SK 38 369 20 0.3829 0.7166 AMW +0.011 314.573 +0.03 312.796 +0.066 300.786 +0.12 304.087 +0.084 300.502 +0.175 312.998 +0.266 324.086 +0.356 332.224 +0.447 347.855 +0.538 371.972 +0.629 382.833 +0.719 385.552 +0.81 385.586 +0.901 384.836 +0.992 382.296 +1.082 378.323 +1.173 370.837 +1.264 357.564 +1.355 347.122 +1.445 328.332 +1.536 202.733 +1.627 90.867 +1.718 35.427 +1.808 8.192 +1.815 0 +; +;Animal Motor Works 54-1050 +J230SK 54 326 0 0.6578 1.1835 AMW +0.054 273.635 +0.132 235.131 +0.248 218.229 +0.365 218.503 +0.481 222.04 +0.597 226.658 +0.714 231.969 +0.83 235.208 +0.946 238.968 +1.063 243.012 +1.179 245.522 +1.295 249.208 +1.412 252.897 +1.528 256.528 +1.644 260.244 +1.76 265.497 +1.877 270.48 +1.993 273.227 +2.109 275.693 +2.226 279.851 +2.342 280.76 +2.458 274.551 +2.575 262.987 +2.691 247.241 +2.807 228.611 +2.924 213.841 +3.04 185.353 +3.156 137.595 +3.273 85.388 +3.46 0 +; +;Animal Motor Works 54-1050 +;AMW J357WW RASP.ENG file made from NAR published data +;File produced December 25, 2002 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +J357WW 54 326 0 0.5481 1.2101 AMW +0.02 129.64 +0.03 205.95 +0.05 265 +0.06 316.51 +0.09 326.05 +0.13 314.6 +0.18 301.25 +0.24 299.34 +0.35 312.69 +0.5 326.05 +0.66 333.68 +0.87 345.13 +1.07 358.48 +1.46 383.18 +1.77 398.45 +1.86 400.36 +1.98 402.35 +2.18 398.45 +2.29 390.82 +2.41 369.93 +2.51 354.67 +2.55 352.76 +2.6 347.03 +2.65 335.59 +2.69 310.79 +2.75 249.73 +2.81 175.43 +2.84 108.65 +2.9 53.38 +2.92 20.98 +2.95 0 +; +;Animal Motor Works 54-1050 +;AMW J370GG RASP.ENG file made from NAR data +;File produced FEB 20, 2003 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +J370GG 54 326 0 0.5983 1.2491 AMW +0.008 185.496 +0.024 149.516 +0.063 225.273 +0.087 272.647 +0.122 304.829 +0.158 304.829 +0.273 335.212 +0.431 363.796 +0.573 390.381 +0.707 413.168 +0.877 428.459 +1.019 441.852 +1.126 441.852 +1.224 458.46 +1.284 443.951 +1.386 440.153 +1.572 438.454 +1.651 438.554 +1.813 417.765 +2.022 404.673 +2.141 385.883 +2.212 385.883 +2.255 374.59 +2.299 387.882 +2.362 357.599 +2.401 384.184 +2.421 348.204 +2.457 316.122 +2.559 251.758 +2.697 115.635 +2.753 45.624 +2.82 0 +; +;Animal Motor Works 54-1050 +;AMW J400RR RASP.ENG file made from NAR published data +;File produced April 19, 2004 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +J400RR 54 326 0 0.558 1.2314 AMW +0.043 246.55 +0.06 317.381 +0.081 344.709 +0.107 358.372 +0.15 356.062 +0.201 365.204 +0.308 392.532 +0.568 435.734 +0.863 458.339 +1.094 469.24 +1.209 467.18 +1.466 460.148 +1.705 443.972 +1.923 423.275 +2.132 409.411 +2.303 413.831 +2.402 420.563 +2.47 413.831 +2.517 395.445 +2.543 347.421 +2.568 265.238 +2.598 128.198 +2.615 68.801 +2.632 25.398 +2.66 0 +; +;Animal Motor Works 54-1050 +;AMW J450ST RASP.ENG file made from NAR published data +;File produced SEPT 4, 2002 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +J450ST 54 326 0 0.5331 1.1964 AMW +0.009 251.586 +0.016 376.074 +0.03 413.45 +0.051 430.832 +0.094 423.296 +0.162 413.149 +0.262 395.566 +0.402 420.182 +0.495 444.898 +0.805 504.078 +1.048 536.028 +1.223 550.597 +1.299 563.18 +1.334 555.319 +1.47 560.042 +1.588 559.841 +1.764 546.98 +1.921 516.838 +1.993 496.743 +2.025 499.154 +2.047 479.16 +2.086 414.354 +2.115 344.525 +2.141 252.29 +2.177 140.161 +2.213 82.78 +2.239 50.347 +2.271 27.861 +2.296 12.86 +2.33 0 +; +;Animal Motor Works 54-1050 +;AMW J480BB RASP.ENG file made from NAR published data +;File produced April 19, 2004 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +J480BB 54 326 0 0.556 1.2131 AMW +0.015 225.429 +0.041 348.18 +0.071 388.127 +0.194 422.453 +0.385 459.49 +0.699 502.347 +0.968 528.042 +1.2 536.573 +1.454 543.15 +1.674 533.763 +1.887 522.321 +2.044 519.41 +2.108 525.131 +2.164 528.042 +2.197 488.095 +2.25 419.543 +2.283 333.928 +2.328 231.15 +2.354 176.95 +2.392 111.309 +2.418 68.501 +2.436 37.106 +2.49 0 +; +;AMW J500ST RASP.ENG file made from Tripoli published data +;File produced May 15, 2004 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to the people who produced the data. +;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. +J500ST 38 370 0 0.3265 0.744 AMW +0.008 448.516 +0.027 506.086 +0.048 448.426 +0.08 450.851 +0.101 498.901 +0.117 532.131 +0.163 563.565 +0.227 616.105 +0.285 666.398 +0.312 668.643 +0.32 692.444 +0.362 728.024 +0.442 757.108 +0.493 771.477 +0.528 778.578 +0.576 779 +0.631 778.662 +0.706 716.631 +0.754 620.146 +0.77 598.591 +0.813 526.293 +0.887 439.895 +0.973 343.841 +1.074 230.949 +1.095 238.089 +1.111 214.11 +1.13 185.279 +1.194 98.836 +1.255 36.368 +1.3 0 +; +;Animal Motor Works 54-1400 +J365SK 54 403 0 0.7571 1.4593 AMW +0.029 389.731 +0.123 360.219 +0.218 334.2 +0.376 326.15 +0.534 334.217 +0.692 341.669 +0.85 347.676 +1.007 359.408 +1.165 370.043 +1.323 383.343 +1.481 399.248 +1.639 417.477 +1.797 443.735 +1.955 472.683 +2.112 501.668 +2.27 497.077 +2.428 425.371 +2.586 349.017 +2.744 262.068 +2.902 107.073 +3.06 41.821 +3.157 0 +; +;Animal Motor Works 75-1700 +;AMW K365RR RASP.ENG file made from NAR published data +;File produced April 19, 2004 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +K365RR 75 244 0 0.946 2.3456 AMW +0.049 138.157 +0.068 381.241 +0.084 454.75 +0.106 481.536 +0.164 488.182 +0.291 514.867 +0.435 545.982 +0.666 561.49 +0.868 565.73 +1.082 565.518 +1.296 550.111 +1.591 529.871 +1.805 509.731 +1.828 536.517 +1.886 498.554 +2.124 467.237 +2.501 411.35 +2.924 328.677 +3.296 241.573 +3.638 172.293 +3.969 100.798 +4.195 56.098 +4.265 51.607 +4.346 35.959 +4.433 15.859 +4.51 0 +; +;AMW K450BB RASP.ENG file made from NAR published data +;File produced Aug 19, 2003 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane. +;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. +K450BB 75 302 0 0.8816 2.8349 AMW +0.03 78.903 +0.045 227.9 +0.064 449.955 +0.069 508.417 +0.094 555.187 +0.151 563.956 +0.362 625.442 +0.562 651.85 +0.825 660.62 +1.134 652.254 +1.453 626.147 +1.793 594.296 +2.113 538.958 +2.458 469.106 +2.798 384.538 +3.165 276.686 +3.201 279.609 +3.325 232.94 +3.51 171.757 +3.732 107.65 +3.861 58.018 +3.959 40.55 +4.036 20.149 +4.11 0 +; +;AMW K470ST RASP.ENG file made from Tripoli published data +;File produced May 15, 2004 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to the people who produced the data. +;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. +K470ST 75 302 0 0.826 2.779 AMW +0.028 699.309 +0.039 799.337 +0.09 765.845 +0.157 770.311 +0.258 785.941 +0.41 804 +0.572 794.425 +0.707 794.425 +0.886 792.192 +0.998 783.261 +1.15 752.002 +1.318 709.579 +1.447 655.992 +1.593 595.707 +1.728 522.025 +1.885 444.101 +2.092 354.923 +2.356 270.167 +2.664 187.554 +2.945 131.734 +3.27 78.058 +3.433 55.686 +3.478 48.987 +3.556 28.909 +3.7 0 +; +;Animal Motor Works 54-1400 +;AMW K475WW RASP.ENG file made from NAR data +;File produced Feb 22, 2003 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +K475WW 54 403 0 0.7286 1.4925 AMW +0.022 127.831 +0.041 386.016 +0.063 548.326 +0.096 521.308 +0.134 499.129 +0.18 486.83 +0.285 486.83 +0.478 501.649 +0.731 523.727 +1.096 553.266 +1.433 577.962 +1.601 588.29 +1.756 582.704 +1.895 580.284 +1.958 575.344 +2.063 550.746 +2.209 518.788 +2.344 477.051 +2.495 417.974 +2.561 354.058 +2.582 334.399 +2.599 331.98 +2.62 297.501 +2.67 226.226 +2.707 157.37 +2.74 98.353 +2.799 49.176 +2.853 17.208 +2.94 0 +; +;Animal Motor Works 54-1400 +;AMW K530GG RASP.ENG file made from NAR data +;File produced Feb 25, 2003 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +K350GG 54 403 0 0.7967 1.616 AMW +0.013 129.764 +0.054 171.852 +0.096 284.122 +0.138 392.892 +0.171 455.975 +0.217 501.662 +0.238 498.063 +0.326 508.66 +0.542 564.745 +0.755 613.831 +1.01 645.423 +1.17 657.23 +1.273 648.922 +1.51 638.425 +1.656 634.925 +1.702 606.833 +1.803 606.833 +1.857 585.839 +1.936 589.338 +1.974 575.242 +2.015 589.338 +2.04 564.745 +2.132 536.652 +2.207 540.251 +2.291 522.656 +2.357 487.566 +2.42 375.297 +2.478 242.033 +2.529 140.361 +2.583 66.651 +2.66 0 +; +;Animal Motor Works 54-1400 +;AMW K560RR RASP.ENG file made from NAR published data +;File produced April 19, 2004 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +K560RR 54 430 0 0.75 1.5866 AMW +0.023 229.13 +0.046 415.135 +0.059 485.264 +0.078 512.268 +0.106 525.67 +0.154 523.05 +0.211 528.39 +0.261 536.451 +0.369 560.734 +0.511 587.738 +0.657 603.86 +0.77 612.022 +1.096 625.73 +1.358 620.083 +1.627 612.022 +1.839 603.86 +2.057 590.459 +2.218 598.52 +2.335 609.301 +2.385 601.24 +2.407 585.018 +2.426 533.831 +2.467 385.511 +2.507 283.037 +2.542 164.441 +2.576 67.399 +2.595 29.653 +2.62 0 +; +;Animal Motor Works 54-1750 +;AMW K570WW RASP.ENG file made from NAR published data +;File produced December 25, 2002 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +K570WW 54 492 0 0.9146 1.8151 AMW +0.02 364.42 +0.03 664.79 +0.051 751.47 +0.071 745.81 +0.096 705.25 +0.137 674.93 +0.284 661.38 +0.528 651.24 +0.913 644.51 +1.192 651.24 +1.43 651.24 +1.649 651.24 +1.872 644.51 +2.176 624.23 +2.318 600.64 +2.394 597.33 +2.455 546.63 +2.501 485.89 +2.562 421.84 +2.597 340.83 +2.638 266.54 +2.734 175.48 +2.836 97.86 +2.927 47.24 +3.04 0 +; +;Animal Motor Works 75-2500 +;AMW K600WW RASP.ENG file made from NAR data +;File produced August 22, 2002 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +K600WW 75 368 0 1.2233 2.9129 AMW +0.01 412.229 +0.029 522.21 +0.059 547.215 +0.083 524.8 +0.122 497.305 +0.181 484.852 +0.333 495.113 +0.69 560.464 +1.195 643.548 +1.4 673.833 +1.42 708.799 +1.508 701.427 +1.591 721.551 +1.782 731.712 +2.017 752.035 +2.174 756.816 +2.257 765.2 +2.502 766.44 +2.727 752.931 +2.918 738.187 +3.143 705.91 +3.408 643.847 +3.603 569.131 +3.692 526.793 +3.745 439.426 +3.799 289.596 +3.883 112.272 +3.922 64.862 +3.971 37.437 +3.995 22.474 +4.07 0 +; +;Animal Motor Works 75-2500 +;AMW K605RR RASP.ENG file made from NAR published data +;File produced April 19, 2004 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +K605RR 75 368 0 1.231 2.7688 AMW +0.03 165.845 +0.053 309.12 +0.077 361.916 +0.142 392.042 +0.527 501.412 +0.988 606.905 +1.515 682.37 +2.101 730.593 +2.355 737.58 +2.692 731.289 +3 712.497 +3.361 671.036 +3.503 663.479 +3.586 659.701 +3.645 633.353 +3.692 573 +3.734 444.838 +3.775 297.785 +3.828 162.066 +3.864 98.015 +3.905 41.471 +3.95 0 +; +;Animal Motor Works 54-1750 +;AMW K650RR RASP.ENG file made from NAR published data +;File produced April 19, 2004 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +K650RR 54 492 0 0.931 1.8087 AMW +0.022 308.257 +0.045 566.48 +0.058 620.44 +0.081 639.668 +0.135 639.668 +0.229 643.494 +0.351 662.823 +0.594 701.38 +0.81 724.434 +0.999 743.763 +1.151 751.22 +1.381 747.588 +1.61 736.001 +1.835 709.031 +2.073 685.876 +2.244 674.4 +2.334 682.051 +2.429 685.876 +2.469 666.648 +2.528 597.285 +2.573 481.714 +2.609 358.391 +2.631 250.471 +2.681 146.477 +2.721 65.507 +2.748 23.124 +2.77 0 +; +;Animal Motor Works 54-2550 +;AMW K670GG RASP.ENG file made from NAR data +;File produced August 22, 2002 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +K670GG 54 492 0 1.014 1.9145 AMW +0.016 294.054 +0.035 398.582 +0.086 506.299 +0.153 496.434 +0.264 506.1 +0.461 558.114 +0.722 629.56 +0.983 688.052 +1.116 714.06 +1.193 785.805 +1.409 788.794 +1.737 804.56 +2.074 781.42 +2.195 764.879 +2.226 781.221 +2.277 764.779 +2.398 751.527 +2.44 744.95 +2.468 718.843 +2.484 666.529 +2.525 418.112 +2.551 218.821 +2.573 120.77 +2.595 52.144 +2.62 0 +; +;Animal Motor Works 54-1400 +;AMW K700BB RASP.ENG file made from NAR published data +;File produced April 19, 2004 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +K700BB 54 430 0 0.754 1.4831 AMW +0.014 359.559 +0.022 625.425 +0.03 737.756 +0.047 771.505 +0.082 786.516 +0.106 771.505 +0.144 775.233 +0.272 786.516 +0.477 812.71 +0.693 842.632 +0.97 847.06 +1.283 838.904 +1.516 816.438 +1.706 801.427 +1.779 793.972 +1.811 775.233 +1.841 726.573 +1.873 625.425 +1.909 509.367 +1.95 393.208 +1.982 337.093 +2.035 292.16 +2.073 228.489 +2.111 153.535 +2.155 86.137 +2.193 37.446 +2.24 0 +; +;Animal Motor Works 54-1750 +;AMW K800BB RASP.ENG file made from NAR published data +;File produced April 19, 2004 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +K800BB 54 492 0 0.914 1.7866 AMW +0.017 516.316 +0.035 745.845 +0.046 817.592 +0.09 860.56 +0.191 889.338 +0.27 908.424 +0.438 918.017 +0.689 945.892 +0.996 955.09 +1.325 922.713 +1.557 894.035 +1.726 874.949 +1.849 884.542 +1.92 894.035 +1.954 894.035 +1.984 855.863 +2.011 741.048 +2.049 592.859 +2.079 492.433 +2.113 430.28 +2.154 377.719 +2.196 329.854 +2.237 243.818 +2.275 152.986 +2.309 71.716 +2.339 33.465 +2.38 0 +; +;Animal Motor Works 54-1750 +;AMW K950ST RASP.ENG file made from NAR published data +;File produced SEPT 4, 2002 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +K950ST 54 492 0 0.8874 1.7949 AMW +0.011 771.836 +0.025 1204.52 +0.039 1083.24 +0.053 1158.05 +0.067 1036.36 +0.085 1110.18 +0.099 1022.4 +0.135 982.102 +0.22 968.835 +0.404 1010.43 +0.566 1044.34 +0.701 1079.25 +0.867 1106.19 +0.995 1134.12 +1.211 1114.17 +1.313 1101.2 +1.43 1067.29 +1.529 1020.4 +1.579 993.772 +1.642 892.43 +1.674 818.119 +1.717 757.273 +1.738 621.918 +1.766 466.313 +1.791 351.306 +1.823 249.864 +1.865 175.553 +1.908 87.696 +1.943 33.654 +1.97 0 +; +;Animal Motor Works 54-2550 +;AMW K975WW RASP.ENG file made from NAR published data +;File produced December 25, 2002 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +K975WW 54 728 0 1.3573 2598.5 AMW +0.017 526.644 +0.029 901.85 +0.038 1098.92 +0.046 1151.72 +0.076 1112.87 +0.13 1060.06 +0.219 1053.09 +0.336 1053.09 +0.479 1059.07 +0.609 1091.94 +0.866 1136.78 +1.046 1176.63 +1.164 1175.63 +1.202 1228.44 +1.239 1208.51 +1.315 1215.49 +1.353 1267.29 +1.387 1228.44 +1.487 1241.39 +1.538 1260.32 +1.634 1290.9 +1.723 1281.24 +1.794 1266.3 +1.836 1207.52 +1.933 1049.1 +1.992 851.437 +2.08 666.923 +2.118 640.521 +2.193 462.582 +2.269 212.311 +2.378 119.854 +2.51 0 +; +;Animal Motor Works 54-2550 +;AMW K1000SK RASP.ENG file made from NAR published data +;File produced April 19, 2004 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +K1000SK 54 728 0 1.297 2.556 AMW +0.019 1155.06 +0.045 1426.12 +0.094 1248.23 +0.161 1112.99 +0.239 1128.02 +0.343 1113.99 +0.377 1149.05 +0.44 1121 +0.544 1221.18 +0.633 1178.11 +0.674 1221.18 +0.737 1193.13 +0.883 1200.14 +1.009 1194.13 +1.057 1236.21 +1.188 1137.03 +1.299 1145.05 +1.396 1087.94 +1.516 954.104 +1.631 855.228 +1.717 827.077 +1.777 650.061 +1.848 465.932 +1.93 303.141 +2.023 147.463 +2.083 83.879 +2.132 41.484 +2.18 0 +; +;Animal Motor Works 54-2550 +;AMW K1075GG RASP.ENG file made from NAR data +;File produced Feb 22, 2003 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +K1075GG 54 726 0 1.3999 2.6658 AMW +0.009 672.664 +0.015 963.511 +0.022 860.518 +0.047 987.857 +0.075 975.835 +0.106 921.332 +0.215 958.001 +0.529 1092.05 +0.878 1220.29 +1.077 1269.39 +1.158 1311.47 +1.235 1293.43 +1.448 1330.5 +1.577 1318.48 +1.672 1319.48 +1.721 1337.52 +1.759 1337.52 +1.805 1337.52 +1.829 1331.5 +1.856 1384.67 +1.889 1277.4 +1.906 1216.29 +1.938 1052.98 +1.96 871.338 +1.988 659.239 +2.027 453.352 +2.062 301.967 +2.115 138.46 +2.168 41.608 +2.2 0 +; +;AMW L700BB RASP.ENG file made from NAR published data +;File produced Aug 19, 2003 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane. +;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. +L700BB 75 368 0 1.1931 2.732 AMW +0.024 221.872 +0.033 399.33 +0.048 467.56 +0.076 494.892 +0.134 498.409 +0.239 535.991 +0.482 614.671 +0.769 683.202 +1.232 755.251 +1.623 789.717 +1.919 810.417 +2.258 821.14 +2.582 817.853 +2.912 801.072 +3.136 773.941 +3.255 750.126 +3.322 743.393 +3.37 729.828 +3.418 688.83 +3.461 593.368 +3.499 484.14 +3.532 368.179 +3.57 248.802 +3.618 149.824 +3.661 61.135 +3.72 0 +; +;Animal Motor Works 75-3500 +;AMW L777WW RASP.ENG file made from NAR published data +;File produced SEPT 4, 2002 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +L777WW 75 497 0 1.7623 3.6987 AMW +0.025 140.882 +0.064 209.474 +0.108 360.055 +0.204 652.185 +0.36 641.518 +0.373 693.745 +0.418 683.28 +0.528 730.073 +0.67 761.268 +0.761 781.998 +0.787 802.828 +0.871 802.728 +1.065 854.754 +1.338 911.811 +1.668 963.636 +1.914 989.498 +2.115 1000.16 +2.368 962.831 +2.647 926 +2.985 878.603 +3.303 805.143 +3.472 752.815 +3.55 705.72 +3.602 648.26 +3.647 611.631 +3.693 512.409 +3.779 334.897 +3.857 178.216 +3.935 89.379 +3.981 26.687 +4.05 0 +; +;Animal Motor Works 75-3500 +;AMW L900RR RASP.ENG file made from NAR published data +;File produced April 19, 2004 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +L900RR 75 497 0 1.771 3.5888 AMW +0.029 464.292 +0.053 630.937 +0.059 684.506 +0.096 702.328 +0.133 696.387 +0.201 714.311 +0.486 803.524 +0.777 910.661 +1.099 988.093 +1.26 1041.16 +1.284 1071.37 +1.378 1053.24 +1.607 1101.57 +1.917 1142.86 +2.208 1173.56 +2.413 1160.98 +2.624 1107.62 +2.866 976.211 +3.053 886.897 +3.208 839.27 +3.314 827.388 +3.382 809.465 +3.432 720.252 +3.495 547.564 +3.57 345.273 +3.627 214.273 +3.714 77.382 +3.79 0 +; +;Animal Motor Works 75-3500 +;AMW L1060GG RASP.ENG file made from NAR data +;File produced August 22, 2002 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +L1060GG 75 497 0 1.9188 3.9388 AMW +0.02 258.765 +0.024 368.224 +0.032 328.375 +0.076 427.947 +0.1 567.267 +0.116 751.329 +0.128 791.178 +0.169 816.045 +0.225 816.045 +0.309 875.768 +0.518 985.227 +0.763 1079.61 +1.024 1174.48 +1.308 1229.41 +1.606 1288.34 +1.782 1298.25 +1.983 1293.33 +2.256 1239.4 +2.525 1184.47 +2.822 1129.54 +3.038 1069.62 +3.111 1044.65 +3.135 995.114 +3.183 835.92 +3.239 552.286 +3.299 268.652 +3.327 164.187 +3.339 84.59 +3.36 44.782 +3.4 0 +; +;Animal Motor Works 75-3500 +;AMW L1080BB RASP.ENG file made from NAR published data +;File produced April 19, 2004 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +L1080BB 75 497 0 1.717 3.5922 AMW +0.024 406.295 +0.043 812.489 +0.052 895.202 +0.088 929.641 +0.314 991.55 +0.626 1087.69 +0.988 1163.44 +1.346 1218.99 +1.638 1246.25 +1.864 1257.91 +2.247 1254.84 +2.6 1218.99 +2.766 1211.92 +2.851 1197.78 +2.942 1204.85 +3.002 1226.06 +3.033 1204.85 +3.089 1040.23 +3.124 874.499 +3.15 660.999 +3.191 461.336 +3.232 275.408 +3.268 144.622 +3.303 75.744 +3.339 41.316 +3.39 0 +; +;Animal Motor Works 54-2550 +;AMW L1100RR RASP.ENG file made from NAR published data +;File produced April 19, 2004 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +L1100RR 54 728 0 1.346 2.5881 AMW +0.013 681.489 +0.029 1116.88 +0.041 1196.3 +0.079 1210.38 +0.147 1203.34 +0.257 1218.42 +0.366 1225.45 +0.567 1254.61 +0.824 1282.76 +1.059 1311.91 +1.267 1340.23 +1.459 1311.91 +1.622 1297.84 +1.713 1290.8 +1.785 1268.68 +1.83 1218.42 +1.886 1080.69 +1.969 819.214 +2.048 558.24 +2.108 376.985 +2.156 246.498 +2.205 144.963 +2.269 72.501 +2.35 0 +; +;AMW L1111ST RASP.ENG file made from Tripoli published data +;File produced May 15, 2004 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to the people who produced the data. +;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. +L1111ST 75 497 0 1.642 3.517 AMW +0.012 947.531 +0.034 1002.77 +0.055 956.063 +0.109 947.531 +0.238 986.151 +0.485 1058 +0.732 1138.83 +1.027 1232.24 +1.312 1317.56 +1.527 1359.77 +1.624 1372.8 +1.726 1379.4 +1.866 1368.31 +1.93 1343.16 +2.075 1296.01 +2.275 1211.13 +2.469 1130.3 +2.609 1066.53 +2.738 998.724 +2.76 964.595 +2.803 934.957 +2.879 790.357 +2.928 624.652 +2.993 433.483 +3.031 254.979 +3.08 140.243 +3.1 67.989 +3.14 0 +; +;Animal Motor Works 54-2550 +;AMW L1300BB RASP.ENG file made from NAR published data +;File produced April 19, 2004 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +L1300BB 54 728 0 1.314 2.5454 AMW +0.014 710.467 +0.025 1247.64 +0.039 1384.13 +0.053 1447.83 +0.074 1420.53 +0.12 1447.83 +0.276 1474.12 +0.475 1519.61 +0.712 1555 +0.942 1586.74 +1.147 1562.08 +1.36 1534.78 +1.484 1551.97 +1.537 1551.97 +1.569 1497.37 +1.59 1406.38 +1.604 1451.87 +1.615 1333.58 +1.64 1168.78 +1.689 986.687 +1.753 767.749 +1.824 512.503 +1.891 275.512 +1.933 147.816 +1.987 74.737 +2.06 0 +; +;Animal Motor Works 75-6000 +;AMW M1350WW RASP.ENG file made from NAR data +;File produced Nov 3, 2002 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +M1350WW 75 785 0 2.9673 5.6322 AMW +0.026 728.705 +0.046 1381.7 +0.066 1609.64 +0.092 1662.71 +0.151 1609.64 +0.242 1592.57 +0.478 1592.57 +1.041 1592.57 +1.71 1635.75 +2.299 1643.78 +2.672 1601.61 +3.092 1508.22 +3.197 1500.19 +3.249 1423.87 +3.301 1338.52 +3.386 1067.4 +3.524 788.05 +3.721 440.617 +3.779 389.807 +3.838 381.272 +3.904 364.402 +3.976 305.058 +4.055 194.903 +4.14 93.214 +4.23 0 +; +;Animal Motor Works 75-6000 +;AMW M1480RR RASP.ENG file made from NAR published data +;File produced April 19, 2004 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +M1480RR 75 785 0 3 5.5248 AMW +0.022 713.002 +0.032 1254.68 +0.055 1473.37 +0.078 1569.11 +0.156 1569.11 +0.352 1559.03 +0.642 1597.33 +0.974 1644.69 +1.289 1702.13 +1.52 1739.42 +1.918 1796.87 +2.279 1814.83 +2.481 1796.87 +2.707 1739.42 +2.968 1644.69 +3.058 1616.47 +3.135 1520.73 +3.218 1378.64 +3.284 1217.39 +3.332 1065.22 +3.344 1140.8 +3.368 1016.85 +3.41 741.522 +3.5 522.935 +3.613 275.727 +3.691 171.12 +3.768 66.553 +3.85 0 +; +;AMW M1850GG RASP.ENG file made from Tripoli published data +;File produced May 15, 2004 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to the people who produced the data. +;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. +M1850GG 75 781 0 3.375 5.851 AMW +0.012 1326.73 +0.018 894.224 +0.069 1177.46 +0.099 1244.68 +0.211 1319.32 +0.271 1535.34 +0.434 1714.28 +0.642 1990.1 +0.779 2012.35 +1.069 2191.29 +1.257 2263.51 +1.46 2267.93 +1.658 2269 +1.959 2268.48 +2.254 2258.04 +2.508 2183.87 +2.564 2235.79 +2.595 2153.74 +2.687 2124.07 +2.733 2064.27 +2.779 1833.41 +2.82 1468.12 +2.857 1118.13 +2.903 752.835 +2.97 424.814 +3.042 201.235 +3.149 59.614 +3.2 0 +; +;Animal Motor Works 75-6000 +;AMW M1900BB RASP.ENG file made from NAR published data +;File produced April 19, 2004 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +M1900BB 75 785 0 2.733 5.4225 AMW +0.018 1109.21 +0.044 1761.75 +0.061 1910.65 +0.085 1938.62 +0.159 1929.63 +0.29 1956.62 +0.409 2031.56 +0.438 1974.6 +0.569 2011.58 +0.815 2104.51 +1.073 2197.44 +1.401 2280.39 +1.688 2324.7 +1.905 2297.37 +2.073 2241.41 +2.254 2138.49 +2.397 2063.54 +2.479 2016.57 +2.54 2025.57 +2.581 2006.58 +2.63 1885.67 +2.716 1493.94 +2.805 1120.21 +2.887 840.605 +2.972 569.996 +3.046 299.488 +3.119 150.193 +3.168 56.829 +3.23 0 +; +;Animal Motor Works 75-7600 +;AMW M2200SK RASP.ENG file made from NAR published data +;File produced April 19, 2004 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +M2200SK 75 1039 0 3.766 7.0098 AMW +0.02 972.329 +0.049 1612.84 +0.101 1601.78 +0.243 1701.33 +0.482 1878.3 +0.571 1889.36 +0.802 2088.45 +0.997 2254.36 +1.073 2254.36 +1.227 2486.63 +1.426 2574.11 +1.616 2651.53 +1.681 2751.08 +1.782 2839.56 +1.831 2817.44 +1.961 2916.99 +2.07 2979.38 +2.155 2939.11 +2.196 2961.23 +2.256 2872.75 +2.321 2839.56 +2.374 2684.72 +2.422 2331.78 +2.483 1568.6 +2.524 1215.66 +2.584 1094 +2.674 1060.81 +2.747 961.268 +2.868 740.358 +2.953 464.043 +3.046 165.708 +3.11 0 +; +;Animal Motor Works 75-7600 +;AMW M2500GG RASP.ENG file made from NAR data +;File produced DEC 25, 2002 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +M2500GG 75 1039 0 4.248 7.5515 AMW +0.026 1288.79 +0.053 2021.4 +0.079 2140.01 +0.123 2105.12 +0.207 2117.09 +0.54 2309.46 +0.971 2560.64 +1.265 2727.09 +1.48 2836.74 +1.678 2920.46 +1.757 2980.27 +1.946 2995.51 +2.047 2959.34 +2.24 2889.56 +2.31 2854.68 +2.486 2820.79 +2.526 2880.59 +2.592 2773.94 +2.653 2821.78 +2.706 2752.01 +2.758 2752.01 +2.807 2763.97 +2.842 2504.82 +2.886 2115.09 +2.93 1630.67 +2.987 1051.57 +3.04 437.571 +3.057 284.072 +3.079 142.434 +3.097 83.497 +3.11 0 +; +;AMW M3000ST RASP.ENG file made from Tripoli published data +;File produced May 15, 2004 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to the people who produced the data. +;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. +M3000ST 75 1038 0 3.819 7.5515 AMW +0.014 2721.02 +0.032 2553.37 +0.096 2601.84 +0.22 2722.8 +0.353 2807.73 +0.476 2928.24 +0.518 3048.75 +0.577 3061.2 +0.76 3314.22 +0.944 3519.67 +1.14 3772.69 +1.315 3942.12 +1.511 4039.5 +1.617 4088.42 +1.708 4115 +1.791 4089.75 +1.837 4006.15 +1.873 3814.49 +1.951 3359.58 +2.002 2784.61 +2.052 2257.66 +2.111 1587.08 +2.162 1108.15 +2.221 629.227 +2.308 318.126 +2.395 139.052 +2.446 67.503 +2.5 0 +; +;Animal Motor Works 98-11000 +M1730SK 98 870 0 4.9452 9.8718 AMW +0.04 682.642 +0.064 1153.39 +0.221 1354.66 +0.269 1414.77 +0.381 1458.03 +0.541 1526.92 +0.701 1589.2 +0.861 1675.2 +1.021 1732.67 +1.181 1802.23 +1.341 1886.64 +1.5 1973.71 +1.66 2070.51 +1.82 2183.82 +1.98 2299.31 +2.14 2433.86 +2.3 2568.12 +2.46 2679.42 +2.62 2638.38 +2.78 2484.18 +2.94 2306.04 +3.099 2173.85 +3.259 2074.69 +3.419 1961.3 +3.579 1807.81 +3.739 1640.26 +3.899 1303.04 +4.059 940.6 +4.219 567.152 +4.379 309.143 +4.539 188.981 +4.637 0 +; +;Animal Motor Works 98-11000 +N2020WT 98 870 0 5.1609 9.9693 AMW +0.106 1941.34 +0.221 2151.15 +0.381 2253.41 +0.541 2340.79 +0.701 2400.85 +0.861 2453.82 +1.021 2506.31 +1.181 2556.31 +1.341 2607.25 +1.5 2652.79 +1.66 2688.66 +1.82 2710.68 +1.98 2729.8 +2.14 2733.89 +2.3 2704.26 +2.46 2634.58 +2.62 2532.16 +2.78 2433.38 +2.94 2329.74 +3.099 2234.25 +3.259 2165.8 +3.419 2099.68 +3.579 2028.35 +3.739 1951.01 +3.899 1871.32 +4.059 1558.11 +4.219 1053.38 +4.379 890.506 +4.539 636.689 +4.998 0 +; +;Animal Motor Works 98-11000 +N2700BB 98 870 0 4.7837 9.9308 AMW +0.027 2229.53 +0.069 2476.18 +0.111 2539.74 +0.36 2723.21 +0.527 2863.83 +0.735 3016.48 +0.943 3141.25 +1.151 3241.72 +1.359 3335.56 +1.567 3519.92 +1.775 3425.88 +1.983 3420.56 +2.191 3356.08 +2.399 3270.48 +2.607 3182.6 +2.815 3098.31 +3.023 3002.95 +3.231 2888.73 +3.439 2266.61 +3.647 1498.26 +3.855 780.04 +4.063 233.545 +4.16 0 +; +;Animal Motor Works 98-11000 +N2600GG 98 870 0 4.8812 10.4726 AMW +0.024 1674.37 +0.064 1949.62 +0.104 2039.52 +0.306 2189.98 +0.508 2334.45 +0.709 2491.23 +0.911 2668.93 +1.113 2874.7 +1.314 3038.83 +1.516 3191.29 +1.718 3266.01 +1.92 3318.98 +2.121 3336.18 +2.323 3229.26 +2.525 3089.68 +2.726 2943.98 +2.928 2847.69 +3.13 2751.68 +3.331 2682.22 +3.533 2463.48 +3.735 1339.63 +3.937 269.834 +4.034 0 +; +;Animal Motor Works 98-17500 +N4000BB 98 1213 0 6.1026 13.6683 AMW +0.029 4207.59 +0.071 4709.55 +0.113 4906.31 +0.155 5007.78 +0.239 5041.56 +0.323 4993.6 +0.534 5046.91 +0.744 5145.82 +0.954 5248.06 +1.165 5293.2 +1.375 5232.46 +1.585 5209.53 +1.796 5165.47 +2.006 5047.7 +2.216 4913.09 +2.427 4783.45 +2.637 4659.16 +2.847 4195.99 +3.058 2850.73 +3.268 1981.97 +3.478 1295.54 +3.689 907.699 +3.899 490.196 +4.11 316.338 +4.207 0 +; +;Animal Motor Works 38-390 +I195WT 38 249 17 0.193 0.495 AMW +0.002 10.548 +0.018 42.653 +0.046 136.214 +0.064 179.784 +0.072 191.248 +0.078 197.211 +0.088 198.587 +0.126 198.587 +0.175 207.759 +0.217 211.887 +0.349 216.931 +0.401 221.059 +0.554 225.646 +0.586 228.856 +0.626 228.48 +0.65 230.232 +1.013 231.607 +1.105 230.691 +1.2 225.187 +1.356 210.511 +1.392 207.759 +1.441 206.842 +1.457 205.007 +1.519 181.159 +1.563 155.936 +1.693 49.992 +1.727 28.435 +1.756 16.512 +1.798 7.338 +1.86 1.376 +1.89 0 +; +;Animal Motor Works 38-390 +I220SK 38 249 20 0.202 0.495 AMW +0.005 12.747 +0.019 45.25 +0.036 79.666 +0.052 125.554 +0.069 162.519 +0.076 169.53 +0.095 174.629 +0.167 176.541 +0.229 191.199 +0.447 235.175 +0.602 260.668 +0.733 288.073 +0.85 302.095 +0.974 301.457 +1.094 289.985 +1.184 268.954 +1.268 240.273 +1.302 219.879 +1.388 177.178 +1.418 147.224 +1.435 127.467 +1.473 91.139 +1.504 65.645 +1.543 40.789 +1.593 19.12 +1.622 10.197 +1.65 0 +; +;AMW 38-390 +I271BB 38 258 0 0.189 0.493 AMW +0.011 119.53 +0.035 213.907 +0.05 245.903 +0.074 262.705 +0.115 269.446 +0.225 267.736 +0.346 282.929 +0.465 296.411 +0.584 303.152 +0.727 311.504 +0.916 318.245 +1.054 324.986 +1.162 331.4 +1.201 326.696 +1.225 313.214 +1.242 286.249 +1.268 240.99 +1.294 188.888 +1.323 136.833 +1.346 87.565 +1.368 45.467 +1.392 18.523 +1.43 0 +; +;AMW 38-390 +I285GG 38 258 0 0.206 0.515 AMW +0.013 61.575 +0.032 119.327 +0.055 164.575 +0.076 191.004 +0.094 201.014 +0.139 212.326 +0.232 231.247 +0.357 258.876 +0.456 267.686 +0.592 278.998 +0.716 289.358 +0.841 291.2 +0.936 290.31 +1.051 285.204 +1.139 277.696 +1.204 280.199 +1.243 278.998 +1.265 268.887 +1.286 242.559 +1.319 187.2 +1.359 134.443 +1.387 86.702 +1.407 52.776 +1.428 31.413 +1.448 16.337 +1.465 5.026 +1.48 0 +; +;Animal Motor Works 38-640 +I325WT 38 370 17 0.317 0.712 AMW +0.014 68.71 +0.022 113.038 +0.026 153.671 +0.037 244.545 +0.045 299.216 +0.055 330.246 +0.065 350.194 +0.079 365.709 +0.094 376.79 +0.124 381.963 +0.185 373.836 +0.252 373.836 +0.35 381.224 +0.47 382.701 +0.622 388.611 +1.102 384.179 +1.366 364.971 +1.379 360.537 +1.415 331.724 +1.49 223.119 +1.505 211.298 +1.551 187.657 +1.592 162.538 +1.688 80.529 +1.726 50.978 +1.775 27.336 +1.806 16.993 +1.834 9.605 +1.901 0 +; +;Animal Motor Works 54-1750 K555 skidmark +;File provide by Joel Rogers of AMW +K555SK 54 492 0 0.8707 1.7343 AMW +0.063 507.328 +0.144 535.181 +0.226 559.826 +0.308 585.793 +0.389 607.239 +0.471 629.034 +0.553 664.586 +0.634 683.688 +0.716 697.625 +0.798 719.618 +0.879 756.521 +0.961 777.7 +1.043 789.004 +1.124 797.934 +1.206 801.689 +1.288 804.331 +1.369 799.414 +1.451 768.014 +1.533 704.469 +1.614 641.709 +1.696 568.727 +1.778 481.013 +1.859 401.614 +1.941 333.897 +2.023 277.226 +2.104 205.009 +2.186 129.425 +2.268 73.717 +2.349 22.38 +2.368 0 +; +;Animal Motor Works 75-3500 +L666SK 75 497 0 1.8877 3.5344 AMW +0.096 105.88 +0.175 509.783 +0.312 549.481 +0.449 577.319 +0.586 602.9 +0.722 615.605 +0.859 632.54 +0.996 652.072 +1.133 671.418 +1.27 685.671 +1.407 701.286 +1.543 718.069 +1.68 734.116 +1.817 753.292 +1.954 771.589 +2.091 790.453 +2.228 819.222 +2.364 846.663 +2.501 874.629 +2.638 890.083 +2.775 898.271 +2.912 899.312 +3.049 881.683 +3.185 845.157 +3.322 768.451 +3.459 672.771 +3.596 525.466 +3.733 304.694 +3.87 86.663 +3.968 0 +; +;@File: N2800b.txt, @Pts-I: 5383, @Pts-O: 31, @Sm: 8, @CO: 5% +;@TI: 14810.26, @TIa: 14792.71, @TIe: 0.0%, @ThMax: 3650.74, @ThAvg: 2770.17, @Tb: 5.34 +;Exported using ThrustCurveTool, www.ThrustGear.com, by John DeMar +N2800 98 1213 100 7.6947 13.8 AMW +0 93.0947 +0.002 168.347 +0.006 387.836 +0.019 1271.17 +0.029 1776.34 +0.043 2298.6 +0.062 2841.03 +0.072 3021.31 +0.084 3128.89 +0.14 3296.17 +0.277 3483.35 +0.293 3431.67 +0.369 3495.76 +0.978 3598.65 +1.973 3655.16 +2.977 3534.8 +3.3 3437.12 +3.497 3308.46 +3.583 3193.8 +3.651 3015.65 +3.748 2548.37 +3.836 2223.91 +4.109 1644.08 +4.245 1443.68 +4.272 1447.01 +4.397 1163.58 +4.489 1022.95 +4.516 1057.2 +4.574 883.885 +4.647 776.407 +5.569 0 +; +; +G20 29 149 3 0.0729 0.1179 EM +0.0463679 46.6843 +0.278207 30.3888 +0.479134 26.8655 +1.00464 24.6634 +3.47759 22.0209 +4.32767 13.653 +5.11592 3.08293 +5.47 0 +; +;Ellis Mountain G35 Single Use Motor +G35EM 29 165 6-10 0.082 0.135 EM +0.01 51.12 +0.04 57.55 +0.08 43.78 +2.73 28.16 +3.28 28.16 +3.78 6.73 +4 0 +; 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+; +I130 38 330 100 0.308 0.625 EM +0.015456 266.453 +0.0540958 160.753 +0.502318 169.561 +2.23338 180.571 +2.48841 149.742 +2.99073 136.53 +3.49304 77.0732 +4.01082 26.4251 +4.43 0 +; +;Ellis Mountain Rocket Works +;I134 38mm Single Use motor +I134 38 355 15 0.2807 0.5812 EM +0.1 268.8 +0.2 138 +1 116 +2 102 +3 85 +4 67 +4.65 16.46 +4.82 6.86 +5.07 6.86 +5.15 0 +; +; +I150 38 229 20-100 0.1718 0.3983 EM +0 101.15 +0.1 155.94 +0.15 155.94 +0.3 177.01 +0.4 181.23 +0.7 198.09 +0.9 198.09 +1.1 181.23 +1.9 160.15 +2 147.51 +2.1 126.44 +2.3 21.07 +2.4 8.43 +2.67 0 +; +; +I160 38 280 100 0.2319 0.4867 EM +0.01 205.72 +0.01 192.73 +0.2 192.73 +0.4 201.39 +0.5 199.22 +0.75 199.22 +0.76 197.06 +0.95 194.89 +1.5 203.55 +2.2 199.22 +2.35 155.91 +2.4 41.14 +2.7 42.88 +3.25 0 +; +; +I230 38 331 20-100 0.292 0.5751 EM +0 309.64 +0 305.28 +0.1 346.71 +0.15 322.72 +0.5 290.01 +1 283.47 +1.5 270.39 +1.7 252.94 +2 218.05 +2.25 82.86 +2.4 78.5 +2.45 47.97 +2.6 43.61 +2.8 4.36 +2.83 0 +; +; +J110 54 276 100 0.45359 0.8754 EM +0.108192 193.784 +0.386399 147.54 +1.00464 139.833 +4.034 116.711 +5.00773 94.6899 +6.01236 67.1637 +6.53787 37.4355 +6.8 0 +; +; +J148 54 355 14 0.67 1.179 EM +0.139104 218.007 +0.231839 183.875 +0.448223 171.763 +1.00464 170.662 +2.10201 170.662 +5.02318 147.54 +5.31685 133.226 +5.67233 49.547 +6.1 0 +; +; +J228 38 562 6 0.27 0.8391 EM +0.0309119 665.031 +0.0927357 444.822 +0.262751 356.739 +0.664606 343.526 +0.989181 317.101 +1.96291 259.847 +2.99845 193.784 +4.01855 118.913 +4.99227 35.2334 +5.2 0 +; +; +J270 38 384 20-100 0.3471 0.6868 EM +0 308.91 +0.1 419.24 +0.15 441.3 +0.2 397.17 +0.3 375.11 +0.33 353.04 +1.5 330.98 +1.9 286.85 +2 165.49 +2.1 110.33 +2.5 66.19 +2.65 22.07 +2.9 0 +; +; +J330 38 433 20-100 0.4119 0.78 EM +0.05 541.77 +0.07 520.1 +0.2 485.43 +0.5 507.1 +1 455.09 +1.25 433.42 +1.5 379.24 +1.77 216.71 +2 104.02 +2.1 99.69 +2.2 86.68 +2.5 73.68 +2.75 0 +; +; +K475 54 663 14 1.035 2.168 EM +0.0463679 797.157 +0.15456 616.585 +0.278207 585.756 +0.479134 568.139 +2.92117 576.948 +3.29212 568.139 +4.00309 303.888 +4.51314 224.613 +5.02318 74.8711 +5.5 0 +; +; +L330-76mm 76 381 100 1.4899 2.3959 EM +0.05 343 +0.25 381.58 +0.5 362.29 +1 360.15 +2.5 390.16 +3.5 392.3 +6.5 325.85 +7.5 321.56 +7.6 317.27 +8 150.06 +8.5 64.31 +8.9 21.44 +9.35 0 +; +;Ellis Mountain L600 +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +L600 76 584 100 2.4407 4.11981 EM +0.186 829.668 +0.561 773.861 +0.936 767.837 +1.313 755.034 +1.689 736.454 +2.064 722.717 +2.44 706.215 +2.816 688.253 +3.191 673.457 +3.567 660.981 +3.943 648.124 +4.318 634.689 +4.694 622.058 +5.07 607.97 +5.445 594.926 +5.821 583.003 +6.197 573.084 +6.572 553.53 +6.948 399.379 +7.324 270.41 +7.699 211.401 +8.075 144.237 +8.451 74.227 +8.826 19.378 +9.202 4.274 +9.578 0 +; +; +M1000 75 787 100 3.47514 5.5776 EM +0.16 1897.85 +0.48 1606.84 +0.8 1442.25 +1.13 1360.56 +1.45 1300.03 +1.77 1259.95 +2.09 1231.62 +2.41 1203.01 +2.73 1180.44 +3.06 1155.04 +3.38 1109.26 +3.7 1075.88 +4.02 1045.73 +4.34 1010.71 +4.67 951.57 +4.99 860.89 +5.31 727.66 +5.63 595.9 +5.96 519.12 +6.28 440.08 +6.6 347.88 +6.92 239.48 +7.24 144.67 +7.57 75.14 +7.89 33.55 +8.21 0 +; +;The J465GT "Green Tornado" motor is a green flame, low smoke propellant. +;This reload produces a 60% "J" motor with 1023 N-seconds of total impulse, +;maximum thrust of 662.6 Newtons, and an average thrust of 466.9 Newtons, +;for a 2.24 second burn time. +J465GT 54 326 0 0.566 1.1818 GM +0.0475391 200 +0.09 364.9 +0.1 382.7 +0.14 400.5 +0.313199 453.846 +0.53132 515.385 +0.788591 576.923 +1.04306 638.462 +1.16 662.6 +1.27 650 +1.43456 592.308 +1.62192 523.077 +1.82886 423.077 +2 335.78 +2.05 231.4 +2.1 124.6 +2.24 0 +; +;The J365BL "Black Lightning" motor is a black smoke sparky propellant This +;reload produces a 33.2% "J" motor that has 852.4 N-seconds total impulse, +;maximum thrust of 498 Newtons, and an average impulse of 364.9 Newtons for a +;2.38 second burn time. +J365BL 54 326 1000 0.498 1.20454 GM +0.04 102.35 +0.06 155.75 +0.1 192.8 +0.159574 242.308 +0.4 315.95 +0.6 400.5 +0.7 436.1 +0.88 480.6 +1.18 498.4 +1.6 455.6 +1.84564 418.846 +2.05 378.25 +2.14 213.6 +2.2 102.35 +2.3 22.25 +2.38 0 +; +;The J450BL "Black Lightning" motor is a black smoke sparky propellant This +;reload produces a 75% "J" motor that has 1120 N-seconds total impulse, maximum +;thrust of 601 Newtons, and an average impulse of 442.4 Newtons for a 2.57 +;second burn time. +J450BL 54 430 1000 0.658 1.45454 GM +0.08 124.6 +0.130872 215.385 +0.19 333.75 +0.3 413.85 +0.469799 480 +0.68 556.25 +0.8 578.5 +1.05 601 +1.27181 590.769 +1.49329 566.154 +1.68792 535.385 +1.90268 498.35 +2.2 409.4 +2.3 267 +2.4 87.2 +2.57 0 +; +;The K533BL "Black Lightning" motor is a black smoke sparky propellant This +;reload produces a 10% "K" motor that has 1419.75 N-seconds total impulse, +;maximum thrust of 1419.76 Newtons, and an average impulse of 533.45 Newtons +;for a 2.66 second burn time. +K533BL 54 492 1000 0.9 1.7167 GM +0.075 525.1 +0.11745 491.538 +0.15 467.25 +0.228188 484.615 +0.290828 498.462 +0.40604 546.923 +0.530201 616.154 +0.661074 678.462 +0.75 699.56 +1 699.231 +1.19128 692.308 +1.35906 671.538 +1.55369 643.846 +1.87919 581.538 +2.2 493.95 +2.32886 353.077 +2.46644 207.692 +2.65 22.5 +2.7 0 +; +;The K327WC "White Cloud" motor is a white smoke propellant This reload +;produces a 26% "K" motor that has 1615.57 N-seconds total impulse, maximum +;thrust of 684.54 Newtons, and an average impulse of 326.52 Newtons for a 5.18 +;second burn time. +K327WC 54 492 1000 1 1.8167 GM +0.05 556.25 +0.10179 529.231 +0.15 520.65 +0.242729 553.846 +0.375839 603.077 +0.5 658.6 +0.571588 596.923 +0.65 520.65 +1.3311 455.385 +1.79306 412.308 +2.50559 332.308 +2.99888 276.923 +3.47651 227.692 +4.00112 166.154 +4.49441 110.769 +4.92506 61.5385 +5.25 22.25 +5.65 0 +; +;The K222WC "White Cloud" motor is a white smoke propellant This reload +;produces a 2% "K" motor that has 1314.46 N-seconds total impulse, maximum +;thrust of 444.35 Newtons, and an average impulse of 221.56 Newtons for a +;5.937 second burn time. +K222WC 54 430 1000 0.8 1.59654 GM +0.1 396.05 +0.15 378.25 +0.232662 388.462 +0.322148 411.538 +0.4 433.875 +0.456376 400 +0.5 347.1 +0.7 311.5 +1.15 289.25 +1.68233 276.923 +2.25 267 +3 231.4 +3.51678 200 +4 169.1 +4.55481 130.769 +5.18121 88.4615 +5.68233 57.6923 +6.2 22.25 +6.7 0 +; +;The J167WC "White Cloud" motor is a white smoke propellant This reload +;produces a 48% "J" motor that has 949.97 N-seconds total impulse, maximum +;thrust of 366.47 Newtons, and an average impulse of 167.21 Newtons for a +;5.677 second burn time. +J167WC 54 326 1000 0.8 1.2158 GM +0.1 333.75 +0.143177 315 +0.2 307.05 +0.268456 332.308 +0.35 363.66 +0.45 311.5 +0.6 293.7 +1.00224 273.462 +1.50336 249.231 +2.01342 225 +2.56823 197.308 +3.22148 162.692 +4 121.154 +4.53691 90 +5.00224 65.7692 +5.46756 41.5385 +5.85 22.25 +6.25 0 +; +;The K555GT "Green Tornado" motor is a green flame, low smoke propellant. +;This reload produces a 9% "K" motor with 1397 N-seconds of total impulse, +;maximum thrust of 645.3 Newtons, and an average thrust of 556 Newtons, +;for a 2.51 second burn time. +K555GT 54 430 1000 0.78 1.52 GM +0.025 267 +0.05 338.2 +0.1 471.7 +0.12 498.4 +0.15 511.75 +0.18 522.875 +0.2 534 +0.7 631.9 +0.75 636.35 +0.9 645.25 +1.15 636.35 +1.57 623 +1.87 614.1 +2.17 600.75 +2.25 578.5 +2.27 480.6 +2.3 356 +2.35 178 +2.45 66.75 +2.51 0 +; +;The K763GT "Green Tornado" motor is a green flame, low smoke propellant. +;This reload produces a 36% "K" motor with 1740.27 N-seconds of total impulse, +;maximum thrust of 867.75 Newtons, and an average thrust of 763.56 Newtons, +;for a 2.27 second burn time. +K763GT 54 492 1000 0.954 1.81 GM +0.05 498.4 +0.07 565.15 +0.08 623 +0.1 689.75 +0.12 720.9 +0.25 801 +0.38 845.5 +0.65 867.75 +0.83 854.4 +1.95 778.75 +2.1 712 +2.15 400.5 +2.25 44.5 +2.27 0 +; +; +J395RT 54 326 1000 0.5406 1.1604 GM +0.06 267 +0.1 333.75 +0.16 356 +0.21 360.45 +0.33 387.15 +1 460.157 +1.5 453.9 +2.2 409.4 +2.4 360.45 +2.48 267 +2.57 44.5 +2.59 0 +; +; +K520RT 54 430 1000 0.7211 1.4421 GM +0.05 400.5 +0.07 471.7 +0.16 502.85 +0.23 498.4 +0.35 529.55 +0.87 593.13 +1.2 605.2 +1.55 578.5 +1.85 569.6 +2.32 511.75 +2.45 387.15 +2.58 26.7 +2.61 0 +; +; +K470WC 54 728 1000 1.4 2.327 GM +0.025 1001.25 +0.175 905 +0.45 1050.2 +0.65 827.7 +1.091 716.45 +1.633 623 +5.275 0 +; +; +K1075RT 54 728 1000 1.314 2.541 GM +0.017 687.71 +0.042 1026.66 +0.134 1121.18 +0.242 1171.15 +0.325 1203.77 +1.225 1247.2 +1.659 1238.53 +1.742 1223.36 +1.8 1123.36 +2.24 0 +; +; +K700RT 54 492 1000 0.90135 0.17535 GM +0.12 534 +0.18 658.6 +0.2 725.35 +0.24 747.6 +0.28 747.6 +0.4 783.2 +0.65 788.215 +1 787.65 +1.65 769.85 +2 729.8 +2.1 712 +2.2 645.25 +2.38 115.7 +2.41 0 +; +; +K980BL 54 728 1000 1.23 2.457 GM +0.05 1186.45 +0.07 1021.76 +0.25 1135.45 +0.35 1200 +0.5 1225.45 +0.75 1297.45 +0.91 1265.75 +1.1 1201.5 +1.58 1045.75 +1.65 1068 +1.7 1001.25 +1.8 495 +2 222.5 +2.17 0 +; +;HyperTek I310 +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +I310 54 645 0 0.40096 1.30502 HT +0.042 465.886 +0.128 450.815 +0.216 438.421 +0.303 443.241 +0.391 433.808 +0.478 415.992 +0.566 406.746 +0.653 380.383 +0.741 385.17 +0.828 372.458 +0.916 358.282 +1.003 348.621 +1.091 337.887 +1.178 333.898 +1.266 303.469 +1.353 301.589 +1.441 268.788 +1.528 222.719 +1.616 155.314 +1.703 112.163 +1.791 80.51 +1.878 58.562 +1.966 41.774 +2.053 30.243 +2.141 21.27 +2.228 0 +; +;HyperTek J115 (440CC076J) +;Copyright Tripoli Motor Testing 2001 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +J115 54 614 0 0.411264 1.28218 HT +0.129 218.303 +0.391 230.563 +0.653 216.171 +0.916 165.676 +1.178 158.834 +1.441 161.888 +1.703 157.955 +1.966 152.977 +2.228 148.337 +2.491 141.919 +2.753 136.97 +3.016 129.152 +3.278 121.815 +3.541 111.971 +3.803 79.163 +4.066 53.433 +4.328 42.975 +4.591 38.391 +4.853 33.418 +5.116 28.709 +5.378 23.886 +5.641 19.658 +5.903 15.894 +6.166 11.955 +6.428 9.151 +6.691 0 +; +;HyperTek J120 (440CC076JFX) +;Copyright Tripoli Motor Testing 2001 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +J120 54 614 0 0.442176 1.29338 HT +0.134 232.707 +0.405 264.084 +0.676 230.699 +0.948 185.971 +1.22 174.226 +1.491 173.853 +1.763 165.828 +2.034 158.016 +2.305 152.389 +2.577 143.399 +2.849 135.969 +3.12 129.537 +3.392 124.822 +3.664 118.872 +3.934 109.922 +4.206 69.777 +4.478 47.837 +4.749 40.178 +5.021 35.768 +5.293 31.265 +5.564 26.359 +5.835 21.215 +6.107 17.175 +6.378 12.931 +6.65 9.463 +6.922 0 +; +;HyperTek J150 +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +J150 54 645 0 0.428288 1.30592 HT +0.111 177.498 +0.336 193.696 +0.561 200.136 +0.786 204.034 +1.011 200.531 +1.236 197.233 +1.461 192.706 +1.686 189.854 +1.911 185.892 +2.136 183.117 +2.361 179.325 +2.586 174.178 +2.813 171.123 +3.039 164.933 +3.264 160.032 +3.489 154.604 +3.714 148.653 +3.939 92.092 +4.164 55.325 +4.389 42.913 +4.614 32.903 +4.839 24.742 +5.064 16.445 +5.289 8.527 +5.515 4.923 +5.741 0 +; +;HyperTek J170 (440CC098J) +;Copyright Tripoli Motor Testing 2001 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +J170 54 614 0 0.4032 1.28218 HT +0.092 315.198 +0.278 351.486 +0.466 314.152 +0.653 255.278 +0.841 235.396 +1.027 234.785 +1.214 230.871 +1.401 223.051 +1.589 217.688 +1.776 209.94 +1.962 203.806 +2.149 197.52 +2.336 191.243 +2.524 178.598 +2.711 129.785 +2.898 82.459 +3.084 71.693 +3.272 64.633 +3.459 54.015 +3.647 45.022 +3.833 36.373 +4.02 28.397 +4.207 21.518 +4.395 16.072 +4.582 11.712 +4.77 0 +; +;HyperTek J190 (440CC098JFX) +;Copyright Tripoli Motor Testing 2001 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +J190 54 614 0 0.439488 1.29338 HT +0.095 338.583 +0.287 384.416 +0.481 341.472 +0.674 279.175 +0.867 267.528 +1.06 256.325 +1.254 250.108 +1.447 244.404 +1.64 238.846 +1.833 236.505 +2.026 232.026 +2.219 223.962 +2.413 213.236 +2.606 201.661 +2.799 150.523 +2.992 101.327 +3.185 84.001 +3.378 73.902 +3.571 60.222 +3.765 49.208 +3.958 39.096 +4.151 29.873 +4.344 22.6 +4.538 16.842 +4.731 11.964 +4.925 0 +; +;HyperTek J220 +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +J220 54 645 0 0.417984 1.30502 HT +0.071 277.975 +0.215 271.735 +0.358 289.851 +0.502 298.227 +0.647 293.803 +0.792 290.609 +0.935 283.211 +1.079 276.013 +1.223 271.808 +1.368 269.774 +1.513 262.986 +1.656 257.451 +1.8 253.286 +1.944 245.781 +2.089 239.739 +2.233 230.852 +2.377 220.234 +2.521 159.239 +2.665 97.18 +2.809 73.147 +2.954 58.766 +3.098 48.973 +3.242 37.549 +3.385 27.41 +3.53 19.267 +3.675 0 +; +;HyperTek J250 (440CC125J) +;Copyright Tripoli Motor Testing 2001 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +J250 54 614 0 0.40768 1.29248 HT +0.064 409.711 +0.194 453.238 +0.324 416.509 +0.454 383.773 +0.584 359.202 +0.715 343.963 +0.845 336.331 +0.975 328.849 +1.105 318.614 +1.235 309.097 +1.366 306.155 +1.496 290.597 +1.626 283.18 +1.756 261.19 +1.886 200.168 +2.017 143.646 +2.147 126.521 +2.277 113.229 +2.407 91.31 +2.538 71.216 +2.668 54.183 +2.798 40.347 +2.928 29.057 +3.058 20.139 +3.19 13.793 +3.321 0 +; +;HyperTek J270 (440CC125JFX) +;Copyright Tripoli Motor Testing 2001 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +J270 54 614 0 0.419776 1.29606 HT +0.064 438.643 +0.193 498.603 +0.322 468.869 +0.451 438.261 +0.581 412.686 +0.711 390.684 +0.841 376.193 +0.97 362.205 +1.1 347.649 +1.23 333.459 +1.359 324.401 +1.489 311.483 +1.619 298.076 +1.749 278.397 +1.878 220.239 +2.007 150.276 +2.137 125.603 +2.268 121.989 +2.397 91.398 +2.526 71.671 +2.656 55.779 +2.786 41.822 +2.916 30.46 +3.045 22.243 +3.175 16.42 +3.305 0 +; +;HyperTek J317 (835CC172J) +;Copyright Tripoli Motor Testing 2001 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +J317 81 552 0 0.704256 1.7575 HT +0.071 438.483 +0.215 471.024 +0.358 459.716 +0.502 447.348 +0.647 431.653 +0.792 418.545 +0.935 407.806 +1.079 400.212 +1.223 395.752 +1.368 382.516 +1.513 372.89 +1.656 368.033 +1.8 349.298 +1.944 336.071 +2.089 324.486 +2.233 301.205 +2.377 233.601 +2.521 176.972 +2.665 132.539 +2.809 96.229 +2.954 69.718 +3.098 49.457 +3.242 33.983 +3.385 23.063 +3.53 16.524 +3.675 0 +; +;HyperTek J330 (835CC172JFX) +;Copyright Tripoli Motor Testing 2001 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +J330 81 552 0 0.727104 1.77722 HT +0.068 453.5 +0.206 485.741 +0.345 476.873 +0.483 463.622 +0.623 439.951 +0.761 423.26 +0.9 426.386 +1.04 415.245 +1.178 443.371 +1.317 431.352 +1.456 407.015 +1.595 392.143 +1.733 390.332 +1.872 360.092 +2.01 334.24 +2.15 307.215 +2.289 225.611 +2.427 169.224 +2.567 126.562 +2.705 93.167 +2.844 68.293 +2.983 48.099 +3.122 32.856 +3.26 21.857 +3.4 15.193 +3.54 0 +; +;HyperTek K240 +;Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +K240 81 552 0 0.789376 1.80723 HT +0.131 278.007 +0.396 329.552 +0.66 338.024 +0.925 334.092 +1.191 326.199 +1.456 319.745 +1.721 315.195 +1.985 311.182 +2.25 302.916 +2.516 305.943 +2.781 289.975 +3.046 281.781 +3.31 273.33 +3.575 268.852 +3.841 255.702 +4.106 251.068 +4.371 234.82 +4.635 159.972 +4.9 96.543 +5.166 73.367 +5.431 55.477 +5.696 40.928 +5.96 29.542 +6.225 21.25 +6.491 14.787 +6.756 0 +; +;HyperTek L200 (1685CC098L) +;Copyright Tripoli Motor Testing 2001 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +L200 111 724 0 1.59398 3.89491 HT +0.292 310.935 +0.877 311.934 +1.464 284.574 +2.05 259.236 +2.636 245.149 +3.223 240.798 +3.809 246.021 +4.396 251.509 +4.981 255.559 +5.568 250.045 +6.154 242.343 +6.741 236.221 +7.327 230.527 +7.914 224.062 +8.5 218.24 +9.086 212.215 +9.673 189.706 +10.258 94.608 +10.845 67.128 +11.431 53.35 +12.018 41.55 +12.604 31.112 +13.191 22.445 +13.777 16.763 +14.364 10.892 +14.95 0 +; +;HyperTek L225 (1685CC098LFX) +;Copyright Tripoli Motor Testing 2001 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +L225 111 724 0 1.66118 3.94822 HT +0.271 380.609 +0.815 364.078 +1.359 347.671 +1.904 311.98 +2.449 292.842 +2.994 284.62 +3.539 284.123 +4.083 295.754 +4.628 286.654 +5.173 271.822 +5.718 258.225 +6.263 249.357 +6.807 240.396 +7.352 232.666 +7.897 226.844 +8.442 217.601 +8.986 208.639 +9.531 122.739 +10.076 74.667 +10.621 60.93 +11.166 48.898 +11.71 38.996 +12.255 29.719 +12.8 21.925 +13.345 16.36 +13.89 0 +; +;HyperTek L350 (1685CC125L) +;Copyright Tripoli Motor Testing 2001 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +L350 111 724 0 1.6025 3.90342 HT +0.188 592.182 +0.566 598.015 +0.945 479.774 +1.324 427.223 +1.702 406.561 +2.08 395.128 +2.459 393.279 +2.839 410.729 +3.217 517.335 +3.595 506.496 +3.974 439.49 +4.353 391.732 +4.731 463.388 +5.109 446.876 +5.489 436.237 +5.868 387.456 +6.246 247.342 +6.624 147.845 +7.003 117.459 +7.382 93.081 +7.76 73.034 +8.139 55.605 +8.518 40.854 +8.897 29.575 +9.276 21.627 +9.655 0 +; +;HyperTek L355 (1685CC125LFX) +;Copyright Tripoli Motor Testing 2001 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +L355 111 724 0 1.61952 3.95405 HT +0.185 638.681 +0.559 623.792 +0.933 538.081 +1.307 493.173 +1.682 465.144 +2.056 432.702 +2.43 410.644 +2.804 388.862 +3.178 395.452 +3.553 384.851 +3.927 370.103 +4.301 356.484 +4.675 346.195 +5.049 342.684 +5.424 325.43 +5.798 317.798 +6.172 272.453 +6.546 156.214 +6.92 117.579 +7.295 93.203 +7.669 73.056 +8.043 56.997 +8.417 42.994 +8.791 30.338 +9.166 21.725 +9.541 0 +; +;HyperTek L475 (1685CC172L) +;Copyright Tripoli Motor Testing 2001 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +L475 111 724 0 1.52992 3.89805 HT +0.129 640.755 +0.391 638.069 +0.652 619.018 +0.914 609.661 +1.176 597.937 +1.437 596.251 +1.699 594.039 +1.961 572.245 +2.223 578.304 +2.484 589.224 +2.747 578.752 +3.008 612.426 +3.27 646.188 +3.531 674.617 +3.793 652.574 +4.055 555.384 +4.317 299.749 +4.578 220.284 +4.841 170.007 +5.102 127.011 +5.364 94.998 +5.626 70.208 +5.888 49.458 +6.149 32.102 +6.411 18.382 +6.674 0 +; +;HyperTek L535 (1685CC172LFX) +;Copyright Tripoli Motor Testing 2001 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +L535 111 724 0 1.59667 3.94822 HT +0.119 838.518 +0.358 768.667 +0.598 727.551 +0.838 745.172 +1.077 712.851 +1.317 694.613 +1.556 672.145 +1.796 656.726 +2.035 685.07 +2.275 808.735 +2.515 798.521 +2.754 755.277 +2.995 726.985 +3.235 699.331 +3.475 670.049 +3.715 515.315 +3.954 293.947 +4.194 227.905 +4.433 180.167 +4.673 140.714 +4.912 107.564 +5.152 80.907 +5.392 58.898 +5.631 39.782 +5.872 24.901 +6.113 0 +; +;HyperTek L540 (2800CC172L) +;Copyright Tripoli Motor Testing 2001 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +L540 111 876 0 2.5303 5.656 HT +0.191 685.548 +0.574 665.171 +0.957 635.467 +1.341 634.122 +1.725 656.225 +2.109 706.931 +2.493 696.526 +2.876 777.726 +3.26 775.919 +3.645 781.611 +4.028 712.736 +4.411 695.555 +4.796 701.251 +5.18 645.985 +5.564 607.757 +5.947 546.408 +6.331 387.372 +6.716 234.214 +7.099 181.086 +7.482 139.253 +7.867 106.109 +8.251 78.293 +8.634 54.851 +9.018 36.384 +9.402 20.375 +9.786 0 +; +;HyperTek L550 (1685CCRGL) +;Copyright Tripoli Motor Testing 2001 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +L550 111 724 0 1.53261 3.89805 HT +0.124 816.849 +0.375 796.043 +0.626 781.861 +0.877 767.44 +1.129 759.627 +1.38 735.948 +1.631 714.454 +1.883 701.582 +2.134 674.667 +2.385 656.493 +2.637 636.076 +2.889 612.409 +3.14 587.801 +3.391 567.17 +3.642 559.971 +3.894 534.157 +4.145 444.562 +4.396 280.51 +4.648 216.702 +4.899 163.136 +5.15 120.571 +5.402 86.544 +5.653 59.99 +5.904 39.527 +6.156 25.914 +6.408 0 +; +;HyperTek L570 (2800CC172LFX) +;Copyright Tripoli Motor Testing 2001 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +L570 111 876 0 2.57734 5.70618 HT +0.181 793.916 +0.547 800.029 +0.914 811.765 +1.28 761.283 +1.647 725.674 +2.014 733.246 +2.38 783.159 +2.747 795.348 +3.112 823.178 +3.478 831.812 +3.845 805.614 +4.211 780.534 +4.578 741.917 +4.945 628.98 +5.311 547.886 +5.678 537.83 +6.044 330.85 +6.409 230.792 +6.776 180.51 +7.143 140.226 +7.509 108.348 +7.876 81.342 +8.243 59.608 +8.609 41.592 +8.976 25.536 +9.343 0 +; +;HyperTek L575 (2800CCRGL) +;Copyright Tripoli Motor Testing 2001 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +L575 111 876 0 2.52134 5.65286 HT +0.19 705.343 +0.572 723.437 +0.955 738.414 +1.337 749.383 +1.72 735.169 +2.103 725.088 +2.486 733.751 +2.869 700.454 +3.251 690.771 +3.634 682.897 +4.017 674.825 +4.399 687.463 +4.782 675.411 +5.166 645.685 +5.548 643.612 +5.93 634.693 +6.314 559.731 +6.696 304.009 +7.078 229.423 +7.461 167.643 +7.845 121.036 +8.227 83.673 +8.609 54.311 +8.993 33.029 +9.376 19.886 +9.759 0 +; +;HyperTek L610 (1685CCRGLFX) +;Copyright Tripoli Motor Testing 2001 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +L610 111 724 0 1.57696 3.95091 HT +0.11 850.823 +0.333 837.7 +0.556 775.061 +0.779 739.656 +1.002 807.273 +1.225 809.462 +1.448 801.752 +1.671 789.534 +1.894 763.842 +2.117 858.087 +2.34 890.644 +2.563 837.593 +2.785 749.631 +3.008 648.961 +3.231 643.064 +3.454 637.413 +3.677 431.325 +3.9 276.205 +4.123 220.93 +4.346 166.632 +4.569 124.031 +4.792 89.721 +5.015 64.295 +5.237 45.36 +5.461 30.4 +5.685 0 +; +;HyperTek L625 (2800CCRGLFX) +;Copyright Tripoli Motor Testing 2001 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +L625 111 876 0 2.56614 5.70618 HT +0.169 855.024 +0.509 896.169 +0.851 905.926 +1.193 902.118 +1.534 853.016 +1.876 953.21 +2.218 904.246 +2.559 856.525 +2.901 743.522 +3.243 758.646 +3.584 751.619 +3.926 745.737 +4.267 751.907 +4.607 728.305 +4.949 691.703 +5.291 658.843 +5.632 504.45 +5.974 279.745 +6.316 216.661 +6.657 164.957 +6.999 123.426 +7.341 89.428 +7.682 62.955 +8.024 43.519 +8.366 27.956 +8.707 0 +; +;Data entered by Tim Van Milligan +;Based on TRA Certification 6-19-2002 +;And Instructions provided by Aerotech. +I170S 38 258 14 0.1819 0.52 KBA +0.019 194.885 +0.131 190.481 +0.255 191.582 +0.513 199.289 +0.641 204.794 +0.753 206.996 +0.88 209.199 +1 208.098 +1.051 208.098 +1.147 206.996 +1.24 201.491 +1.391 198.188 +1.537 190.481 +1.707 181.672 +1.746 178.369 +1.781 173.96 +1.808 168.46 +1.854 132.12 +1.939 53.951 +2.005 22.02 +2.059 9.909 +2.13 0 +; +; +I280F 38 258 14 0.182 0.52 KBA +0.009 253.24 +0.055 255.442 +0.219 277.463 +0.482 301.686 +0.67 323.707 +0.735 330.314 +0.797 323.707 +1.001 297.282 +1.162 266.453 +1.205 259.847 +1.236 237.826 +1.363 50.6481 +1.428 26.4251 +1.5 0 +; +;Kosdon by AeroTech I310S +;Copyright Tripoli Motor Testing 2001 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +I310S 38 368 100 0.312256 0.713216 KBA +0.045 334.66 +0.136 314.409 +0.228 322.556 +0.32 326.871 +0.411 331.851 +0.503 335.911 +0.595 336.933 +0.686 340.151 +0.778 342.066 +0.87 344.722 +0.961 348.578 +1.053 349.548 +1.146 351.943 +1.239 347.939 +1.33 345.079 +1.422 337.035 +1.514 333.332 +1.605 323.832 +1.697 289 +1.789 215.097 +1.88 136.596 +1.972 83.863 +2.064 37.922 +2.155 20.736 +2.248 5.943 +2.341 0 +; +;Kosdon by AeroTech I370F +;Copyright Tripoli Motor Testing 2001 (www.tripoli.org) +;provided by ThrustCurve.org (www.thrustcurve.org) +I370F 38 368 100 0.312256 0.705152 KBA +0.035 373.074 +0.109 389.927 +0.184 401.07 +0.259 416.613 +0.334 429.598 +0.409 438.025 +0.484 443.83 +0.559 447.326 +0.634 446.764 +0.709 447.263 +0.784 444.735 +0.859 441.302 +0.933 435.676 +1.007 425.29 +1.082 414.897 +1.157 404.222 +1.232 395.358 +1.307 382.062 +1.382 334.152 +1.457 275.974 +1.532 179.654 +1.607 83.023 +1.682 39.608 +1.757 16.105 +1.832 4.151 +1.907 0 +; +; +I450F 38 370 14 0.3032 0.73 KBA +0.012 634.202 +0.037 550.523 +0.108 519.693 +0.241 510.885 +0.639 550.523 +0.729 554.927 +0.809 546.118 +0.939 497.672 +1.072 471.247 +1.128 440.418 +1.165 387.568 +1.211 206.996 +1.295 88.0836 +1.36 26.4251 +1.41 0 +; +; +J405S 38 476 14 0.367 0.88 KBA +0.009 528.502 +0.024 488.864 +0.046 462.439 +0.136 462.439 +0.268 458.035 +0.986 453.631 +1.421 444.822 +1.523 255.442 +1.697 92.4878 +1.93 0 +; +; +J605F 38 476 14-100 0.367 0.88 KBA +0.024 886.341 +0.037 704.669 +0.077 660.627 +0.438 704.669 +0.506 715.679 +0.59 710.174 +0.853 655.122 +0.973 594.564 +1.041 412.892 +1.091 324.808 +1.177 132.125 +1.3 0 +; +; +K400S 54 403 6-10-14 0.713216 1.50931 KBA +0.074 465.928 +0.225 441.922 +0.377 442.414 +0.529 445.492 +0.681 449.048 +0.833 451.88 +0.985 454.481 +1.138 456.929 +1.29 458.237 +1.442 457.021 +1.594 455.62 +1.746 451.772 +1.897 446.421 +2.048 438.843 +2.2 429.377 +2.352 419.003 +2.504 408.274 +2.656 397.608 +2.808 388.018 +2.96 367.07 +3.113 263.666 +3.265 114.378 +3.417 46.238 +3.569 8.62 +3.721 2.401 +3.873 0 +; +; +K600F 54 403 6-10-14-100 0.68096 1.41568 KBA +0.045 639.654 +0.148 711.292 +0.252 695.617 +0.358 696.252 +0.462 701.336 +0.568 703.242 +0.67 705.265 +0.772 704.302 +0.878 702.819 +0.982 701.336 +1.088 696.888 +1.192 689.262 +1.295 681.245 +1.398 668.928 +1.502 653.465 +1.608 637.366 +1.712 619.785 +1.818 599.451 +1.92 586.275 +2.022 510.698 +2.128 334.676 +2.232 125.397 +2.338 37.916 +2.442 17.157 +2.548 4.025 +2.653 0 +; +; +L1000S 54 727.96 100 1.301 1.248 KBA +0.038 1310.24 +0.085 1090.03 +0.139 1023.97 +0.216 1001.95 +0.479 979.93 +1.035 1112.06 +1.993 1244.18 +2.047 1222.16 +2.094 1189.13 +2.179 924.878 +2.233 737.7 +2.264 847.805 +2.295 682.648 +2.295 539.512 +2.302 649.617 +2.318 451.428 +2.7 0 +; +; +L1400F 54 727 14-100 1.248 2.502 KBA +0.037 1541.46 +0.061 1453.38 +0.166 1354.29 +1.001 1772.68 +1.279 1783.69 +1.329 1882.79 +1.387 1992.89 +1.486 1387.32 +1.604 869.826 +1.65 748.711 +1.666 726.69 +1.69 924.878 +1.697 594.564 +1.758 319.303 +1.88 0 +; +; +J528-LW 38 406 5-8-10-13-17 0.372 0.752 LR +0.01 704.2 +0.02 1019 +0.03 983.9 +0.05 881.1 +0.1 797.5 +0.15 771.7 +0.17 765.72 +0.21 765.72 +0.25 778.2 +0.42 789.28 +0.51 771.61 +0.6 756.89 +0.66 751 +0.71 762.78 +0.76 697.99 +0.8 665.59 +0.84 612.58 +0.92 488.88 +0.95 385.81 +1.02 282.73 +1.06 179.65 +1.14 53.01 +1.19 35.34 +1.23 32.2 +1.25 0 +; +; +I405-LW 38 292 5-8-10-13-17 0.24 0.54 LR +0.01 151.1 +0.03 781.4 +0.05 800.7 +0.06 755.7 +0.09 724.3 +0.12 697.7 +0.15 701 +0.17 675.3 +0.2 643.1 +0.3 607.7 +0.4 569.2 +0.5 517.7 +0.6 472.7 +0.7 392.3 +0.8 318.3 +0.9 241.2 +1 151.1 +1.1 93.3 +1.15 40 +1.2 0 +; +; +H144-LW 38 178 5-8-10-13-17 0.12 0.335 LR +0.02 209 +0.04 247.6 +0.05 241.2 +0.1 247.6 +0.15 244.4 +0.2 237.9 +0.25 231.54 +0.3 228.3 +0.4 215.32 +0.45 212.43 +0.5 204.48 +0.6 194.36 +0.7 189.7 +0.8 170.4 +0.9 154.3 +1 127.83 +1.1 109.3 +1.2 80.4 +1.3 64.6 +1.4 44.6 +1.5 32.1 +1.6 0 +; +; +J175-LW 54 327 0 0.59 1.264 LR +0.01 4.8 +0.1 420.4 +0.2 347.5 +0.3 349.9 +0.4 364.5 +0.5 320.7 +1 296.4 +1.5 279.4 +2 260 +2.5 238.1 +3 209 +3.5 172 +4 133.6 +4.5 102 +5 75.3 +5.5 46.2 +6 17 +6.5 0 +; +; +J525-LW 54 327 0 0.59 1.264 LR +0.01 210.9 +0.03 499.3 +0.05 628.5 +0.1 594 +0.13 568.2 +0.15 559.6 +0.2 555.3 +0.3 572.5 +0.4 589.7 +0.5 606.9 +0.6 624.2 +0.7 637.1 +0.8 645.7 +0.9 650 +1 658.6 +1.1 637.1 +1.2 628.5 +1.3 615.5 +1.41 586.27 +1.52 561.52 +1.67 536.78 +1.78 517.74 +1.85 485.38 +1.92 91.37 +2 0 +; +; +J820-LW 54 327 0 0.57 1.244 LR +0.01 4.8 +0.02 982.43 +0.07 1033.1 +0.11 982.43 +0.2 959.9 +0.3 943.02 +0.4 947 +0.5 972.8 +0.6 981.4 +0.7 990 +0.8 990 +0.9 981.4 +0.95 1033.1 +1 981.4 +1.1 641.4 +1.2 353 +1.3 206.6 +1.4 120.5 +1.5 0 +; +; +M1882-LW 76 785 0 3.12979 5.53383 LR +0.01 4.8 +0.0174014 2579.22 +0.0696056 2392.32 +0.232019 2298.87 +0.50464 2261.49 +0.771462 2298.87 +0.986079 2411.01 +1.1891 2579.22 +1.49652 2597.91 +1.72854 2485.77 +2.00116 2354.94 +2.5 1644.72 +2.99884 242.97 +3.25 0 +; +; +I110-LW 38 292 5-8-12 0.289 0.589 LR +0 282.365 +0.0348028 218.735 +0.12181 170.944 +0.214617 163.592 +0.400232 169.106 +1.50232 176.458 +2.00116 152.563 +2.5 108.448 +2.99884 64.3338 +4 0 +; +; +L1400-LW 54 726 0 1.4 2.54 LR +0.00580046 1606.3 +0.11891 1535.7 +0.327726 1535.7 +0.49884 1588.65 +1.00058 1782.82 +1.40661 1906.38 +1.49942 1376.83 +1.60673 953.19 +1.74594 547.202 +1.90545 335.382 +1.99826 211.82 +2 0 +; +; +L930-LW 76 498 0 1.81437 3.53802 LR +0.025 532 +0.05 1123 +0.075 1123 +0.125 1094 +0.2 930 +0.5 881 +0.6 878 +0.75 898 +1 921 +1.25 940 +1.5 1012 +1.75 1081 +2 1100 +2.25 1120 +2.5 1051 +2.75 980 +3 934 +3.25 826 +3.5 722 +3.75 280 +4 0 +; +; +K350-LW 54 702 0 1.4 2.54012 LR +0.025 1329 +0.0375 1061 +0.1 1006 +0.15 891 +0.2 768 +0.4 571 +0.5 542 +0.75 486 +1 486 +1.25 477 +1.5 481 +2.5058 460 +3.00464 427 +3.5 375 +4 333 +4.5 297 +5 249 +5.5 210 +6 164 +6.5 98 +7 0 +; +; +K250-LW 54 498 0 0.952544 1.79169 LR +0.03 800 +0.1 682 +0.125 574 +0.15 476 +0.175 447 +0.25 385 +0.45 340 +0.6 320 +1 313 +1.5 300 +2 297 +2.5 303 +3 294 +3.5 287 +4 248 +4.5 222 +5 187 +5.5 147 +6 114 +6.5 62 +7 0 +; +; +K960-LW 54 498 0 0.929864 1.74633 LR +0.03 1210 +0.05 1512 +0.075 1535 +0.1 1502 +0.125 1437 +0.2 1237 +0.3 1175 +0.5 1139 +0.6 1130 +0.7 1156 +0.8 1182 +0.9 1192 +1 1166 +1.1 1139 +1.2 1101 +1.3 1091 +1.4 1026 +1.5 839 +1.6 790 +1.7 575 +1.8 284 +1.9 150 +2 0 +; +; +H500-LW 38 292 5-7-9-12-15 0.16 0.454 LR +0.001 189.286 +0.0116009 534.733 +0.099768 539.465 +0.199536 544.197 +0.302784 553.662 +0.402552 548.93 +0.50464 544.197 +0.584687 435.358 +0.61949 9.4643 +0.62 0 +; +; +H100-SP 38 178 5-8-10-13-17 0.12 0.335 LR +0.015528 127.586 +0.151398 127.586 +0.477484 139.655 +0.74146 146.552 +1.00543 150 +1.13742 122.414 +1.30823 86.2069 +1.59938 39.6552 +2 0 +; +; +I316-SP 38 292 5-8-10-13-17 0.24 0.54 LR +0.00931677 448.276 +0.127329 491.379 +0.242236 500 +0.347826 482.759 +0.484472 439.655 +1 258.621 +1.5 0 +; +; +J396-SP 38 406 5-8-10-13-17 0.372 0.752 LR +0.00621118 396.552 +0.201863 413.793 +0.400621 439.655 +0.593168 491.379 +0.717391 543.103 +0.801242 508.621 +0.993789 491.379 +1.20186 448.276 +1.40062 250 +1.6 0 +; +H90-LR 38 178 5-8-10-14 0.12 0.335 LR +0.0543478 146.552 +1.51398 94.8276 +2.1972 44.8276 +2.6087 0 +; +; +I210-LR 38 292 5-8-10-14 0.24 0.54 LR +0.00388199 452.586 +0.0427019 387.931 +1.00155 271.552 +1.80901 77.5862 +2.3 0 +; +; +J320-LR 38 406 5-8-10-14 0.372 0.752 LR +0.015528 534.031 +0.100932 439.791 +1.94099 319.372 +2.18944 78.534 +2.6 0 +; +; +G80-LW 38 127 5-8-10-13-17 0.06 0.275 LR +0.00931677 112.069 +0.416149 112.069 +0.872671 89.6552 +1.5 0 +; +; +J712-LB 38 406 7-9-12-15 0.372 0.752 LR +0.00931677 870.69 +0.0496894 810.345 +0.791925 793.103 +1 706.897 +1.06211 172.414 +1.2 0 +; +; +H160-LB 38 178 7-9-12-15 0.12 0.335 LR +0.015528 288.793 +0.599379 237.069 +1.03106 107.759 +1.5 0 +; +; +I430-LB 38 292 7-9-12-15 0.24 0.54 LR +0.00931677 534.483 +0.0310559 448.276 +0.0962733 465.517 +0.372671 456.897 +0.748447 439.655 +1.14907 422.414 +1.2 0 +; +; +L1482 76 498 0 1.814 3.538 LR +0.00776398 1344.83 +0.0465839 1241.38 +0.48913 1551.72 +1.01708 1568.97 +1.99534 1603.45 +2.3913 1586.21 +2.48447 1758.62 +2.50776 103.448 +2.6 0 +; +; +M2550 76 785 0 3.13 5.53 LR +0.00776398 2974.14 +0.0621118 2887.93 +0.427019 2887.93 +0.861801 3017.24 +1.49845 2974.14 +2.11957 2413.79 +2.45342 474.138 +2.6 0 +; +; +F50T 29 98 4-6-9 0.0379 0.0849 AT +0.01 37.97 +0.02 56.27 +0.03 65.08 +0.12 71.86 +0.23 75.25 +0.33 77.29 +0.35 77.7 +0.45 75.25 +0.59 71.86 +0.72 65.76 +0.83 58.98 +1.01 43.39 +1.19 25.76 +1.25 15.59 +1.3 8.81 +1.36 4.75 +1.42 0 +; +;PML G40W is the same as the Aerotech G40W. +G40W 29 124 4-7-10 0.0624 0.115 PML +0.015 40 +0.037 66.479 +0.066 60.845 +0.161 55.775 +0.308 55.775 +0.447 54.085 +0.549 52.394 +0.637 51.268 +0.857 52.958 +1.018 52.394 +1.172 50.141 +1.362 46.761 +1.611 41.69 +1.691 41.127 +1.845 34.366 +1.999 30.423 +2.372 23.099 +2.585 13.521 +2.738 6.761 +3.039 0 +; +;PML G80T is the same as the old Aerotech G80T. +G80T 29 124 4-7-10 0.0574 0.106 PML +0.007 82.746 +0.018 104.754 +0.051 104.754 +0.095 97.711 +0.245 94.19 +0.458 95.07 +0.6 93.31 +0.86 84.507 +1.003 76.585 +1.139 69.542 +1.252 57.218 +1.303 51.056 +1.34 37.852 +1.38 19.366 +1.424 7.923 +1.461 2.641 +1.497 0 +; +;Ace Aeronautics L500 (Historical) +;Kline-Rogers +;"D" Grain Motor +L500 54 1016 0 1.53638 2.61184 Hist +0 733.957 +0.5 782.887 +1 800.68 +1.5 796.232 +2 760.646 +2.5 702.819 +3 631.648 +3.5 538.235 +4 440.374 +4.5 333.617 +5 226.859 +6 35.586 +6.23 0 +; +;Aerotech J100 (Historical) +;Old single-use Aerotech J100 +;delays: 5/10/15 +J100 54 251 0 0.445 0.8 Hist +0 187.804 +0.11 160.981 +0.3 144.879 +0.6 136.783 +2.2 128.776 +4 109.96 +8.2 29.492 +10.8 0 +; +;Aerotech J125 (Historical) +;Old single-use Aerotech J125 +J125 54 334 0 0.001644 0.002425 Hist +0.02 212.091 +0.07 238.87 +0.24 224.546 +0.49 221.655 +0.71 224.546 +0.98 228.372 +1.17 235.044 +1.95 233.131 +2.25 223.568 +2.68 212.091 +3.19 193.943 +3.59 178.641 +4.03 162.405 +4.46 142.388 +5.25 110.85 +5.8 87.897 +6.34 66.857 +6.88 52.578 +7.56 37.276 +8 33.451 +8.44 24.866 +8.98 18.149 +9.31 11.476 +9.46 5.738 +9.61 5.738 +9.8 0 +; +;Kosdon O10000 (Historical) +O10000 98 1651 0 11.34 16.840 Hist +0.01 6844.983 +2.27 12127.03 +2.28 0.0 +; +;Animal Motor Works 38-640 +J440BB 38 369 20 0.3853 0.6985 AMW +0.007 468.505 +0.022 509.996 +0.037 527.687 +0.052 532.792 +0.082 530.181 +0.127 525.586 +0.202 521.566 +0.277 519.840 +0.352 521.522 +0.426 525.414 +0.501 531.248 +0.576 538.724 +0.651 541.761 +0.726 538.508 +0.801 531.072 +0.876 516.175 +0.950 494.942 +1.025 477.251 +1.100 433.297 +1.175 313.900 +1.250 187.467 +1.325 101.546 +1.400 45.751 +1.474 22.083 +1.497 0.000 +; +;Animal Motor Works K475 RASP.ENG file made from NAR data +;File produced Feb 22, 2003 +;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. +K475WW 54 403 100 0.7286 1.4925 AMW +0.022 127.831 +0.041 386.016 +0.063 548.326 +0.096 521.308 +0.134 499.129 +0.18 486.83 +0.285 486.83 +0.478 501.649 +0.731 523.727 +1.096 553.266 +1.433 577.962 +1.601 588.29 +1.756 582.704 +1.895 580.284 +1.958 575.344 +2.063 550.746 +2.209 518.788 +2.344 477.051 +2.495 417.974 +2.561 354.058 +2.582 334.399 +2.599 331.98 +2.62 297.501 +2.67 226.226 +2.707 157.37 +2.74 98.353 +2.799 49.176 +2.853 17.208 +2.94 0 +; +; Entered by Tim Van Milligan. Used John Coker's ThrustCurve Tracer software and +; data from NAR certification dated May 7, 2007 +K500SK 75 368 100 1.1235 2.713 AMW + 0.018 194.373 + 0.031 207.161 + 0.036 268.542 + 0.103 319.693 + 0.138 322.251 + 0.17 314.578 + 0.67 309.463 + 0.692 322.251 + 0.902 319.693 + 0.929 332.481 + 1.263 355.499 + 1.585 383.632 + 1.969 411.765 + 2.112 416.88 + 2.272 447.57 + 2.415 488.491 + 2.46 485.934 + 2.634 534.527 + 2.83 618.926 + 3.018 710.997 + 3.143 767.263 + 3.228 815.857 + 3.339 841.432 + 3.402 826.087 + 3.504 785.166 + 3.585 718.67 + 3.661 631.714 + 3.728 519.182 + 3.772 365.729 + 3.826 181.586 + 3.862 99.744 + 3.893 43.478 + 3.946 0.0 +; +;Animal Motor Works 54-1400 +;AMW K530GG RASP.ENG file made from NAR data +;File produced Feb 25, 2003 +;This file my be used or given away. All I ask is that this header +;is maintained to give credit to NAR S&T. Thank you, Jack Kane +;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. +K530GG 54 403 1000 0.7967 1.616 AMW +0.013 129.764 +0.054 171.852 +0.096 284.122 +0.138 392.892 +0.171 455.975 +0.217 501.662 +0.238 498.063 +0.326 508.66 +0.542 564.745 +0.755 613.831 +1.01 645.423 +1.17 657.23 +1.273 648.922 +1.51 638.425 +1.656 634.925 +1.702 606.833 +1.803 606.833 +1.857 585.839 +1.936 589.338 +1.974 575.242 +2.015 589.338 +2.04 564.745 +2.132 536.652 +2.207 540.251 +2.291 522.656 +2.357 487.566 +2.42 375.297 +2.478 242.033 +2.529 140.361 +2.583 66.651 +2.66 0 +; +; Blue Baboon +K1130-BB 54 728 0 1.359 2.574 AMW/ProX +0.01 1000 +0.013 1490 +0.02 1548 +0.04 1500 +0.09 1335 +0.2 1325 +1 1325 +1.5 1325 +1.63 1345 +1.7 1155 +1.8 805 +1.9 685 +2 475 +2.1 315 +2.2 145 +2.3 0 +; +K1250-WW 54 491 0 0.925 1.815 AMW/ProX +0.01 600 +0.02 1400 +0.03 1610 +0.05 1360 +0.07 1410 +0.1 1440 +0.15 1470 +0.2 1480 +0.4 1480 +0.8 1395 +1.28 1185 +1.36 985 +1.4 680 +1.45 570 +1.5 210 +1.6 60 +1.7 0 +; +; Skidmark +K610-SK 54 491 0 0.866 1.765 AMW/ProX +0.01 300 +0.02 745 +0.035 650 +0.06 560 +0.12 635 +0.21 670 +0.4 695 +0.7 700 +1 690 +1.35 665 +1.7 630 +2.05 585 +2.19 590 +2.24 500 +2.3 350 +2.4 205 +2.5 60 +2.6 15 +2.7 0 +; +K710-BB 54 491 0 0.902 1.812 AMW/ProX +0.01 500 +0.02 850 +0.025 910 +0.03 840 +0.06 860 +0.12 875 +0.2 875 +0.3 872 +1.1 815 +1.85 740 +1.95 720 +2.2 295 +2.37 280 +2.5 90 +2.6 20 +2.8 0 +; AMX/ProX 2729L1276 RR +L1276RR 54 728 P 1.475 2.96 AMW + 0.015 76.924 + 0.017 692.317 + 0.026 1495.003 + 0.037 1244.164 + 0.052 1401.357 + 0.084 1307.71 + 0.127 1307.71 + 0.181 1367.911 + 0.289 1401.357 + 0.384 1408.046 + 0.807 1421.424 + 0.993 1461.558 + 1.215 1491.659 + 1.673 1474.936 + 1.727 1384.634 + 1.798 1083.627 + 1.947 531.78 + 1.986 351.175 + 2.047 177.26 + 2.092 93.647 + 2.144 33.445 + 2.185 0.0 +; +;@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 +E20 24 65 4-7-10 0.0162 0.049 AT +0 0.0290422 +0.024 0.227567 +0.038 1.39403 +0.048 2.6721 +0.056 5.81661 +0.06 7.76916 +0.062 9.00446 +0.064 10.7176 +0.072 20.3365 +0.074 22.4147 +0.08 27.1311 +0.084 28.9874 +0.09 30.5394 +0.104 32.9513 +0.124 34.2647 +0.138 34.677 +0.252 33.8465 +0.36 32.0816 +0.63 29.8124 +0.672 28.8301 +0.77 27.3596 +0.8 26.3903 +0.9 24.2069 +1.084 18.0681 +1.134 16.8918 +1.16 15.8701 +1.2899 12.1921 +1.3719 9.38065 +1.5079 4.03928 +1.5519 2.72185 +1.6019 1.72082 +1.7579 0 +; +; From AT Instruction Sheet by C. Kobel 1/4/11 +F30FJ 24 90 4-6-8 0.0318 0.070 AT + 0.056 22.706 + 0.102 34.315 + 0.134 36.363 + 0.200 36.876 + 0.300 36.705 + 0.400 37.217 + 0.500 38.241 + 0.600 37.900 + 0.700 37.900 + 0.800 37.217 + 0.900 36.363 + 1.000 35.168 + 1.100 33.291 + 1.175 32.608 + 1.200 31.413 + 1.260 26.974 + 1.300 22.706 + 1.400 9.219 + 1.453 5.805 + 1.500 4.097 + 1.600 0.0 +; +; AeroTech G138T +; from the reload instruction sheet 08/11/2010 +; Created by Scott Sager 10/10/2010 +G138T 29 123.8 14 0.0704 0.152 AT + 0.0020 113.497 + 0.043 118.736 + 0.098 125.065 + 0.138 126.157 + 0.198 133.578 + 0.251 140.999 + 0.293 146.019 + 0.347 148.856 + 0.398 156.932 + 0.447 160.861 + 0.5 165.881 + 0.548 169.591 + 0.601 173.738 + 0.646 177.449 + 0.697 183.123 + 0.739 182.032 + 0.798 182.469 + 0.839 181.159 + 0.901 182.469 + 0.947 194.691 + 0.972 185.306 + 0.986 174.611 + 0.998 161.515 + 1.0 156.714 + 1.012 143.618 + 1.018 133.796 + 1.026 120.263 + 1.031 111.969 + 1.036 98.437 + 1.041 89.052 + 1.044 77.484 + 1.049 67.662 + 1.054 54.784 + 1.059 46.708 + 1.064 33.176 + 1.073 23.136 + 1.082 12.659 + 1.098 0.873 + 1.099 0.0 +; +; @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 +G142 29 113 6-10-14 0.0386 0.0976 AT + 0.016 4.06052 + 0.018 6.53754 + 0.02 13.44075 + 0.022 24.4211 + 0.024 43.7388 + 0.026 72.8495 + 0.028 106.9426 + 0.03 132.0076 + 0.032 141.5423 + 0.034 147.6844 + 0.038 154.1148 + 0.054 165.5675 + 0.076 166.3214 + 0.084 168.7605 + 0.118 172.9402 + 0.15 173.3837 + 0.224 171.8426 + 0.3 164.7803 + 0.372 156.6537 + 0.418 148.9594 + 0.432 144.9903 + 0.452 137.0965 + 0.518 96.8779 + 0.568 69.3937 + 0.576 63.1618 + 0.618 21.4754 + 0.628 13.57047 + 0.64 7.98504 + 0.652 2.92169 + 0.672 0.966347 + 0.9 0.687625 + 0.901 0 +; +; Curve fit of AT Instruction sheet by C. Kobel 7/29/08 +G76G 29 124 4-7-10 0.06 0.147 AT + 0.025 89.368 + 0.042 133.581 + 0.052 144.87 + 0.067 154.277 + 0.098 144.399 + 0.117 136.873 + 0.150 132.64 + 0.196 129.348 + 0.255 123.233 + 0.299 118.059 + 0.349 112.885 + 0.399 108.652 + 0.449 101.126 + 0.486 101.597 + 0.511 105.36 + 0.516 118.53 + 0.543 100.186 + 0.601 95.482 + 0.656 88.897 + 0.720 81.842 + 0.737 93.601 + 0.754 80.431 + 0.797 70.553 + 0.856 63.498 + 0.898 58.794 + 0.948 51.739 + 1.000 47.976 + 1.063 43.273 + 1.102 41.391 + 1.152 39.04 + 1.200 36.688 + 1.301 30.103 + 1.347 25.399 + 1.401 19.755 + 1.499 12.229 + 1.547 7.996 + 1.599 5.644 + 1.699 2.352 + 1.750 0.0 +; +; 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 +G79 29 146 4,7,10 0.0601 0.124 AT + 0.000 0.4562 + 0.014 1.1376 + 0.018 3.2129 + 0.022 6.2017 + 0.034 27.3705 + 0.040 33.5757 + 0.044 34.8528 + 0.062 33.5201 + 0.096 39.9175 + 0.128 56.9842 + 0.138 60.0917 + 0.182 59.6191 + 0.230 68.8942 + 0.266 71.3440 + 0.300 71.6246 + 0.360 75.8167 + 0.484 79.6244 + 0.516 78.6333 + 0.678 82.1075 + 0.700 78.8360 + 0.720 78.1790 + 0.772 79.5565 + 1.054 73.7176 + 1.086 71.1520 + 1.182 68.8555 + 1.420 57.2479 + 1.520 40.7567 + 1.562 30.5794 + 1.628 11.8028 + 1.652 7.1707 + 1.680 3.9601 + 1.738 1.6764 + 1.928 0.0000 +; +; Aerotech I170G from TRA Cert Data +; Created by Mark Hairfield 12-29-10 +I170G 54 151 10 0.227 0.528 AT + 0.06 89.0 + 0.16 169.0 + 0.25 184.6 + 0.5 202.4 + 0.75 207.3 + 1.0 202.4 + 1.5 177.9 + 2.18 137.9 + 2.25 139.7 + 2.30 131.2 + 2.35 22.2 + 2.40 0.0 +; +; Aerotech I49N-P +I49N-P 38 184 P 0.20500000000000002 0.398 AT + 0.0080 1.406 + 0.025 48.594 + 0.093 52.031 + 0.429 57.344 + 0.665 60.313 + 0.841 60.625 + 1.06 62.344 + 1.295 63.438 + 1.556 62.344 + 1.825 62.344 + 1.994 60.625 + 2.212 60.156 + 3.003 56.719 + 3.785 52.344 + 4.349 49.375 + 4.997 46.563 + 5.998 43.438 + 6.393 42.031 + 6.831 41.563 + 6.999 36.875 + 7.083 33.125 + 7.184 31.406 + 7.369 23.125 + 7.495 16.406 + 7.764 4.219 + 7.882 1.875 + 7.941 0.0 +; +; Aerotech I59WN-P +I59WN-P 38 232 P 0.272 0.487 AT + 0.0090 0.357 + 0.046 138.571 + 0.12 150.0 + 0.193 147.857 + 0.368 157.857 + 0.506 167.857 + 0.699 171.071 + 0.791 171.786 + 0.893 168.571 + 1.058 158.214 + 1.233 146.429 + 1.417 132.143 + 1.509 125.714 + 1.61 100.357 + 1.675 80.357 + 1.785 60.357 + 1.96 53.571 + 2.209 48.571 + 2.531 45.357 + 2.669 43.214 + 3.009 40.714 + 3.387 40.714 + 4.021 38.929 + 4.261 37.5 + 4.997 36.429 + 6.0 33.929 + 6.883 31.429 + 7.003 33.571 + 7.187 30.714 + 7.334 27.5 + 7.574 22.5 + 7.96 17.5 + 8.117 9.643 + 8.319 4.643 + 8.604 0.0 +; +; Input by Tim Van Milligan using ThrustCurve Tracer by John Coker. Data from +; Tripoli certification paperwork dated 25 November 2007. +J401FJ 54 325 6 0.511 0.912 AT + 0.011 440.414 + 0.022 488.102 + 0.075 427.791 + 0.116 422.18 + 0.191 446.024 + 0.277 453.037 + 0.382 462.855 + 0.513 468.466 + 0.712 472.673 + 0.775 471.271 + 0.948 471.271 + 1.06 472.673 + 1.281 469.868 + 1.431 462.855 + 1.607 453.037 + 1.858 426.388 + 2.034 403.946 + 2.135 384.31 + 2.202 378.7 + 2.258 374.492 + 2.277 374.492 + 2.3 380.102 + 2.322 380.102 + 2.345 370.284 + 2.367 359.064 + 2.408 314.181 + 2.461 244.051 + 2.502 186.545 + 2.566 103.792 + 2.607 64.519 + 2.652 42.078 + 2.704 18.234 + 2.783 0.0 +; +; +J510 38 584 P 0.662 1.08 AT + 0.032 1055.904 + 0.11 865.54 + 0.161 829.933 + 0.267 794.325 + 0.351 780.63 + 0.512 705.306 + 0.682 654.633 + 1.318 624.504 + 1.461 475.225 + 1.623 345.121 + 1.934 153.387 + 2.039 115.04 + 2.177 41.086 + 2.317 5.478 + 2.5 0.0 +; +; +J99 54 231 P 0.556 0.899 AT + 0.031 117.296 + 0.078 135.045 + 0.242 144.305 + 0.828 131.38 + 2.539 110.737 + 3.594 102.056 + 4.82 94.146 + 5.938 86.043 + 7.523 81.22 + 8.984 76.976 + 9.047 74.082 + 9.547 16.012 + 9.711 5.209 + 9.82 1.929 + 10.0 0.0 +; +; From AT Instruction Sheet by C. Kobel 3/12/10 +K375NW-P 54 568 P 1.238 2.126 AT + 0.027 886.971 + 0.036 1115.263 + 0.054 1268.705 + 0.135 1279.933 + 0.197 1313.615 + 0.292 1317.357 + 0.422 1343.555 + 0.444 1302.387 + 0.489 1336.07 + 0.552 452.842 + 0.574 396.704 + 0.718 452.842 + 0.794 460.327 + 0.902 437.872 + 0.992 411.674 + 1.189 404.189 + 1.400 366.764 + 1.575 381.734 + 1.791 370.507 + 4.000 366.764 + 4.165 344.309 + 4.290 239.520 + 4.398 239.520 + 4.537 183.382 + 4.645 183.382 + 4.761 93.562 + 5.000 93.562 + 5.200 63.622 + 5.400 44.910 + 5.600 33.682 + 5.800 0.0 +; +; From AT Instruction Sheet by C. Kobel 3/12/10 +K480W-P 54 568 P 1.232 2.059 AT + 0.030 535.684 + 0.045 860.341 + 0.057 915.996 + 0.098 830.194 + 0.159 832.513 + 0.246 795.409 + 0.307 811.642 + 0.398 793.090 + 0.492 809.323 + 0.557 823.237 + 0.621 811.642 + 0.689 779.176 + 0.735 795.409 + 0.845 767.581 + 0.989 718.883 + 1.091 707.288 + 1.250 684.098 + 1.307 667.865 + 1.500 653.952 + 1.606 656.271 + 1.742 651.633 + 1.909 628.443 + 2.000 605.253 + 2.250 586.701 + 2.500 565.830 + 2.750 547.279 + 2.886 544.960 + 3.000 524.089 + 3.064 491.623 + 3.144 417.416 + 3.250 394.226 + 3.292 338.571 + 3.451 271.320 + 3.500 231.898 + 3.625 178.561 + 3.700 143.777 + 3.871 132.182 + 4.000 88.121 + 4.133 41.742 + 4.246 23.190 + 4.500 18.552 + 4.800 0.0 +; +; Input by Tim Van Milligan using ThrustCurve Tracer by John Coker. Data from +; Tripoli certification paperwork dated 25 November 2007. +K513FJ 54 410 6 0.974 1.647 AT + 0.0070 555.093 + 0.015 652.655 + 0.041 551.729 + 0.059 592.099 + 0.074 551.729 + 0.2 575.278 + 0.282 582.007 + 0.412 605.556 + 0.519 615.649 + 0.679 635.834 + 0.823 642.562 + 0.986 649.291 + 1.12 652.655 + 1.328 656.019 + 1.48 649.291 + 1.602 629.105 + 1.854 585.371 + 1.999 555.093 + 2.054 545.0 + 2.08 545.0 + 2.114 528.179 + 2.184 524.815 + 2.229 521.451 + 2.258 504.63 + 2.295 474.352 + 2.325 437.346 + 2.358 380.155 + 2.37 349.877 + 2.399 312.871 + 2.451 272.5 + 2.492 238.858 + 2.529 161.482 + 2.57 84.105 + 2.592 43.735 + 2.618 26.914 + 2.655 13.457 + 2.692 6.728 + 2.726 0.0 +; +; From the curve of the motor instruction sheet. +; Made using Thrust Curve Tracer. +; Tom Koszuta 12/26/2008. +K805G 54 410 P 0.871 1.543 AT + 0.0050 443.21 + 0.032 817.925 + 0.053 825.983 + 0.098 854.187 + 0.199 902.537 + 0.298 918.654 + 0.399 938.8 + 0.5 950.888 + 0.595 950.888 + 0.699 950.888 + 0.8 942.829 + 0.903 934.771 + 1.002 922.683 + 1.1 902.537 + 1.201 874.333 + 1.254 866.275 + 1.267 878.362 + 1.299 854.187 + 1.334 846.129 + 1.35 850.158 + 1.398 821.954 + 1.499 781.662 + 1.522 789.72 + 1.536 781.662 + 1.546 765.545 + 1.597 757.487 + 1.698 721.224 + 1.799 701.078 + 1.897 688.991 + 1.95 693.02 + 1.961 705.107 + 1.982 697.049 + 1.995 668.845 + 2.014 596.319 + 2.035 447.24 + 2.051 342.481 + 2.064 269.955 + 2.08 205.488 + 2.099 165.197 + 2.123 120.876 + 2.147 84.613 + 2.171 52.379 + 2.197 0.0 +; +; +L1170FJ 75 665 P 2.8000000000000003 4.99 AT + 0.031 992.64 + 0.072 1400.144 + 0.113 1473.286 + 0.144 1389.696 + 0.351 1285.207 + 1.495 1431.491 + 1.856 1431.491 + 2.227 1358.349 + 2.753 1201.616 + 2.928 1170.27 + 3.0 1065.782 + 3.113 679.175 + 3.247 355.261 + 3.361 177.63 + 3.464 83.591 + 3.67 0.0 +; +;Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve +;Tracer program. Thrust curve and engine data from Aerotech thrust stand. +L1390G 75 517.91 1000 1.973 3.876 AT +0.018 906.203 +0.041 1249.41 +0.055 1336.72 +0.099 1369.84 +0.173 1402.96 +0.236 1411.99 +0.284 1411.99 +0.678 1586.61 +0.869 1649.83 +0.939 1640.8 +1.102 1625.74 +1.197 1628.76 +1.293 1619.72 +1.374 1607.68 +1.455 1601.66 +1.518 1589.62 +1.592 1550.48 +1.691 1499.3 +1.838 1424.03 +1.96 1366.83 +2.1 1312.64 +2.225 1261.46 +2.343 1228.34 +2.417 1213.29 +2.479 1204.26 +2.524 1198.23 +2.564 1198.23 +2.601 1165.12 +2.638 1074.8 +2.66 957.383 +2.689 839.968 +2.712 713.522 +2.737 590.085 +2.763 427.511 +2.8 295.043 +2.844 153.543 +2.877 69.245 +2.911 0 +; +; Based on AT Instruction Sheet by C. Kobel 12/22/2010 +L1520T 75 531 P 1.773 3.620 AT + 0.011 1484.553 + 0.055 1506.304 + 0.089 1468.239 + 0.155 1560.684 + 0.200 1571.559 + 0.300 1582.435 + 0.400 1598.749 + 0.500 1620.501 + 0.600 1642.252 + 0.700 1653.128 + 0.800 1674.88 + 0.900 1691.194 + 1.000 1685.756 + 1.100 1696.632 + 1.200 1691.194 + 1.300 1691.194 + 1.400 1680.318 + 1.500 1664.004 + 1.600 1636.814 + 1.700 1620.501 + 1.800 1604.187 + 1.900 1576.997 + 2.000 1560.684 + 2.100 1538.932 + 2.200 1500.866 + 2.227 1435.611 + 2.250 1125.65 + 2.290 832.002 + 2.366 647.113 + 2.400 456.785 + 2.440 244.706 + 2.500 59.817 + 2.600 0.0 +; +; Curvefit of Aerotech Instructions by C. Kobel 11/19/08 +L2200G 75 665 0-6-10-14-18 2.516 4.751 AT + 0.011 1195.177 + 0.024 2029.903 + 0.037 2380.868 + 0.050 2542.122 + 0.100 2570.578 + 0.150 2561.093 + 0.200 2523.151 + 0.250 2485.208 + 0.300 2523.151 + 0.350 2570.578 + 0.400 2674.919 + 0.500 2912.057 + 0.600 3073.311 + 0.700 3073.311 + 0.800 3101.768 + 0.900 3092.282 + 1.000 3092.282 + 1.100 2959.485 + 1.186 2807.716 + 1.227 2437.781 + 1.270 2257.556 + 1.300 2162.701 + 1.400 1991.961 + 1.500 1878.135 + 1.600 1792.765 + 1.700 1688.424 + 1.800 1612.54 + 1.900 1584.083 + 2.000 1536.656 + 2.048 1498.714 + 2.084 1403.858 + 2.102 1166.72 + 2.134 796.784 + 2.186 455.305 + 2.237 237.138 + 2.300 94.855 + 2.400 0.0 +; +; Entered by Tim Van Milligan. Used John Coker's ThrustCurve Tracer software and +; data supplied by Aerotech thrust stand data. The total weight is a guess. +L339N 98 309 4 1.796 4.5 AT + 0.049 2.884 + 0.074 373.449 + 0.123 399.403 + 0.156 408.054 + 0.279 415.984 + 0.427 417.426 + 0.476 421.031 + 0.509 416.705 + 0.632 415.984 + 0.837 414.542 + 0.894 418.868 + 0.943 405.17 + 1.026 400.124 + 1.124 402.286 + 1.255 397.961 + 1.362 392.914 + 1.51 391.472 + 1.575 394.356 + 1.592 385.705 + 1.657 387.147 + 1.838 384.984 + 2.026 382.821 + 2.174 379.937 + 2.404 377.053 + 2.478 378.495 + 2.552 377.053 + 2.617 378.495 + 2.683 366.96 + 2.773 359.751 + 2.806 363.355 + 2.937 359.751 + 3.232 351.099 + 3.314 355.425 + 3.356 351.099 + 3.815 345.332 + 3.979 340.285 + 4.233 336.681 + 4.414 333.797 + 4.668 330.913 + 4.996 329.471 + 5.39 323.704 + 5.686 320.099 + 5.989 314.331 + 6.178 310.727 + 6.325 306.401 + 6.514 302.075 + 6.621 302.075 + 6.851 297.75 + 7.195 290.54 + 7.277 293.424 + 7.326 287.656 + 7.441 283.331 + 7.49 286.214 + 7.54 283.331 + 7.696 275.4 + 7.81 273.958 + 7.884 276.842 + 7.942 278.284 + 8.015 276.121 + 8.073 270.354 + 8.188 155.003 + 8.212 118.956 + 8.278 54.071 + 8.311 26.675 + 8.352 7.93 + 8.426 0.0 +; +; Curvefit of AeroTech Instructions by C. Kobel 11/19/08 +M1500G 75 665 0-6-10-14-18 2.631 4.896 AT + 0.012 1183.8 + 0.023 1614.273 + 0.050 1694.987 + 0.100 1716.511 + 0.150 1694.987 + 0.200 1603.512 + 0.250 1517.417 + 0.300 1490.512 + 0.400 1474.37 + 0.500 1485.132 + 0.600 1512.036 + 0.700 1533.56 + 0.800 1571.226 + 0.900 1608.892 + 1.000 1630.416 + 1.100 1657.321 + 1.200 1684.225 + 1.300 1694.987 + 1.400 1694.987 + 1.500 1700.368 + 1.600 1700.368 + 1.700 1705.749 + 1.800 1689.606 + 1.900 1662.702 + 2.000 1657.321 + 2.100 1608.892 + 2.200 1581.988 + 2.300 1555.083 + 2.400 1522.798 + 2.500 1490.512 + 2.600 1463.608 + 2.700 1431.322 + 2.800 1415.18 + 2.900 1388.275 + 3.000 1361.371 + 3.100 1372.132 + 3.200 1286.038 + 3.250 1226.848 + 3.300 973.945 + 3.400 478.901 + 3.450 220.617 + 3.500 80.714 + 3.600 0.0 +; +; Entered by Tim Van Milligan. Used John Coker's ThrustCurve Tracer software and +; data from TRA certification dated 10-14-08 +M1800FJ 98 751 4 5.599 9.162 AT + 0.021 3007.361 + 0.043 1964.715 + 0.059 1858.322 + 0.069 1766.116 + 0.134 1829.951 + 0.192 1822.858 + 0.267 1822.858 + 0.363 1865.415 + 0.502 1936.344 + 0.582 1922.158 + 0.684 1964.715 + 1.132 2071.107 + 1.581 2149.129 + 1.923 2198.778 + 2.142 2220.057 + 2.393 2220.057 + 2.463 2198.778 + 2.655 2106.572 + 2.831 2007.272 + 2.922 1978.901 + 3.029 1915.065 + 3.21 1808.673 + 3.349 1695.187 + 3.526 1588.795 + 3.723 1439.845 + 3.851 1397.288 + 3.921 1361.824 + 4.017 1255.432 + 4.097 1120.668 + 4.167 978.811 + 4.263 780.212 + 4.327 624.169 + 4.402 453.941 + 4.428 375.92 + 4.482 276.621 + 4.53 177.321 + 4.583 99.3 + 4.653 42.557 + 4.76 21.279 + 4.952 0.0 +; +; +M1845 98 597 P 3.7720000000000002 6.682 AT + 0.024 2261.638 + 0.067 2115.94 + 1.032 2268.261 + 1.354 2433.828 + 2.253 2288.129 + 2.406 2149.053 + 2.578 1821.232 + 3.065 1579.504 + 3.583 1410.627 + 3.838 1364.268 + 3.913 1218.569 + 3.995 685.445 + 4.109 400.671 + 4.352 248.35 + 4.498 33.113 + 4.729 0.0 +; +; Entered by Tim Van Milligan for RockSim Users. Used John Coker's ThrustCurve +; Tracer software and TRA cert paperwork dated 10-14-08. +M2100G 98 597 4 4.03 7.03 AT + 0.014 72.789 + 0.017 1148.45 + 0.021 1552.833 + 0.038 1593.272 + 0.042 1908.691 + 0.052 2062.357 + 0.077 2151.321 + 0.115 2207.935 + 0.167 2240.285 + 0.223 2256.461 + 0.272 2256.461 + 0.31 2232.198 + 0.415 2280.724 + 0.59 2385.863 + 0.701 2410.126 + 0.876 2507.179 + 0.959 2555.705 + 1.043 2588.055 + 1.176 2677.02 + 1.263 2782.159 + 1.333 2830.685 + 1.437 2846.861 + 1.517 2879.211 + 1.608 2968.176 + 1.667 2943.913 + 1.81 2935.825 + 1.926 2895.387 + 1.999 2846.861 + 2.041 2782.159 + 2.152 2531.442 + 2.393 1949.129 + 2.484 1787.376 + 2.56 1674.148 + 2.738 1504.307 + 2.836 1439.606 + 2.958 1366.817 + 3.091 1285.94 + 3.178 1229.326 + 3.23 1196.976 + 3.283 1180.8 + 3.401 1188.888 + 3.447 1140.362 + 3.478 1035.222 + 3.513 913.907 + 3.516 541.874 + 3.527 444.822 + 3.541 0.0 +; +; @TI: 14137.65, @TIa: 14071.08, @TIe: 0.0%, @ThMax: 2137.42, @ThAvg: 1048.203, @Tb: 13.424 +; Exported using ThrustCurveTool, www.ThrustGear.com +N1048 98 1046 P 7.925 12.777 AT +0.0 0.457288 +0.152 0.314574 +0.162 40.2069 +0.164 148.3954 +0.168 598.904 +0.172 890.058 +0.176 995.096 +0.178 1158.031 +0.182 1342.306 +0.19 1556.716 +0.222 1959.8 +0.234 2050.53 +0.254 2111.01 +0.308 2119.9 +0.356 2073.29 +0.47 2091.07 +0.528 1989.543 +0.582 1825.825 +0.648 1733.526 +0.782 1658.07 +0.892 1701.725 +0.914 1633.231 +0.966 1669.558 +1.7839 1594.076 +1.8239 1551.156 +3.1999 1533.43 +5.4538 1378.986 +6.9577 1170.933 +10.9216 424.692 +13.5895 106.0499 +14.6754 12.60914 +16.1354 0.0 +; +; +N3300 98 1046 P 7.5120000000000005 12.054 AT + 0.0070 2069.581 + 0.025 2444.865 + 0.298 2654.583 + 0.852 3068.499 + 1.197 3576.236 + 1.502 3841.143 + 1.719 3929.445 + 2.007 4188.832 + 2.419 4172.276 + 2.753 3885.294 + 3.193 3278.217 + 3.552 2847.744 + 3.786 2665.621 + 3.871 2345.525 + 4.003 866.465 + 4.092 209.718 + 4.18 0.0 +; +; Pro29-1G 56F120-VM 14A +F120-VM 29 98 14-11-9-7-5 0.0314 0.1062 CTI + 0.013 79.242 + 0.017 90.427 + 0.04 101.422 + 0.125 127.583 + 0.179 136.114 + 0.222 139.905 + 0.289 143.507 + 0.354 138.578 + 0.394 125.498 + 0.406 123.602 + 0.416 125.118 + 0.423 130.047 + 0.431 120.569 + 0.447 25.592 + 0.453 8.72 + 0.455 0.0 +; +; Pro-24-3G VMax +F240-VM-15A 24 133 3-5-6-8-9-10 0.0303 0.0918 CTI + 0.0040 100.528 + 0.0070 197.493 + 0.01 222.032 + 0.022 241.425 + 0.028 237.863 + 0.041 239.446 + 0.058 252.507 + 0.077 263.984 + 0.089 275.462 + 0.097 271.504 + 0.104 273.879 + 0.119 278.628 + 0.147 281.398 + 0.177 272.296 + 0.207 258.443 + 0.246 226.385 + 0.253 218.47 + 0.259 188.786 + 0.266 127.045 + 0.272 74.802 + 0.28 31.266 + 0.286 15.831 + 0.294 8.707 + 0.31 3.562 + 0.328 0.0 +; +; Pro29-1G 55F29-IM 12A +F29-IM 29 98 12-9-7-5-3 0.0376 0.1058 CTI + 0.0060 5.661 + 0.038 23.312 + 0.05 26.309 + 0.229 30.257 + 0.327 32.208 + 0.485 33.159 + 1.031 31.78 + 1.516 27.07 + 1.688 24.834 + 1.765 20.172 + 1.852 9.467 + 1.963 2.093 + 2.0 0.0 +; +; Pro-24-3G White Long Burn +F30-WH_LB-6A 24 133 2-3-5-6 0.04 0.1022 CTI + 0.014 54.222 + 0.056 43.456 + 0.092 50.185 + 0.16 54.063 + 0.232 48.364 + 0.363 45.752 + 0.499 43.14 + 0.655 40.29 + 0.843 37.836 + 1.216 32.612 + 1.368 30.317 + 1.54 26.359 + 1.675 23.509 + 1.861 19.077 + 2.013 14.565 + 2.159 10.053 + 2.302 4.828 + 2.462 1.504 + 2.598 0.0 +; +; +F36-SS 29 98 2-4-6-8-11 0.035 0.104 CTI +0.01 12 +0.02 46 +0.03 75 +0.04 79 +0.06 77 +0.07 62 +0.08 32 +0.1 35 +0.2 38 +0.3 39 +0.4 41 +0.5 43 +0.6 43 +0.7 43 +0.8 43 +0.85 47 +0.92 54 +0.95 32 +0.99 8 +1.05 0 +; +; +F36-BS 29 98 5-7-9-11-14 0.032 0.101 CTI +0.01 12 +0.02 25 +0.03 41 +0.04 42 +0.05 42 +0.06 40 +0.07 34 +0.08 34 +0.09 35 +0.1 36 +0.2 40 +0.3 42 +0.4 43 +0.5 43 +0.6 43 +0.7 43 +0.8 42 +0.9 41 +1 40 +1.1 38 +1.24 37 +1.3 12 +1.4 2 +1.5 0 +; +; +F59-WT 29 98 3-5-7-9-12 0.031 0.099 CTI +0.01 16 +0.02 62 +0.03 67 +0.04 71 +0.07 58 +0.1 63 +0.2 67 +0.3 69 +0.4 67 +0.5 65 +0.6 63 +0.7 61 +0.87 60 +0.9 23 +0.97 0 +; +; Pro-24-3G Smoky Sam +F79-SS-13A 24 133 4-6-7-9-11 0.0401 0.1075 CTI + 0.0050 60.0 + 0.013 89.007 + 0.022 96.291 + 0.043 81.722 + 0.119 85.563 + 0.198 87.947 + 0.267 89.272 + 0.343 89.934 + 0.404 90.861 + 0.498 91.523 + 0.555 89.669 + 0.622 83.974 + 0.663 80.53 + 0.704 78.94 + 0.729 74.172 + 0.747 66.887 + 0.768 53.775 + 0.793 36.556 + 0.821 18.543 + 0.852 7.815 + 0.892 2.119 + 0.928 0.795 + 0.997 0.0 +; +; +G106-SK 29 187 5-7-9-11-14 0.081 0.187 CTI +0.018 20 +0.023 80 +0.03 131 +0.05 105 +0.065 75 +0.1 94 +0.25 104 +0.4 111 +0.65 120 +0.86 123 +1.05 124 +1.13 121 +1.17 110 +1.2 85 +1.23 40 +1.25 20 +1.3 5 +1.36 0 +; +; Pro-24-6G White/Dual Thrust +G107-WH_DT-12A 24 228 3-5-6-8-9-10 0.0757 0.1698 CTI + 0.0060 133.228 + 0.011 198.418 + 0.022 221.835 + 0.046 212.658 + 0.081 218.354 + 0.125 214.873 + 0.168 210.443 + 0.219 204.43 + 0.253 195.886 + 0.274 183.544 + 0.305 88.291 + 0.412 93.671 + 0.529 93.987 + 0.663 94.304 + 0.789 93.987 + 0.899 91.139 + 0.953 89.873 + 0.999 87.025 + 1.03 81.329 + 1.057 69.937 + 1.102 54.114 + 1.154 42.405 + 1.197 31.646 + 1.277 17.089 + 1.335 9.81 + 1.398 3.165 + 1.451 0.0 +; +; Pro-24-6G White +G117-WH-11A 24 228 4-6-8-9-10 0.0791 0.1725 CTI + 0.0080 168.643 + 0.013 177.339 + 0.022 177.866 + 0.035 171.278 + 0.063 157.839 + 0.103 154.941 + 0.151 151.515 + 0.196 148.88 + 0.246 147.563 + 0.311 144.137 + 0.391 140.711 + 0.474 138.076 + 0.564 135.705 + 0.662 131.225 + 0.762 125.955 + 0.858 116.733 + 0.928 101.713 + 0.973 83.004 + 1.038 57.444 + 1.08 42.688 + 1.131 31.884 + 1.185 17.655 + 1.224 9.486 + 1.258 5.27 + 1.322 2.372 + 1.4 0.791 + 1.441 0.0 +; +; +G118-BS 29 187 6-8-10-12-15 0.083 0.188 CTI +0.005 1.3 +0.012 80 +0.02 156 +0.04 148 +0.05 105 +0.11 121 +0.3 131 +0.5 134 +0.7 130 +0.95 126 +1.13 126 +1.18 115 +1.27 40 +1.31 20 +1.35 6 +1.37 0 +; +; Pro29 3G 159G125-RL 14A +G125-RL 29 187 14-11-9-7-5 0.0896 0.1945 CTI + 0.0040 15.683 + 0.022 170.834 + 0.039 116.877 + 0.122 142.642 + 0.236 149.737 + 0.589 142.642 + 0.801 131.253 + 1.068 122.104 + 1.118 107.915 + 1.145 78.416 + 1.174 43.129 + 1.211 21.471 + 1.247 8.775 + 1.299 0.0 +; +; +G126-WT 29 142 4-6-8-10-13 0.059 0.145 CTI +0.01 55 +0.02 168 +0.03 157 +0.04 148 +0.05 125 +0.1 135 +0.2 141 +0.3 142 +0.4 141 +0.6 133 +0.75 127 +0.81 128 +0.86 60 +0.9 15 +0.95 0 +; +; +G131-SS 29 187 5-7-9-11-14 0.094 0.2 CTI +0.01 6 +0.02 40 +0.03 116 +0.04 131 +0.05 146 +0.06 147 +0.07 140 +0.08 136 +0.09 130 +0.1 126 +0.2 129 +0.3 132 +0.4 137 +0.5 139 +0.6 141 +0.7 142 +0.8 145 +0.85 150 +0.87 155 +0.9 116 +0.93 60 +0.95 30 +1 3 +1.1 0 +; +; Pro-24-6G Blue Streak +G150-BS-13A 24 228 4-6-8-9-11-12 0.0659 0.1599 CTI + 0.0050 114.776 + 0.0060 177.441 + 0.01 222.625 + 0.016 243.404 + 0.019 247.032 + 0.037 215.369 + 0.077 206.135 + 0.12 204.485 + 0.163 200.198 + 0.204 195.91 + 0.249 192.942 + 0.316 186.675 + 0.387 180.409 + 0.444 176.121 + 0.536 168.206 + 0.616 160.62 + 0.639 156.662 + 0.676 142.48 + 0.715 114.776 + 0.75 93.008 + 0.784 72.23 + 0.831 49.802 + 0.889 31.662 + 0.923 21.768 + 0.953 14.842 + 0.996 8.245 + 1.03 5.937 + 1.061 2.309 + 1.099 0.0 +; +; Pro29-2G 110G250-VM 14A +G250-VM 29 142 14-11-9-7-5 0.0575 0.1413 CTI + 0.0060 151.621 + 0.011 198.079 + 0.016 203.121 + 0.031 201.681 + 0.075 226.17 + 0.122 250.3 + 0.216 280.192 + 0.25 287.035 + 0.287 284.874 + 0.354 269.748 + 0.374 258.583 + 0.4 233.373 + 0.413 234.094 + 0.42 227.611 + 0.433 137.935 + 0.445 33.854 + 0.454 0.0 +; +; +G50-IM 38 127 6-8-11-12-15 0.0777 0.218 CTI +0.02 10 +0.04 58 +0.052 72 +0.07 65 +0.106 43 +0.23 51 +0.4 55 +0.85 57 +1.5 55 +2 51 +2.5 44.5 +2.78 44 +2.86 37 +2.93 20 +3.02 0 +; +; Pro29-3G 159G54-RL 12A +G54-RL 29 187 12-9-7-5-3 0.0968 0.1982 CTI + 0.018 107.269 + 0.031 113.588 + 0.059 103.508 + 0.135 121.712 + 0.22 104.561 + 0.299 95.534 + 0.432 88.312 + 0.959 69.657 + 1.757 43.479 + 2.418 20.762 + 2.851 9.478 + 3.013 5.567 + 3.026 0.0 +; +; +G57-CL 29 142 3-5-7-9-12 0.059 0.146 CTI +0.01 8 +0.02 70 +0.04 88 +0.05 80 +0.06 71 +0.08 76 +0.11 79 +0.2 81 +0.6 72 +1 56 +1.5 47 +1.6 48 +1.7 28 +1.8 14 +1.9 3 +1.93 0 +; +; Pro-38-1G White +G58-WH-13A 38 127 5-7-8-10-12-13 0.0763 0.2125 CTI + 0.029 90.25 + 0.046 69.17 + 0.058 59.947 + 0.084 47.167 + 0.171 57.971 + 0.28 59.552 + 0.455 61.265 + 0.586 61.66 + 0.741 62.319 + 0.952 63.768 + 1.217 64.69 + 1.43 63.768 + 1.626 61.265 + 1.807 58.103 + 1.959 53.887 + 2.104 48.353 + 2.168 47.563 + 2.21 44.005 + 2.247 37.286 + 2.329 22.266 + 2.375 10.277 + 2.414 2.767 + 2.442 1.186 + 2.5 0.0 +; +; Cesaroni G60 +; converted from TMT test stand data 2002 (www.tripoli.org) +; provided by ThrustCurve.org (www.thrustcurve.org) +G60 38 125 0 0.077056 0.2016 CTI + 0.043 65.216 + 0.130 74.906 + 0.218 84.596 + 0.305 83.963 + 0.393 81.982 + 0.480 81.956 + 0.568 81.138 + 0.655 80.530 + 0.743 79.923 + 0.830 78.867 + 0.918 76.675 + 1.005 75.118 + 1.094 73.732 + 1.182 71.315 + 1.270 68.781 + 1.357 66.853 + 1.445 65.111 + 1.532 63.526 + 1.620 61.229 + 1.707 59.249 + 1.795 57.110 + 1.882 51.671 + 1.970 18.562 + 2.057 2.667 + 2.146 1.470 + 2.234 0.000 +; +; Pro-24-6G White Long Burn +G65-WH_LB-8A 24 228 3-5-6-7 0.08 0.1740 CTI + 0.011 157.857 + 0.024 149.524 + 0.042 132.143 + 0.057 125.476 + 0.094 134.048 + 0.122 131.19 + 0.175 106.429 + 0.269 94.048 + 0.376 87.381 + 0.54 82.143 + 0.707 78.333 + 0.845 74.762 + 1.002 71.19 + 1.206 65.476 + 1.376 57.857 + 1.553 48.333 + 1.726 39.048 + 1.914 28.333 + 2.061 18.095 + 2.205 8.571 + 2.299 3.095 + 2.398 0.0 +; +; Pro-29-2G White +G68-WH-13A 29 142 5-6-7-9-10-11 0.0599 0.1559 CTI + 0.012 50.329 + 0.017 79.315 + 0.019 86.693 + 0.03 91.831 + 0.047 73.386 + 0.048 81.686 + 0.049 65.876 + 0.061 58.235 + 0.088 66.798 + 0.12 70.883 + 0.2 72.991 + 0.307 75.099 + 0.38 75.626 + 0.487 76.416 + 0.614 76.548 + 0.726 75.626 + 0.818 73.518 + 0.987 70.487 + 1.096 68.116 + 1.269 63.505 + 1.388 61.528 + 1.446 57.444 + 1.483 49.144 + 1.537 29.381 + 1.569 18.05 + 1.613 5.665 + 1.638 2.899 + 1.676 1.449 + 1.723 0.395 + 1.759 0.0 +; +; CTI Pro38-1G 117 G69SK - 14A +G69SK 38 126 14-11-9-7-5 0.067 0.198 CTI + 0.015 49.371 + 0.023 79.41 + 0.035 91.872 + 0.064 82.605 + 0.099 52.407 + 0.166 57.041 + 0.228 59.278 + 0.375 64.231 + 1.297 69.024 + 1.453 68.864 + 1.533 67.746 + 1.589 65.189 + 1.686 58.639 + 1.735 42.821 + 1.781 26.363 + 1.816 13.901 + 1.89 5.432 + 1.954 1.278 + 1.969 0.0 +; +;CTI Pro38-1G 141 G78BS - 15A +G78BS 38 126 15-12-10-8-6 0.069 0.197 CTI +0.006 104.068 +0.018 137.928 +0.036 70.707 +0.047 62.242 +0.084 73.694 +0.135 78.176 +0.238 84.151 +0.438 89.628 +0.63 88.135 +0.859 87.139 +1.283 77.18 +1.447 70.707 +1.643 67.719 +1.713 64.234 +1.743 54.275 +1.79 18.424 +1.818 6.473 +1.852 0 +; +; Pro29-3G 93G80-SK 14A +G80-SK 29 142 14-11-9-7-5 0.0564 0.1432 CTI + 0.0070 51.315 + 0.025 108.143 + 0.047 65.31 + 0.122 78.032 + 0.307 89.059 + 0.446 93.865 + 0.581 95.137 + 0.75 91.886 + 0.924 84.252 + 0.972 83.404 + 1.038 88.352 + 1.064 67.147 + 1.08 40.43 + 1.093 21.629 + 1.11 9.754 + 1.131 2.545 + 1.178 0.0 +; +; +G83-BS 29 142 5-7-9-11-14 0.058 0.145 CTI +0.01 13 +0.02 82 +0.03 98 +0.04 100 +0.05 90 +0.06 86 +0.12 93 +0.2 96 +0.3 96 +0.7 92 +0.9 88 +1.07 83 +1.1 80 +1.2 30 +1.3 4 +1.33 0 +; +; Pro-24-6G Green3 +G84-GR-10A 24 228 4-5-7-8-9 0.0773 0.1720 CTI + 0.0050 80.264 + 0.017 94.69 + 0.023 108.745 + 0.031 124.835 + 0.044 129.828 + 0.081 124.28 + 0.149 116.513 + 0.224 111.149 + 0.301 107.635 + 0.386 103.382 + 0.506 98.203 + 0.623 94.135 + 0.759 89.696 + 0.849 85.997 + 0.974 81.374 + 1.09 77.86 + 1.149 74.716 + 1.171 78.97 + 1.202 70.832 + 1.244 69.168 + 1.3 68.243 + 1.326 56.777 + 1.373 52.523 + 1.403 40.687 + 1.447 29.036 + 1.515 14.425 + 1.562 6.103 + 1.597 2.034 + 1.641 0.0 +; +; +G88-SS 29 142 2-4-6-8-11 0.064 0.152 CTI +0.03 7 +0.04 60 +0.05 90 +0.06 113 +0.07 116 +0.08 113 +0.1 86 +0.12 81 +0.15 86 +0.3 92 +0.4 95 +0.5 97 +0.75 100 +0.82 108 +0.84 106 +0.9 56 +0.93 25 +1 0 +; +; +H100-IM 38 186 6-8-11-12-15 0.1544 0.327 CTI +0.016 68 +0.056 116 +0.09 118 +0.14 115 +0.5 116 +0.6 114 +1.25 113 +2.32 99 +2.44 100 +2.55 89 +2.77 0 +; +; Pro-38-2G White +H110-WH-14A 38 186 5-7-9-11-13-14 0.1526 0.3253 CTI + 0.029 93.733 + 0.052 118.066 + 0.093 98.531 + 0.153 109.327 + 0.238 113.439 + 0.461 118.923 + 0.592 120.979 + 0.72 122.693 + 0.896 124.406 + 1.15 124.92 + 1.246 122.521 + 1.461 119.608 + 1.622 117.381 + 1.79 115.667 + 1.922 112.583 + 2.114 112.754 + 2.174 111.726 + 2.21 98.874 + 2.259 69.4 + 2.319 47.466 + 2.365 28.96 + 2.441 12.166 + 2.526 7.368 + 2.597 2.228 + 2.692 0.0 +; +; +H118-CL 29 231 3-5-7-9-12 0.111 0.232 CTI +0.01 7 +0.02 144 +0.04 183 +0.06 182 +0.08 176 +0.09 173 +0.1 172 +0.2 160 +0.4 147 +0.5 142 +0.7 134 +0.8 127 +1 121 +1.1 118 +1.2 115 +1.4 109 +1.5 104 +1.6 75 +1.7 31 +1.8 13 +1.9 0 +; +;Pro-38 Red Lightning 2 Grain reload +H120-14A 38 186 14-11-9-7-5 0.1366 0.295 CTI +0.016 53.023 +0.029 107.113 +0.036 124.55 +0.049 129.532 +0.062 117.789 +0.072 98.217 +0.131 123.838 +0.199 136.649 +0.258 144.122 +0.313 147.681 +0.369 146.257 +0.441 145.19 +0.558 143.411 +0.683 141.631 +0.777 140.92 +0.859 139.14 +0.98 136.293 +1.097 133.091 +1.251 128.82 +1.434 122.771 +1.558 118.856 +1.639 117.077 +1.731 117.077 +1.884 117.077 +1.927 105.334 +1.959 88.964 +1.995 68.325 +2.031 41.991 +2.083 18.505 +2.142 6.761 +2.181 2.135 +2.24 0 +; +; +H123-SK-29mm 29 231 3-5-7-9-12 0.106 0.228 CTI +0.021 10 +0.028 139 +0.055 139 +0.075 108 +0.13 120 +0.35 132 +0.65 140 +1 144 +1.15 143 +1.22 145 +1.35 23 +1.53 0 +; +; Entered by Tim Van Milligan for RockSim users. Used ThrustCurve Tracer by John +; Coker. Data from CAR web site. +H123-38mm 38 186 14 0.123 0.297 CTI + 0.02 143.233 + 0.039 136.193 + 0.057 141.067 + 0.061 138.088 + 0.072 95.308 + 0.084 86.644 + 0.112 108.575 + 0.17 113.72 + 0.243 120.76 + 0.327 125.904 + 0.413 130.236 + 0.487 134.839 + 0.699 142.15 + 0.71 142.42 + 0.765 143.503 + 0.812 142.691 + 0.871 148.377 + 0.888 143.774 + 0.914 144.586 + 0.949 144.857 + 0.99 141.879 + 1.033 145.399 + 1.072 145.399 + 1.112 144.045 + 1.143 142.42 + 1.182 144.316 + 1.241 142.691 + 1.307 141.608 + 1.387 138.63 + 1.448 135.651 + 1.499 133.485 + 1.552 129.965 + 1.577 131.59 + 1.605 131.59 + 1.634 132.402 + 1.652 132.402 + 1.669 129.153 + 1.685 121.843 + 1.699 108.575 + 1.744 61.463 + 1.775 27.347 + 1.822 14.892 + 1.869 7.581 + 1.912 1.895 + 1.939 0.0 +; +; +H125-TamedTiger 38 186 3-5-7-9-12 0.1380 0.293 CTI +0.01 1.252 +0.02 2.921 +0.03 9.635 +0.04 78.025 +0.05 128.019 +0.06 139.095 +0.07 98.5463 +0.08 93.122 +0.09 98.0152 +0.1 102.947 +0.2 128.398 +0.3 135.947 +0.4 140.309 +0.5 145.961 +0.6 148.616 +0.7 149.906 +0.8 150.589 +0.9 152.675 +1.0 154.078 +1.1 153.471 +1.2 151.992 +1.3 151.537 +1.4 146.757 +1.5 145.961 +1.6 141.371 +1.7 139.209 +1.8 133.595 +1.9 70.7805 +2.0 18.4726 +2.1 4.58967 +2.15 0.0 +; +; +H133-BS 29 187 5-7-9-11-14 0.085 0.19 CTI +0.01 10 +0.017 100 +0.023 190 +0.028 200 +0.042 140 +0.05 135 +0.12 152 +0.35 154 +1 135 +1.065 110 +1.2 25 +1.28 0 +; +; Pro-29-4G White +H135-WH-12A 29 231 3-5-7-8-10-11 0.1198 0.2512 CTI + 0.012 166.804 + 0.054 158.622 + 0.101 155.718 + 0.156 153.079 + 0.223 151.496 + 0.312 150.44 + 0.566 150.968 + 0.706 149.12 + 0.946 143.842 + 1.121 140.411 + 1.222 136.452 + 1.278 136.979 + 1.341 131.437 + 1.374 126.686 + 1.4 117.185 + 1.431 100.029 + 1.482 71.261 + 1.535 49.355 + 1.558 30.88 + 1.598 11.877 + 1.62 5.015 + 1.644 2.375 + 1.676 0.0 +; +; +H140-CL 29 276 2-4-6-8-11 0.139 0.277 CTI +0.015 30 +0.025 240 +0.04 245 +0.09 220 +0.2 200 +0.4 185 +0.8 160 +1.4 140 +1.49 100 +1.63 50 +1.75 35 +1.9 12 +2.05 0 +; +; Pro29-4G 207H151-RL 15A +H151-RL 29 231 15-12-10-8-6 0.118 0.238 CTI + 0.0080 125.295 + 0.021 209.602 + 0.052 160.928 + 0.118 186.779 + 0.293 190.738 + 0.465 183.518 + 0.683 171.641 + 0.988 145.557 + 1.133 134.145 + 1.221 74.292 + 1.293 29.81 + 1.372 10.014 + 1.398 6.521 + 1.4 0.0 +; +; +H152BS 38 186 15-12-10-8-6 0.138 0.298 CTI + 0.018 212.503 + 0.051 207.443 + 0.059 153.052 + 0.077 153.052 + 0.099 163.172 + 0.139 166.966 + 0.168 174.556 + 0.223 173.291 + 0.256 175.821 + 0.304 175.821 + 0.396 179.615 + 0.538 175.821 + 0.659 174.556 + 0.714 174.556 + 0.758 174.556 + 0.802 170.761 + 0.89 172.026 + 0.974 165.701 + 1.022 168.231 + 1.084 163.172 + 1.212 155.582 + 1.293 151.788 + 1.385 146.728 + 1.447 149.258 + 1.484 144.198 + 1.531 145.463 + 1.575 144.198 + 1.601 137.874 + 1.615 134.079 + 1.623 120.165 + 1.663 82.218 + 1.714 46.801 + 1.766 34.152 + 1.788 30.358 + 1.821 26.563 + 1.828 0.0 +; +; Pro29-6G 298H159-GR 15A +H159-GR 29 320 15-12-10-8-6 0.1874 0.3428 CTI + 0.012 117.276 + 0.032 158.638 + 0.103 177.806 + 0.171 184.868 + 0.299 185.372 + 0.511 178.058 + 0.717 179.319 + 1.272 162.926 + 1.424 159.647 + 1.519 152.585 + 1.584 149.811 + 1.632 146.28 + 1.727 89.281 + 1.768 109.962 + 1.834 25.977 + 1.865 10.593 + 1.887 0.0 +; +; +H160-CL 29 320 3-5-7-9-12 0.166 0.319 CTI +0.015 10 +0.022 260 +0.04 316 +0.1 280 +0.25 241 +0.6 201 +1 175 +1.27 165 +1.35 140 +1.45 100 +1.65 48 +1.85 25 +2.2 0 +; +; +H160-SK 29 276 5-7-9-11-14 0.132 0.272 CTI +0.01 10 +0.02 160 +0.03 185 +0.09 170 +0.25 168 +0.5 176 +0.9 184 +1.1 185 +1.16 180 +1.31 28 +1.383 0 +; +; +H163-WT 29 187 5-7-9-11-14 0.086 0.187 CTI +0.018 10 +0.026 225 +0.055 165 +0.1 170 +0.2 175 +0.35 180 +0.9 175 +0.95 100 +0.98 45 +1.062 0 +; +; +H170-BS 29 231 5-7-9-11-14 0.111 0.232 CTI +0.01 150 +0.015 200 +0.025 240 +0.075 210 +0.13 205 +0.35 204 +0.7 205 +0.8 190 +0.9 185 +0.99 173 +1.1 60 +1.22 25 +1.34 0 +; +; +H175-SS 29 231 5-7-9-11-14 0.122 0.247 CTI +0.021 13 +0.032 175 +0.057 215 +0.08 180 +0.13 175 +0.4 185 +0.6 190 +0.76 195 +0.84 236 +0.88 150 +0.92 30 +1 0 +; +; +H180-SK 29 320 5-7-9-11-14 0.158 0.314 CTI +0.01 10 +0.02 250 +0.03 270 +0.07 239 +0.13 227 +0.35 218 +0.6 216 +0.8 207 +0.98 208 +1.06 204 +1.15 135 +1.23 65 +1.4 12 +1.56 0 +; +; Pro29-5G 260H194-RL 14A +H194-RL 29 276 14-11-9-7-5 0.145 0.284 CTI + 0.0060 179.792 + 0.011 244.07 + 0.021 285.99 + 0.049 204.944 + 0.117 233.823 + 0.181 241.275 + 0.386 236.152 + 0.98 193.765 + 1.075 170.476 + 1.136 144.392 + 1.19 80.58 + 1.285 22.823 + 1.347 0.0 +; +; +H200-BS 29 276 5-7-9-11-14 0.136 0.274 CTI +0.01 40 +0.018 280 +0.026 295 +0.06 250 +0.15 236 +0.65 235 +0.8 227 +0.9 212 +0.98 205 +1.09 135 +1.2 68 +1.3 20 +1.4 0 +; +; +H226-SK 29 365 5-7-9-11-14 0.175 0.360 CTI +0.007 9 +0.012 178 +0.017 320 +0.023 362 +0.047 319 +0.08 302 +0.14 291 +0.615 276 +0.95 257.5 +1 215 +1.077 105 +1.18 81 +1.29 31 +1.34 16 +1.5 0 +; +; Pro29 6G 311H233-RL 14A +H233-RL 29 320 14-11-9-7-5 0.1738 0.3276 CTI + 0.0040 98.643 + 0.01 263.822 + 0.018 348.041 + 0.051 263.822 + 0.156 299.185 + 0.82 262.426 + 0.988 228.46 + 1.05 214.501 + 1.111 142.38 + 1.17 84.218 + 1.242 49.321 + 1.331 17.681 + 1.399 0.0 +; +; +H237-SS 29 276 4-6-8-10-13 0.151 0.294 CTI +0.026 10 +0.028 154 +0.033 238 +0.055 270 +0.07 234 +0.71 259 +0.78 296 +0.8 280 +0.87 50 +0.9 10 +0.937 0 +; +; +H255-BS 29 320 5-7-9-11-14 0.162 0.318 CTI +0.015 10 +0.018 260 +0.024 404 +0.03 412 +0.047 375 +0.08 340 +0.2 316 +0.4 303 +0.6 295 +0.87 285 +0.93 273 +1 200 +1.1 80 +1.252 0 +; +; +H255-WT 29 231 5-7-9-11-14 0.113 0.232 CTI +0.018 10 +0.023 345 +0.039 325 +0.05 276 +0.13 287 +0.35 292 +0.75 259 +0.78 265 +0.87 40 +0.936 0 +; +; +H295-SS 29 320 4-6-8-10-13 0.181 0.342 CTI +0.03 15 +0.031 320 +0.05 355 +0.075 325 +0.13 312 +0.35 315 +0.66 327 +0.72 368 +0.75 370 +0.78 290 +0.8 150 +0.85 25 +0.925 0 +; +; +H340-SS 29 365 5-7-9-11-14 0.2067 0.391 CTI +0.017 6 +0.024 255 +0.0311 395 +0.035 423 +0.043 447.5 +0.06 398 +0.064 389 +0.075 397.5 +0.25 388 +0.4 382 +0.542 376 +0.62 379 +0.66 400 +0.68 407 +0.705 398 +0.74 248 +0.8 59.5 +0.85 8 +0.9 0 +; +; +H399-WT 29 320 3-5-7-9-12 0.14 0.294 CTI +0.015 10 +0.02 320 +0.024 555 +0.05 490 +0.075 475 +0.1 468 +0.2 463 +0.53 451 +0.55 460 +0.575 400 +0.64 200 +0.685 25 +0.71 0 +; +; Pro-29-3G White Long Burn +H54-WH_LB-10A 29 187 3-5-7-8-9 0.0966 0.209 CTI + 0.017 103.061 + 0.047 83.272 + 0.088 91.821 + 0.155 97.836 + 0.199 89.288 + 0.271 80.264 + 0.406 76.623 + 0.599 73.773 + 0.898 69.024 + 1.182 66.016 + 1.475 60.475 + 1.785 53.826 + 2.099 44.802 + 2.296 38.945 + 2.577 27.546 + 2.845 16.148 + 3.097 6.491 + 3.199 2.058 + 3.298 1.108 + 3.5 0.0 +; +; +H87-IM 29 187 3-5-7-9-12 0.0927 0.205 CTI +0.018 5 +0.027 73 +0.032 139.2 +0.048 117 +0.056 87 +0.081 95 +0.147 101 +0.336 103 +0.52 101 +1.6 83 +1.686 81 +1.72 79 +1.778 60 +1.82 38 +1.94 0 +; +; +H90-CL 29 187 3-5-7-9-12 0.084 0.19 CTI +0.021 10 +0.028 154 +0.055 155 +0.075 108 +0.13 120 +0.35 115 +1.4 83 +1.48 84 +1.56 73 +1.69 22 +1.76 8 +1.85 0 +; +; Pro-54-2G Red Lightning Long Burn +I100-RL_LB-17A 54 236 9-11-12-13-15-17 0.3501 0.807 CTI + 0.042 269.267 + 0.043 332.429 + 0.07 225.102 + 0.091 202.307 + 0.14 234.125 + 0.202 245.522 + 0.349 220.828 + 0.523 202.307 + 0.837 183.311 + 1.186 164.315 + 1.681 139.62 + 2.358 110.651 + 3.321 76.459 + 4.095 55.563 + 4.919 37.042 + 5.944 21.37 + 6.726 12.347 + 7.437 6.174 + 8.142 2.849 + 8.735 0.95 + 8.993 0.0 +; +; Pro54-1G 502I120-IM 15A +I120-IM 54 143 15-14-13-12-11-10-9-8-7-6-5 0.3 0.6232000000000001 CTI + 0.035 13.687 + 0.047 87.183 + 0.067 148.493 + 0.096 129.744 + 0.212 141.931 + 0.385 142.118 + 0.671 141.743 + 1.032 139.681 + 1.545 136.868 + 2.15 127.869 + 3.757 92.433 + 4.031 89.058 + 4.122 67.122 + 4.216 23.436 + 4.283 5.25 + 4.3 0.0 +; +; CTI Pro54-1G 465 I150BS 11A +I150BS 54 153 11-10-9-8-7-6-5-4-3-2-1 0.226 0.5700000000000001 CTI + 0.017 11.039 + 0.039 103.397 + 0.045 164.846 + 0.065 179.932 + 0.09 153.439 + 0.166 162.638 + 0.194 161.902 + 0.303 169.261 + 0.483 171.837 + 0.666 173.309 + 0.834 171.469 + 1.275 168.525 + 1.725 156.015 + 2.559 128.05 + 2.77 122.53 + 2.899 118.851 + 2.978 119.219 + 3.003 99.349 + 3.034 82.791 + 3.087 66.233 + 3.16 19.502 + 3.208 0.0 +; +; Cesaroni I170 +; converted from TMT test stand data 2002 (www.tripoli.org) +; provided by ThrustCurve.org (www.thrustcurve.org) +I170 38 242 0 0.209216 0.404992 CTI + 0.044 133.251 + 0.134 230.114 + 0.226 224.136 + 0.318 223.695 + 0.409 223.888 + 0.501 225.265 + 0.593 226.670 + 0.684 229.397 + 0.775 231.998 + 0.866 233.034 + 0.957 233.144 + 1.049 232.703 + 1.141 231.574 + 1.232 227.745 + 1.324 225.844 + 1.416 221.160 + 1.506 217.396 + 1.597 211.711 + 1.689 205.678 + 1.780 198.020 + 1.872 125.016 + 1.964 61.847 + 2.055 23.279 + 2.147 2.066 + 2.239 0.799 + 2.330 0.000 +; +; Pro38-3G White +I175-WH-14A 38 245 6-8-9-11-12-13 0.22890000000000002 0.4375 CTI + 0.019 149.422 + 0.038 180.347 + 0.052 166.763 + 0.106 184.971 + 0.148 187.572 + 0.232 187.861 + 0.338 189.017 + 0.518 190.751 + 0.604 192.197 + 0.733 193.353 + 0.877 195.087 + 1.005 193.931 + 1.128 193.353 + 1.333 193.064 + 1.495 190.751 + 1.648 188.15 + 1.79 183.526 + 1.921 178.035 + 2.001 178.324 + 2.043 176.59 + 2.089 151.156 + 2.147 115.318 + 2.212 70.231 + 2.274 47.11 + 2.32 22.832 + 2.368 8.671 + 2.396 3.757 + 2.435 3.179 + 2.5 0.0 +; +; +I204-IM 29 320 4-6-8-10-13 0.194 0.349 CTI +0.01 100 +0.012 395 +0.03 310 +0.3 286 +0.5 270 +0.7 251 +1 228 +1.1 215 +1.2 165 +1.3 125 +1.4 95 +1.5 52 +1.6 36 +1.72 0 +; +; +I216-CL(I) 38 367 5-7-9-11-14 0.3125 0.601 CTI +0.017 35 +0.03 300 +0.035 345 +0.05 325 +0.07 275 +0.14 292 +0.26 296 +0.8 280 +1.1 280.4 +1.62 255 +1.8 226 +2.105 210 +2.2 195 +2.45 80 +2.75 36 +3.1 0 +; +; CTI Pro54-1G 491 I218WT - 14A +I218WT 54 153 14-13-12-11-10-9-8-7-6-5-4 0.23 0.58 CTI + 0.01 12.222 + 0.022 129.788 + 0.047 215.926 + 0.072 250.846 + 0.079 208.36 + 0.11 233.968 + 0.188 249.1 + 0.436 263.651 + 0.783 258.994 + 1.195 235.714 + 1.614 201.375 + 1.834 191.481 + 1.964 183.915 + 2.074 178.095 + 2.143 179.841 + 2.172 87.884 + 2.188 50.053 + 2.217 18.624 + 2.252 0.0 +; +; CTI Pro38-4G 434 I223 Skidmark 14A +I223SK 38 302 5-7-9-11-14 0.266 0.494 CTI + 0.016 199.183 + 0.024 260.157 + 0.07 207.313 + 0.148 227.637 + 0.425 244.71 + 0.721 254.466 + 1.015 256.905 + 1.3 248.775 + 1.459 240.645 + 1.615 234.954 + 1.712 195.931 + 1.782 119.51 + 1.9 24.39 + 1.984 0.0 +; +; Pro29-6GXL 381I224-CL 15A +I224-CL 29 365 15-12-10-8-6 0.19669999999999999 0.37 CTI + 0.0080 357.455 + 0.02 433.079 + 0.111 343.833 + 0.229 318.938 + 0.479 295.922 + 0.836 277.133 + 1.022 269.618 + 1.097 233.919 + 1.233 117.899 + 1.294 93.004 + 1.39 62.003 + 1.667 26.774 + 1.692 17.38 + 1.7 0.0 +; +; +I236BS 38 245 17-14-12-10-8 0.20400000000000001 0.4 CTI + 0.028 290.772 + 0.042 313.594 + 0.049 267.95 + 0.053 253.58 + 0.072 245.973 + 0.095 256.961 + 0.127 262.033 + 0.153 266.259 + 0.243 268.795 + 0.338 269.64 + 0.454 270.486 + 0.633 266.259 + 0.753 262.878 + 0.89 256.116 + 1.01 251.89 + 1.119 247.663 + 1.277 236.675 + 1.353 231.603 + 1.453 227.377 + 1.525 225.686 + 1.555 195.257 + 1.581 158.91 + 1.618 119.183 + 1.685 89.598 + 1.729 56.633 + 1.743 36.347 + 1.766 21.977 + 1.81 0.0 +; +; Cesaroni I240 +; converted from TMT test stand data 2002 (www.tripoli.org) +; provided by ThrustCurve.org (www.thrustcurve.org) +I240 38 302 0 0.274624 0.503552 CTI + 0.043 265.317 + 0.131 320.903 + 0.221 314.148 + 0.310 312.413 + 0.399 313.564 + 0.488 314.335 + 0.577 321.117 + 0.667 325.923 + 0.755 327.040 + 0.844 326.831 + 0.933 324.348 + 1.023 321.063 + 1.111 317.446 + 1.200 308.301 + 1.290 300.612 + 1.379 293.536 + 1.468 283.358 + 1.556 273.832 + 1.646 259.708 + 1.735 190.662 + 1.824 124.130 + 1.912 60.875 + 2.002 26.967 + 2.092 7.636 + 2.181 2.296 + 2.271 0.000 +; +; Pro-38-4G White +I242-WH-15A 38 303 6-8-9-11-13 0.22480000000000003 0.5498999999999999 CTI + 0.015 241.029 + 0.035 272.691 + 0.063 286.148 + 0.094 277.045 + 0.184 265.567 + 0.299 262.797 + 0.403 262.797 + 0.537 266.359 + 0.734 269.921 + 0.884 271.504 + 1.049 269.921 + 1.223 265.567 + 1.384 260.422 + 1.61 249.34 + 1.727 243.008 + 1.865 235.092 + 1.954 231.135 + 2.0 220.844 + 2.088 155.541 + 2.164 93.008 + 2.211 43.536 + 2.278 10.29 + 2.345 3.958 + 2.402 0.0 +; +; Pro-29-6XGL White +I243-WH-13A 29 365 4-6-7-9-11-12 0.2121 0.3986 CTI + 0.016 443.392 + 0.03 416.3 + 0.061 365.419 + 0.082 331.718 + 0.122 317.181 + 0.174 303.304 + 0.268 298.018 + 0.367 295.374 + 0.514 294.714 + 0.701 290.749 + 0.808 280.837 + 0.968 266.96 + 1.058 247.797 + 1.105 224.009 + 1.155 207.489 + 1.178 202.203 + 1.206 167.181 + 1.254 158.59 + 1.297 154.626 + 1.336 132.819 + 1.395 109.692 + 1.486 69.383 + 1.574 25.771 + 1.649 6.608 + 1.692 0.0 +; +; CTI Pro38-5G 543 I297 Skidmark 15A +I297SM 38 360 6-8-10-12-15 0.329 0.591 CTI + 0.013 340.903 + 0.036 375.121 + 0.069 354.844 + 0.129 335.834 + 0.281 338.369 + 0.662 344.705 + 0.855 344.705 + 1.084 329.498 + 1.295 319.359 + 1.359 313.023 + 1.447 314.29 + 1.534 269.935 + 1.637 119.126 + 1.681 69.701 + 1.74 40.554 + 1.846 12.673 + 1.943 0.0 +; +; +I303BS 38 303 16-13-11-9-7 0.27 0.5 CTI + 0.035 415.763 + 0.053 402.352 + 0.054 329.705 + 0.072 324.117 + 0.109 348.705 + 0.18 353.175 + 0.28 357.646 + 0.432 354.293 + 0.557 353.175 + 0.684 348.705 + 0.886 337.528 + 1.054 325.234 + 1.212 310.705 + 1.371 299.528 + 1.475 292.823 + 1.519 277.176 + 1.542 245.882 + 1.568 204.529 + 1.609 149.764 + 1.639 108.411 + 1.757 50.294 + 1.827 22.353 + 1.887 0.0 +; +; +I360 38 367 15 0.3346 0.5963 CTI +0.08 555.5 +0.1 489.7 +0.13 448 +0.2 449 +0.4 483.7 +0.55 498 +0.6 494.9 +0.7 481.91 +0.8 457.9 +1 406.6 +1.2 344.4 +1.3 309.3 +1.4 182.2 +1.55 158.9 +1.6 101.8 +1.7 55.8 +1.77 0 +; +; Pro-54-3G White long Burn Plugged +J140-WH_LB-P 54 329 P 0.68 1.2798 CTI + 0.073 191.23 + 0.109 196.102 + 0.219 193.362 + 0.51 211.328 + 0.801 216.2 + 0.991 216.2 + 1.195 212.546 + 1.53 209.501 + 2.521 198.234 + 3.096 188.185 + 3.781 174.482 + 4.174 165.043 + 4.794 146.468 + 5.464 125.457 + 6.207 98.356 + 7.001 65.164 + 7.781 36.845 + 8.444 11.267 + 8.771 4.568 + 9.158 1.218 + 9.464 0.0 +; +; CTI Pro54-2G 683 I250 Skidmark 15A +J250SK 54 237 6-8-10-12-15 0.406 0.8300000000000001 CTI + 0.031 191.478 + 0.051 271.111 + 0.082 161.056 + 0.148 206.689 + 0.3 234.426 + 0.413 244.269 + 0.635 264.848 + 0.849 270.217 + 1.06 276.48 + 1.449 283.638 + 1.644 277.375 + 1.8 279.164 + 1.932 272.901 + 2.135 261.269 + 2.291 249.637 + 2.447 246.953 + 2.525 251.427 + 2.579 227.268 + 2.614 157.477 + 2.665 51.896 + 2.727 14.316 + 2.825 6.263 + 2.965 0.0 +; +; Pro-38-5G Green3 +J270-GR-13A 38 367 5-7-8-9-10-11 0.376 0.6548 CTI + 0.0080 194.095 + 0.022 192.747 + 0.061 279.461 + 0.114 287.548 + 0.229 289.345 + 0.311 289.345 + 0.382 292.041 + 0.478 294.288 + 0.587 296.534 + 0.701 297.882 + 0.828 301.926 + 0.981 300.128 + 1.116 299.679 + 1.233 296.085 + 1.323 293.389 + 1.488 289.795 + 1.594 287.099 + 1.676 287.548 + 1.701 293.838 + 1.75 286.65 + 1.797 290.244 + 1.868 280.359 + 1.956 275.866 + 2.052 276.316 + 2.126 265.982 + 2.181 224.198 + 2.234 163.094 + 2.292 97.946 + 2.359 49.872 + 2.428 15.276 + 2.5 0.0 +; +; Pro-38-5G White +J290-WH-15A 38 367 7-8-9-11-12-13 0.3815 0.6597999999999999 CTI + 0.015 334.565 + 0.028 364.116 + 0.037 379.42 + 0.061 391.557 + 0.083 379.42 + 0.107 372.559 + 0.169 355.145 + 0.289 343.536 + 0.381 341.425 + 0.588 337.203 + 0.803 334.565 + 1.011 330.871 + 1.256 324.538 + 1.498 321.372 + 1.684 312.929 + 1.805 306.069 + 1.844 301.319 + 1.89 269.129 + 1.942 243.272 + 1.979 223.747 + 2.043 156.201 + 2.128 118.734 + 2.192 86.016 + 2.279 35.356 + 2.334 15.831 + 2.402 0.0 +; +; CTI Pro54-2G 838 J293BS 13A +J293BS 54 237 13-12-11-10-9-8-7-6-5-4-3 0.41600000000000004 0.84 CTI + 0.019 22.847 + 0.032 250.277 + 0.044 386.32 + 0.06 302.202 + 0.073 256.508 + 0.13 285.586 + 0.266 309.471 + 0.487 318.818 + 0.734 325.049 + 1.432 324.01 + 1.786 309.471 + 2.074 294.933 + 2.33 280.394 + 2.488 273.124 + 2.58 272.086 + 2.634 258.585 + 2.713 163.044 + 2.795 70.618 + 2.852 20.77 + 2.896 0.0 +; +; Cesaroni J300 +; converted from TMT test stand data 2002 (www.tripoli.org) +; provided by ThrustCurve.org (www.thrustcurve.org) +J300 38 360 0 0.340032 0.606592 CTI + 0.043 357.026 + 0.131 436.586 + 0.221 407.925 + 0.310 399.528 + 0.400 400.588 + 0.490 406.733 + 0.578 414.302 + 0.667 417.117 + 0.756 418.415 + 0.846 421.302 + 0.935 422.229 + 1.025 415.951 + 1.114 406.356 + 1.202 395.237 + 1.292 381.728 + 1.381 369.861 + 1.471 355.451 + 1.560 331.691 + 1.649 246.243 + 1.738 161.766 + 1.827 109.478 + 1.917 71.413 + 2.006 37.058 + 2.096 13.880 + 2.185 5.059 + 2.275 0.000 +; +; +J357BS 38 367 17-14-12-10-8 0.337 0.601 CTI + 0.019 514.383 + 0.042 502.824 + 0.054 446.473 + 0.073 434.914 + 0.122 433.469 + 0.258 430.579 + 0.474 427.69 + 0.952 404.571 + 1.236 381.453 + 1.386 372.784 + 1.454 367.004 + 1.487 345.33 + 1.515 317.877 + 1.552 268.751 + 1.615 196.506 + 1.655 134.375 + 1.721 49.127 + 1.758 26.008 + 1.824 0.0 +; +; CTI Pro54-3G 1016 J3360 Skidmark 15A +J360SM-54mm 54 321 6-8-10-12-15 0.606 1.104 CTI + 0.017 560.653 + 0.058 287.423 + 0.167 328.23 + 0.358 363.715 + 0.538 374.36 + 0.85 397.425 + 1.163 400.973 + 1.458 400.973 + 1.733 395.651 + 1.983 381.457 + 2.271 356.618 + 2.496 340.65 + 2.592 351.295 + 2.646 289.198 + 2.679 172.099 + 2.725 86.937 + 2.804 19.516 + 2.904 5.323 + 2.975 0.0 +; +; Cesaroni J360 +; converted from TMT test stand data 2002 (www.tripoli.org) +; provided by ThrustCurve.org (www.thrustcurve.org) +J360-38mm 38 419 0 0.409024 0.709184 CTI + 0.041 618.905 + 0.124 616.584 + 0.207 563.785 + 0.291 557.730 + 0.374 558.409 + 0.457 562.088 + 0.541 561.267 + 0.624 563.219 + 0.708 565.328 + 0.793 566.558 + 0.876 549.383 + 0.959 529.633 + 1.043 511.099 + 1.126 483.285 + 1.209 445.397 + 1.293 421.658 + 1.377 378.330 + 1.461 261.647 + 1.545 197.445 + 1.628 146.570 + 1.711 101.807 + 1.795 78.039 + 1.878 47.847 + 1.961 31.861 + 2.046 9.220 + 2.130 0.000 +; 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+; Pro75-6G 7388-M2045-BS P +M2045-BS 75 893 P 3.739 6.071 CTI + 0.0040 556.851 + 0.019 1690.324 + 0.063 2359.204 + 0.153 2339.434 + 0.182 2570.083 + 0.247 2471.233 + 0.616 2497.593 + 1.028 2547.018 + 2.111 2316.369 + 2.551 2273.535 + 2.635 2253.765 + 2.796 1696.914 + 3.009 1472.855 + 3.349 247.123 + 3.541 108.734 + 3.587 0.0 +; +; AMX75-7600 6774-M2050-SK P +M2050-BS 75 1039 P 4.172 7.1290000000000004 CTI + 0.038 2152.81 + 0.833 2506.091 + 1.189 2539.211 + 1.546 2500.571 + 1.775 2415.011 + 1.907 2279.77 + 2.168 2086.569 + 2.401 1973.409 + 2.616 1909.929 + 2.776 1871.288 + 2.918 1203.365 + 3.056 706.563 + 3.309 135.241 + 3.4 0.0 +; +; Pro75-6G 6287M2075-SS Plugged +M2075-SS 75 893 P 4.5931 7.1913 CTI + 0.034 2350.685 + 0.18 2652.055 + 0.243 2931.507 + 0.303 2734.247 + 0.453 2624.658 + 0.552 2564.384 + 0.813 2487.671 + 1.172 2498.63 + 2.028 2038.356 + 2.415 1610.959 + 2.567 1506.849 + 2.69 1386.301 + 3.01 224.658 + 3.029 0.0 +; +; Pro-75-6GXL Skidmark Plugged +M2080-SK-P 75 1025 P 4.107 7.0395 CTI + 0.027 1813.539 + 0.04 2084.323 + 0.067 2344.418 + 0.097 2276.722 + 0.132 2262.47 + 0.172 2269.596 + 0.218 2319.477 + 0.323 2415.677 + 0.447 2490.499 + 0.541 2522.565 + 0.676 2547.506 + 0.816 2554.632 + 1.026 2522.565 + 1.23 2519.002 + 1.459 2461.995 + 1.669 2369.359 + 1.987 2241.093 + 2.21 2134.204 + 2.539 2002.375 + 2.63 1991.686 + 2.7 1941.805 + 2.746 1842.043 + 2.784 1692.399 + 2.811 1542.755 + 2.843 1339.667 + 2.999 883.61 + 3.083 520.19 + 3.177 277.91 + 3.271 128.266 + 3.365 53.444 + 3.443 24.941 + 3.5 0.0 +; +; Pro75-4G 5472M2250-CS P +M2250-CS 75 621 P 2.628 4.415 CTI + 0.016 2542.114 + 0.051 2390.798 + 0.139 2582.466 + 0.259 2599.278 + 0.877 2663.168 + 1.388 2555.565 + 1.823 2458.05 + 1.86 2303.371 + 1.891 1926.761 + 1.997 1452.637 + 2.195 1452.637 + 2.244 1207.168 + 2.276 645.616 + 2.336 517.838 + 2.414 144.591 + 2.456 40.351 + 2.497 0.0 +; +; Pro75-5G 6118M3100-WT P +M3100-WT 75 757 P 2.95 5.018 CTI + 0.02 3118.031 + 0.057 2976.886 + 0.148 3186.465 + 0.496 3391.768 + 0.817 3665.504 + 0.936 3532.913 + 1.173 3357.551 + 1.501 3199.297 + 1.717 3139.417 + 1.78 2412.304 + 1.812 2130.013 + 1.832 2031.639 + 1.937 346.448 + 1.985 81.266 + 2.0 0.0 +; +; Pro98-4G 9994M3400-WT P +M3400-WT 98 702 P 4.766 8.108 CTI + 0.021 3639.453 + 0.049 3360.146 + 0.111 3300.899 + 0.374 3478.64 + 0.909 3774.874 + 1.059 3897.6 + 1.208 3884.904 + 1.571 3787.57 + 2.168 3402.465 + 2.467 3245.884 + 2.709 3292.435 + 2.734 3254.348 + 2.821 1032.589 + 2.876 550.15 + 2.93 165.045 + 2.99 0.0 +; +; Pro75-6G 6800M3700-WT Plugged +; 5.3G case or 6G + 0.7 spacer +M3700-WT 75 803 P 3.1065 5.7785 CTI + 0.017 3815.753 + 0.04 3969.863 + 0.099 3914.384 + 0.245 3957.534 + 0.563 3951.37 + 0.727 4105.479 + 0.959 4031.507 + 1.25 3982.192 + 1.511 3994.521 + 1.595 3994.521 + 1.739 1306.849 + 1.772 1109.589 + 1.83 221.918 + 1.835 0.0 +; +; Pro98 6G 10347 N10000-VM P +N10000-VM 98 1010 P 5.335 9.9185 CTI + 0.0090 8953.955 + 0.027 10257.379 + 0.074 10753.247 + 0.125 11036.6 + 0.212 11107.438 + 0.358 11277.45 + 0.457 11475.797 + 0.548 11461.629 + 0.599 11277.45 + 0.663 10866.588 + 0.766 9988.194 + 0.837 9350.649 + 0.888 8996.458 + 0.908 8968.123 + 0.923 8585.596 + 0.942 7820.543 + 0.961 6276.269 + 0.976 4491.145 + 0.988 3357.733 + 1.004 1657.615 + 1.008 0.0 +; +; Pro98 4G 10367 N1800-WH Plugged +N1800-WH-P 98 702 P 4.8420000000000005 9.18 CTI + 0.077 1769.444 + 0.123 2205.556 + 0.193 2041.667 + 0.339 1988.889 + 0.744 1994.444 + 2.398 2144.444 + 2.726 2119.444 + 2.977 2077.778 + 3.933 1786.111 + 4.643 1525.0 + 4.986 1444.444 + 5.152 1352.778 + 5.225 1261.111 + 5.348 994.444 + 5.437 738.889 + 5.541 622.222 + 5.73 355.556 + 5.915 75.0 + 5.931 0.0 +; +; Pro98 6G 14272 N1975-GR P +N1975-GR 98 1010 P 8.584 13.2475 CTI + 0.04 1382.46 + 0.08 1699.147 + 0.201 1781.364 + 0.447 1793.544 + 0.678 1820.95 + 0.758 1927.527 + 0.853 1842.266 + 2.425 2088.916 + 2.52 2180.268 + 2.761 2198.538 + 3.434 2213.764 + 3.715 2268.575 + 4.077 2299.026 + 4.96 2238.124 + 5.492 2161.998 + 6.105 2024.97 + 6.446 1878.806 + 6.647 1668.697 + 7.074 602.923 + 7.239 140.073 + 7.254 0.0 +; +; Pro98 6G 15227 N2501-WH Plugged +N2501-WH-P 98 1010 P 8.704 13.308 CTI + 0.039 1715.546 + 0.059 2835.722 + 0.141 3488.423 + 0.224 3188.534 + 0.373 3135.612 + 2.237 2998.897 + 2.905 2928.335 + 3.45 2769.57 + 3.462 2787.211 + 4.537 2407.938 + 4.804 1949.283 + 5.165 1684.675 + 5.511 1181.918 + 6.013 313.12 + 6.088 0.0 +; +; Pro98-6G 11077N2600-SK P +N2600-SK 98 1010 P 6.7700000000000005 11.482000000000001 CTI + 0.063 2794.141 + 0.199 2497.593 + 0.485 2619.507 + 0.907 2777.666 + 1.367 2902.875 + 1.749 2949.005 + 2.051 2972.07 + 2.764 2817.206 + 3.549 2392.154 + 3.767 2309.779 + 3.958 2385.564 + 4.177 639.226 + 4.265 138.389 + 4.297 0.0 +; +; Pro98-6G 13767N2850-BS P +N2850-BS 98 1010 P 6.965 11.688 CTI + 0.0030 286.922 + 0.085 3152.414 + 0.185 3103.973 + 0.322 3077.889 + 0.945 3212.034 + 1.725 3312.643 + 2.819 3118.878 + 4.163 2776.062 + 4.376 1982.369 + 4.538 845.86 + 4.763 435.972 + 4.849 149.05 + 4.9 0.0 +; +; Pro98-6GXL 17613N2900-CL P +N2900-CL 98 1239 P 8.788 14.166 CTI + 0.026 1863.57 + 0.074 3605.399 + 0.122 4022.127 + 0.361 3619.446 + 1.18 3497.706 + 1.981 3586.67 + 3.493 3155.895 + 4.648 2874.955 + 4.939 2322.439 + 5.205 1648.183 + 5.629 945.832 + 5.972 430.775 + 6.219 206.023 + 6.278 149.835 + 6.296 0.0 +; +; Pro98-6GXL 14263N3400-SK P +N3400-SK 98 1239 P 8.471 13.972 CTI + 0.055 3602.205 + 0.177 3060.167 + 0.608 3397.34 + 1.537 3811.337 + 2.252 3973.522 + 2.86 3760.121 + 3.152 3597.937 + 3.545 3346.124 + 3.71 3627.813 + 3.837 2868.106 + 3.884 1907.803 + 3.999 1510.877 + 4.188 273.153 + 4.28 81.092 + 4.3 0.0 +; +; Pro98-6GXL 17631N3800-BS P +N3800-BS 98 1239 P 8.71 14.261000000000001 CTI + 0.016 2671.724 + 0.069 4632.012 + 0.159 4360.745 + 0.293 4355.626 + 1.11 4591.066 + 1.48 4703.667 + 1.847 4729.258 + 2.384 4683.194 + 2.628 4550.12 + 3.141 4135.542 + 3.343 4043.413 + 3.434 4022.94 + 3.497 3787.501 + 3.582 3204.021 + 3.681 2809.916 + 3.853 2385.102 + 4.042 1458.7 + 4.198 972.467 + 4.338 946.875 + 4.401 864.983 + 4.604 378.75 + 4.673 230.321 + 4.7 0.0 +; +; Pro98-6GXL 17790N4100-RL P +N4100-RL 98 1293 P 9.38 14.748000000000001 CTI + 0.0030 203.877 + 0.05 2362.879 + 0.078 3946.845 + 0.121 4281.412 + 0.652 4370.281 + 1.123 4453.923 + 1.655 4772.807 + 2.353 4621.206 + 3.035 4511.427 + 3.7 4375.509 + 3.733 4182.087 + 3.887 2969.282 + 4.036 1589.193 + 4.197 533.216 + 4.262 240.47 + 4.3 0.0 +; +; Pro98-6GXL 20146N5800-CS P +N5800-CS 98 1239 P 9.425 14.826 CTI + 0.019 6694.9 + 0.049 6720.292 + 0.103 6593.334 + 0.384 6677.973 + 1.109 6957.279 + 1.569 6940.352 + 1.991 6720.292 + 2.622 6009.329 + 3.011 3275.507 + 3.192 2606.864 + 3.334 1599.666 + 3.423 1041.053 + 3.513 389.337 + 3.581 220.06 + 3.594 0.0 +; +; Pro-150-40K Skidmark Plugged +O3700-SK-P 161 957 P 17.157 31.3505 CTI + 0.052 1009.021 + 0.071 1646.907 + 0.084 2505.155 + 0.09 3183.634 + 0.116 3409.794 + 0.187 3114.046 + 0.245 3050.258 + 0.316 3108.247 + 0.445 3241.624 + 0.594 3461.985 + 0.819 3653.351 + 1.155 3676.546 + 1.503 3775.129 + 2.471 3931.701 + 3.277 4012.887 + 4.213 4030.284 + 4.787 3983.892 + 5.206 3925.902 + 5.671 3867.912 + 5.981 3850.515 + 6.413 3751.933 + 6.923 3618.557 + 7.387 3496.778 + 7.645 3363.402 + 7.819 3102.448 + 7.903 2905.284 + 7.942 2383.376 + 7.981 1948.454 + 8.026 1310.567 + 8.084 695.876 + 8.135 359.536 + 8.187 162.371 + 8.277 81.186 + 8.387 0.0 +; +; +O4900-BS 161 957 0 18.898 32.648 CTI +0.06 800 +0.1 4000 +0.15 5500 +0.25 5160 +0.45 5130 +0.8 5400 +1 5300 +2 5450 +3 5347 +4 5160 +5 4950 +6 4700 +6.8 4400 +7.05 4400 +7.3 3800 +7.6 300 +7.8 0 +; +; +H186RT 38 248 18 0.1765 0.469 GM +0.008 40.184 +0.042 133.634 +0.058 178 +0.1 196.9 +0.192 204 +0.483 215 +0.842 220.33 +1.075 219 +1.267 219 +1.35 207 +1.42 165 +1.48 118.949 +1.542 75 +1.69 0 +; +; +H225BL 38 248 1000 0.182001 0.474999 GM +0.0150659 113.792 +0.0326428 193.101 +0.0489642 172.412 +0.166981 256.893 +0.310107 296.548 +0.512241 303.445 +0.617702 305.169 +0.838669 298.272 +0.898933 291.376 +0.98 266.893 +1.02 244.652 +1.05 222.411 +1.26303 10.3447 +1.3 0 +; +; +I223GT 38 248 18 0.182 0.475 GM +0.02 170 +0.05 190 +0.141038 225 +0.462292 255 +0.681685 258 +0.887365 260 +1.14789 255 +1.32419 224.138 +1.40451 129.31 +1.48 0 +; +; +I324RT 38 369 1000 0.298 0.688 GM +0.015 238.506 +0.09 310 +0.25 360 +0.65 365 +1.06758 369.24 +1.25563 365 +1.35 340 +1.48678 195.402 +1.65 0 +; +; +I389GT 38 369 18 0.3026 0.6928 GM +0.016 181.961 +0.025 277.057 +0.045 379.719 +0.065 413.405 +0.366 450 +0.683 454.85 +1.066 443.265 +1.14398 421 +1.183 385 +1.241 280.84 +1.35 92.872 +1.42 0 +; +; +J485WC 54 326 1000 0.549 1.1648 GM +0.05 263.913 +0.095 401.808 +0.15 444.822 +0.503226 544.253 +0.8 573.821 +1.075 569.372 +1.5 542.683 +2 444.822 +2.1 311.376 +2.19 0 +; +; +K1185GT 54 728 1000 1.314 2.541 GM +0.01 575 +0.06 810 +0.12 1050 +0.17 1175 +0.68 1345 +0.82 1366.15 +0.92 1379 +1.65 1290.5 +1.8 1268.25 +1.85 1223.75 +1.87 1068 +1.92 801 +2.05 222.5 +2.1 0 +; +; +K630WC 54 430 1000 0.731999 1.4533 GM +0.042 359.461 +0.05 440.908 +0.075 556.028 +0.15 622.751 +0.217 667.233 +0.9 800.68 +1.159 796.232 +1.33871 778.439 +1.517 720.612 +1.9 556.028 +2.1 133.447 +2.24 0 +; +; +K805WC 54 492 1000 0.887499 1.73965 GM +0.025 423.515 +0.0403226 667.233 +0.067 702.819 +0.095 747.301 +0.551613 1000.85 +0.8 1089.81 +1.25 1067.57 +1.75 667.233 +2.19 0 +; +; +L1065BL 75 787 1000 2.693 5.329 GM +0.02 1334.47 +0.1 1312.23 +0.65 1779.29 +1.75 1757.05 +2.2 1245.5 +2.75 667.233 +3.5 222.411 +3.95 0 +; +; +L1150WC 75 497 1000 1.75 3.502 GM +0.1 1000.85 +0.2 1067.57 +0.5 1178.78 +1.25 1668.08 +1.5 1757.05 +1.7 1734.81 +2 1334.47 +2.25047 982.747 +2.5 711.716 +2.75 556.028 +3 266.893 +3.11 0 +; +; +L789RT 75 497 1000 1.8 3.378 GM +0.05 600 +0.1 650 +0.2 712 +0.754163 850 +1.5 900 +2 906 +3.41332 867.816 +3.55 833.333 +3.92752 344.828 +4.17 0 +; +; +L985GT 75 497 1000 1.875 3.453 GM +0.2 725 +0.3 795.5 +0.75 950 +1.5 1120 +2 1120 +3.4 1112.5 +3.6 0 +; +; +M1355RT 75 787 1000 2.831 5.216 GM +0.05 1334.47 +0.85 1779.29 +1.35 1868.25 +1.7 1890.49 +2.15 1859.36 +3.5 489.304 +3.81 0 +; +; +M1610BL 75 1039 1000 3.674 6.918 GM +0.0627746 1560.33 +1.3 2135.15 +1.64783 2206.87 +1.79535 2206.87 +1.89893 2189.63 +1.98996 2155.15 +2.50157 1715.5 +2.82486 1474.12 +2.99435 1241.36 +3.29253 594.82 +3.5 355.858 +3.71 0 +; +; +M1665WC 75 787 1000 2.95 5.579 GM +0.075 2068.42 +0.125 2001.7 +0.7 2224.11 +0.85 2268.59 +1.6 2268.59 +2.12 1801.53 +2.65 1178.78 +3.22 444.822 +3.42 0 +; +;Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve +;Tracer program. Thrust curve and engine data TRA certification dated Oct 14, +;2008. +G135R 29 206 6-10-14 0.0799995 0.226 KBA +0.011 156.916 +0.016 63.461 +0.027 98.191 +0.061 109.872 +0.094 111.135 +0.14 116.187 +0.197 127.553 +0.26 135.13 +0.316 139.235 +0.354 141.445 +0.408 147.128 +0.459 149.022 +0.502 153.443 +0.546 156.6 +0.6 158.178 +0.684 155.968 +0.743 152.811 +0.816 149.97 +0.875 148.075 +0.91 146.812 +0.963 151.232 +0.981 152.18 +0.993 149.022 +1.014 103.558 +1.02 61.251 +1.034 22.732 +1.039 7.893 +1.049 0 +; +;Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve +;Tracer program. Thrust curve and engine data TRA certification dated Oct 14, +;2008. +G82W 29 206 6-10-14 0.0839996 0.231 KBA +0.011 50.341 +0.028 53.498 +0.055 76.3 +0.068 80.159 +0.111 74.02 +0.134 74.02 +0.216 79.458 +0.295 83.667 +0.374 89.982 +0.406 91.911 +0.431 89.631 +0.453 92.437 +0.474 93.841 +0.489 91.385 +0.519 93.314 +0.551 90.333 +0.604 91.911 +0.642 92.262 +0.728 94.367 +0.79 96.647 +0.85 98.401 +0.905 99.453 +0.954 101.734 +0.995 102.962 +1.025 103.839 +1.076 102.435 +1.112 102.435 +1.142 102.26 +1.174 98.576 +1.221 95.244 +1.238 93.49 +1.274 98.226 +1.287 89.631 +1.317 87.877 +1.351 85.597 +1.434 81.913 +1.479 78.581 +1.503 73.845 +1.533 65.075 +1.565 50.516 +1.594 36.835 +1.62 28.591 +1.65 21.048 +1.701 14.208 +1.737 8.946 +1.829 5.613 +1.883 4.385 +1.959 0 +; +;Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve +;Tracer program. Thrust curve and engine data TRA certification dated Oct 14, +;2008. +H130W 29 291 6-10-14 0.140001 0.708999 KBA +0.016 154.848 +0.024 194.715 +0.055 224.09 +0.071 201.848 +0.078 227.027 +0.089 183.384 +0.123 172.054 +0.196 172.054 +0.254 176.67 +0.348 179.607 +0.426 180.866 +0.481 179.188 +0.554 178.348 +0.649 166.179 +0.672 165.339 +0.777 172.473 +0.86 172.893 +0.947 171.634 +1.038 167.018 +1.138 161.143 +1.185 157.366 +1.232 152.75 +1.266 143.098 +1.294 119.598 +1.326 101.134 +1.412 70.08 +1.53 46.58 +1.647 32.732 +1.674 29.375 +1.718 17.625 +1.838 12.17 +1.909 0 +; +; KBA I301W +I301W 38 369.6 18 0.295031 0.724 KBA + 0.0080 266.093 + 0.014 327.114 + 0.03 354.124 + 0.058 350.122 + 0.107 335.117 + 0.133 326.114 + 0.189 326.114 + 0.217 333.116 + 0.237 383.134 + 0.253 402.14 + 0.287 395.138 + 0.33 381.133 + 0.72 381.133 + 1.035 341.119 + 1.437 317.111 + 1.57 262.092 + 1.698 130.045 + 1.789 83.029 + 1.833 74.026 + 1.867 53.019 + 1.893 23.008 + 1.916 13.005 + 1.952 0.0 +; +;KBA I550R +I550R 38 369.6 20 0.294999 0.712999 KBA +0.016 156.054 +0.028 278.097 +0.04 427.149 +0.054 550.192 +0.08 542.189 +0.245 588.205 +0.332 611.213 +0.424 631.22 +0.496 638.223 +0.613 644.225 +0.71 643.225 +0.758 631.22 +0.846 603.211 +0.894 613.214 +0.915 611.213 +0.939 586.205 +0.949 546.191 +0.959 505.176 +0.969 469.164 +0.983 381.133 +0.999 278.097 +1.011 200.07 +1.029 112.039 +1.053 42.015 +1.069 15.005 +1.089 0 +; +; +K1750R 54.0 728.00 0 1.25300 2.56000 KBA + 0.02 1309.09 + 0.03 1679.77 + 0.05 1736.54 + 0.11 1689.79 + 0.26 1799.99 + 0.40 1913.54 + 0.46 1896.84 + 0.68 2023.74 + 0.90 2133.94 + 0.95 2097.21 + 1.00 2050.46 + 1.05 1920.21 + 1.10 1793.31 + 1.16 1676.43 + 1.21 1719.85 + 1.25 1526.15 + 1.27 1302.41 + 1.32 874.95 + 1.35 454.17 + 1.36 317.25 + 1.37 200.37 + 1.40 90.17 + 1.46 0.00 +; +; Kosdon by Aerotech K750 White Lightning. +K750W 54 728 0 1.315 2.62 KBA + 0.0080 266.075 + 0.012 457.102 + 0.02 750.467 + 0.032 999.485 + 0.044 1112.055 + 0.06 1180.279 + 0.095 1098.41 + 0.127 1057.476 + 0.163 1040.42 + 0.334 1050.653 + 0.62 1054.064 + 0.998 975.607 + 1.324 907.382 + 1.69 903.971 + 2.06 886.915 + 2.184 828.924 + 2.299 757.289 + 2.394 651.541 + 2.502 556.028 + 2.609 450.28 + 2.784 327.476 + 2.999 245.607 + 3.039 201.261 + 3.134 92.103 + 3.206 40.935 + 3.337 6.822 + 3.468 0.0 +; +; KBA M1450W +M1450W 75 1038.9 0 4.15 7.6000000000000005 KBA + 0.035 1842.929 + 0.076 2287.088 + 0.146 1968.884 + 0.215 1882.704 + 0.291 1836.299 + 0.499 1862.816 + 1.005 1935.738 + 1.559 1889.333 + 2.155 1816.412 + 2.862 1750.119 + 3.493 1663.939 + 3.853 1358.994 + 4.221 1060.678 + 4.484 788.88 + 4.761 523.71 + 4.942 258.54 + 5.323 258.54 + 5.6 172.36 + 5.801 119.326 + 5.96 0.0 +; +;@File: 070616w11.txt, @Pts-I: 1207, @Pts-O: 32, @Sm: 5, @CO: 5% +;@TI: 5460.0, @TIa: 5447.69, @TIe: 0.0%, @ThMax: 3102.43, @ThAvg: 2675.68, @Tb: 2.036 +;Exported using ThrustCurveTool, www.ThrustGear.com +M2900R 75 1039 1000 3.755 7.195 KBA +0 2.43719 +0.034 19.468 +0.05 69.6872 +0.052 166.128 +0.056 533.998 +0.06 1067.23 +0.064 1683.24 +0.066 1897.53 +0.072 2294.77 +0.082 2495.75 +0.102 2708.42 +0.108 2734.74 +0.204 2696.52 +0.438 2690.17 +0.726 2744.74 +0.824 2794 +1.1159 3041.86 +1.3179 3102.43 +1.5659 3015.86 +1.8159 2846.44 +1.8639 2744.09 +1.8979 2565.3 +1.9079 2455.92 +1.9599 1357.39 +1.9879 857.187 +2.0059 603.283 +2.0259 417.576 +2.0439 303.914 +2.0899 150.616 +2.1419 73.2216 +2.2259 25.6056 +2.4119 0 +; +; +G69-SF 38 127 0 0.0630011 0.240001 LR +0.01 97.9215 +0.2 96.5358 +0.4 94.2263 +0.799544 76.6744 +1.2 58.1986 +1.6 0 +; +; +J350-SF 54 327 0 0.59 1.26 LR +0.02 325.858 +0.5 397.098 +1 457.784 +1.5 447.23 +2 415.567 +2.2 401.055 +2.5 48.8127 +2.7 0 +; +; +K690-SF 54 498 0 0.95 1.8 LR +0.01 643.799 +0.25 688.654 +0.5 730.871 +0.749636 770.449 +1 807.388 +1.25 796.834 +1.5 762.533 +1.75 733.509 +2 696.57 +2.25 659.631 +2.35 0 +; +; +K830-SF 54 726 0 1.4 2.4 LR +0.02 670.185 +0.5 775.726 +1 886.544 +1.5 986.807 +2 1092.35 +2.5 1187.34 +2.7 0 +; +; +L480-LR 75 498 1000 1.814 3.538 LR +0.02 419.525 +1 509.235 +2 551.451 +3 567.282 +4 564.644 +5 522.427 +6 401.055 +6.4 0 +; +; +L780-SF 76 498 0 1.8 3.5 LR +0.02 506.596 +0.5 696.57 +1 844.327 +1.5 897.098 +2 934.037 +2.5 918.206 +3 865.435 +3.5 802.111 +3.8 0 +; +; +M1200-SF 76 785 0 2.968 5.368 LR +0.02 1018.47 +0.5 1203.17 +1 1303.43 +1.5 1398.42 +2 1514.51 +2.5 1498.68 +3 1408.97 +3.5 1203.17 +4 411.609 +4.25 89.7098 +4.5 0 +; +; +M3000-LW 76 1038 P 4.064 6.857 LR +0.083333 3234.3980 +0.166666 3626.9781 +0.333333 4104.8876 +0.5 4045.3220 +0.666667 3824.0989 +0.833333 3649.3737 +1.0 3669.9088 +1.166667 3815.3653 +1.333333 3859.8580 +1.5 3781.1602 +1.666667 3626.9781 +1.833333 3434.5774 +2.0 3093.3818 +2.166667 2643.3598 +2.333333 2052.4438 +2.416667 950.4439 +2.5 846.5966 +2.666667 764.3097 +2.833333 718.9958 +2.916667 718.7712 +3.0 542.0856 +3.166667 410.3503 +3.333333 272.3106 +3.5 0 +; +; +M900-LR 75 785 1000 3.13 5.53 LR +0.02 807.388 +1 992.084 +2 1050.13 +3 1060.69 +4 992.084 +5 923.483 +5.5 591.029 +6 0 +; +; +N3800-LW 98 1016 1000 6.125 11.6 LR +0.01 4780.6 +0.5 4572.75 +1 4688.22 +1.5 4965.36 +2 3972.29 +2.5 3002.31 +3 1986.14 +3.25 0 +; +; Loki Research EX P9381 +P9381 152 2362 0 34.641 57.368 LR-EX +0.25 12185.3 +3.5 13368.3 +5.60 9582.61 +6.25 5323.67 +7.8 354.911 +8.0 0.0 +; +; Loki Research EX P4935 +; From RLK test stand data. +; Created by RL Kinsel. +P4935 152 1829 0 30.0105 51.9196 LR-EX + 0.010 3885.74 + 0.025 3998.33 + 0.050 4117.14 + 1.000 4343.65 + 2.000 4627.11 + 3.000 5123.29 + 4.000 5425.44 + 5.000 5660.40 + 6.000 5825.16 + 7.000 5913.61 + 8.000 5924.29 + 9.000 5864.21 + 9.370 5825.05 + 9.380 4427.75 + 10.000 4366.79 + 10.180 4344.98 + 10.190 3079.40 + 11.920 3079.40 + 11.930 0.00000 +; +; Derek Deville DEAP EX Q Motor. +; Flown in Deville Qu8k rocket to 121,478 ft +; on September 30, 2011. +; Exported from BurnSim 3.1 (www.burnsim.com) +Q18000 203 2438 0 72.515 115.696 DEAP-EX + 0.01 13861.433 + 0.28 14083.922 + 0.55 14316.859 + 0.82 14559.743 + 1.09 14812.149 + 1.36 15073.716 + 1.63 15344.132 + 1.9 15623.138 + 2.17 15910.506 + 2.44 16206.047 + 2.71 16509.592 + 2.98 16821 + 3.25 17140.156 + 3.52 17026.282 + 3.79 16901.881 + 4.06 16778.066 + 4.33 16654.833 + 4.6 16532.181 + 4.87 16410.112 + 5.14 16363.243 + 5.41 16443.846 + 5.68 16602.704 + 5.95 16814.786 + 6.22 17065.827 + 6.49 17346.975 + 6.76 17652.39 + 7.03 17978.053 + 7.3 18321.091 + 7.57 18679.403 + 7.84 19051.404 + 8.11 19435.888 + 8.38 19831.92 + 8.65 3928.48 + 8.92 2525.882 + 9.19 1559.617 + 9.46 838.016 + 9.73 279.483 + 10 0 +; +; Prototype M685W, new Aerotech 75mm Moonburner. +; Flown as upper stage on AeroPac Team two stage +; rocket to 104,659 ft on September 11, 2012. +; Won the Carmack Prize. +; Thrust curve different than standard production +; M685W Moonburner. +M685W-Proto 75 879.3 0 4.436 6.954 AT +0.255639 1066.85 +0.631579 876.987 +1.32331 1012.6 +3.5188 1128.33 +4.81203 1048.77 +6.19549 867.946 +7.21805 560.548 +7.54887 488.219 +7.89474 343.562 +8.27068 216.986 +8.99248 162.74 +9.60902 72.3288 +9.61 0.0 +; +; Boosted Dart (Zero Thrust) +Dart 1 1 0 0.01 0.02 NoThrust +0.01 0.01 +0.02 0.01 +0.03 0.0 +; +;@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 +N1000W 98 1046 1000 7.925 12.777 AT +0 0.457288 +0.152 0.314574 +0.162 40.2069 +0.164 148.395 +0.168 598.904 +0.172 890.058 +0.176 995.096 +0.178 1158.03 +0.182 1342.31 +0.19 1556.72 +0.222 1959.8 +0.234 2050.53 +0.254 2111.01 +0.308 2119.9 +0.356 2073.29 +0.47 2091.07 +0.528 1989.54 +0.582 1825.83 +0.648 1733.53 +0.782 1658.07 +0.892 1701.72 +0.914 1633.23 +0.966 1669.56 +1.7839 1594.08 +1.8239 1551.16 +3.1999 1533.43 +5.4538 1378.99 +6.9577 1170.93 +10.9216 424.692 +13.5895 106.05 +14.6754 12.6091 +16.1354 0 +; +; L1040 Dark Matter +L1040DM-P 75 681 1000 2.602 4.7170000000000005 AT + 0.018 1126.167 + 0.042 1036.413 + 0.053 1002.543 + 0.116 988.995 + 0.504 1049.961 + 0.794 1095.685 + 1.002 1146.489 + 1.252 1192.213 + 1.499 1237.937 + 1.753 1261.646 + 1.912 1268.42 + 2.095 1254.872 + 2.511 1134.635 + 2.772 1056.734 + 3.012 966.98 + 3.153 933.11 + 3.217 863.677 + 3.291 817.953 + 3.34 758.681 + 3.488 438.613 + 3.552 284.505 + 3.598 220.153 + 3.657 167.655 + 3.746 118.544 + 3.88 42.337 + 3.996 6.774 + 4.127 0.0 +; +; M1075 Dark Matter +M1075DM 98 597 1000 3.846 6.971 AT + 0.02 927.501 + 0.112 988.073 + 0.26 1033.501 + 0.53 1080.823 + 0.897 1124.359 + 1.509 1198.18 + 1.998 1239.823 + 2.355 1260.644 + 2.503 1264.43 + 2.773 1237.93 + 2.997 1222.787 + 3.502 1162.216 + 4.001 1063.787 + 4.501 906.68 + 4.741 834.751 + 4.878 742.001 + 4.96 664.394 + 5.062 448.608 + 5.164 223.357 + 5.26 79.5 + 5.352 30.286 + 5.5 0.0 +; +; M1305 Metalstorm +M1305M 98 597 1000 4.08 7.098 AT + 0.016 1288.076 + 0.043 1462.78 + 0.08 1370.986 + 0.407 1622.679 + 0.535 1640.446 + 0.787 1705.59 + 0.985 1693.745 + 1.13 1717.434 + 1.328 1693.745 + 1.349 1927.672 + 1.397 1726.317 + 1.751 1711.512 + 2.018 1687.823 + 2.275 1690.784 + 2.297 1892.139 + 2.318 1678.94 + 2.929 1412.441 + 3.748 1113.371 + 4.24 906.095 + 4.503 802.456 + 4.717 663.285 + 4.813 538.919 + 4.92 387.903 + 5.027 245.771 + 5.166 145.094 + 5.263 79.95 + 5.386 32.572 + 5.498 23.689 + 5.707 0.0 +; +; M685W-PS Moonburner +M685W-PS 75 936 P 4.32 7.008 AT + 0.083 1333.469 + 0.13 1368.376 + 0.249 1361.395 + 0.308 1380.012 + 0.403 1359.068 + 0.675 1184.53 + 1.018 1072.826 + 1.456 996.029 + 1.977 958.794 + 2.995 914.578 + 3.99 856.399 + 4.985 781.929 + 5.494 730.732 + 5.991 679.534 + 7.258 542.231 + 7.862 463.107 + 8.015 456.125 + 8.998 330.458 + 9.993 207.118 + 10.514 137.303 + 11.496 34.908 + 11.994 0.0 +; +; M1780NT Redesign and recert +M1780NT-PS 75 665 P 2.46 4.649 AT + 0.014 1112.055 + 0.015 1497.932 + 0.022 1783.542 + 0.036 2105.612 + 0.047 2157.265 + 0.066 2169.419 + 0.104 2123.843 + 0.14 2108.651 + 0.164 2135.996 + 0.197 2129.92 + 0.238 2157.265 + 0.263 2205.88 + 0.274 2169.419 + 0.312 2145.112 + 0.411 2111.689 + 0.595 2081.305 + 0.899 2075.228 + 1.299 2047.883 + 1.601 1996.23 + 1.899 1938.5 + 2.058 1889.886 + 2.201 1813.926 + 2.3 1753.158 + 2.423 1701.505 + 2.467 1622.506 + 2.508 1555.662 + 2.566 1336.897 + 2.62 1112.055 + 2.67 893.29 + 2.724 668.448 + 2.755 568.181 + 2.812 486.144 + 2.9 267.379 + 2.999 75.96 + 3.029 0.0 +; +;G80 New Blue Thunder +G80NBT 29 123.825 4-7-10 0.069 0.129 AT +0.013 89.054 +0.018 101.584 +0.029 105.388 +0.047 102.927 +0.104 100.018 +0.19 102.255 +0.268 104.94 +0.306 104.269 +0.352 105.835 +0.41 104.94 +0.432 106.73 +0.512 105.612 +0.563 106.954 +0.591 104.493 +0.62 106.283 +0.715 103.15 +0.76 103.374 +0.806 101.36 +0.848 102.032 +1.2 88.383 +1.243 77.866 +1.269 57.952 +1.302 44.079 +1.329 34.011 +1.367 26.403 +1.398 22.823 +1.433 20.585 +1.48 21.704 +1.508 20.809 +1.584 13.201 +1.604 11.635 +1.652 11.188 +1.683 5.37 +1.701 0 +; +; +H195NBT 29 203.2 10 0.115 0.197 AT + 0.003 178.052 + 0.005 224.131 + 0.013 252.516 + 0.019 256.571 + 0.022 248.461 + 0.058 239.614 + 0.1 240.351 + 0.199 235.559 + 0.255 228.555 + 0.285 227.449 + 0.301 230.767 + 0.399 223.025 + 0.5 223.025 + 0.603 220.445 + 0.774 217.127 + 0.802 211.598 + 0.899 201.644 + 0.961 180.632 + 0.999 169.942 + 1.023 161.094 + 1.054 155.196 + 1.101 69.304 + 1.169 0.0 +; +; AT I140W DMS +I140W 38 202.7 14-12-10-8-6 0.183 0.356 AT + 0.011 96.257 + 0.024 80.214 + 0.049 160.428 + 0.062 144.02 + 0.114 160.428 + 0.159 164.074 + 0.238 174.647 + 0.314 173.918 + 0.419 179.023 + 0.627 178.293 + 0.835 176.835 + 0.943 177.2 + 1.146 164.803 + 1.349 148.76 + 1.459 141.103 + 1.562 131.259 + 1.773 113.393 + 2.192 83.86 + 2.295 67.088 + 2.395 37.555 + 2.435 31.356 + 2.47 20.418 + 2.478 0.0 +; +; I280DM DMS +I280DM 38 356.4 14-12-10-8-6 0.355 0.616 AT + 0.016 342.389 + 0.048 297.021 + 0.111 316.16 + 0.173 328.211 + 0.202 327.502 + 0.261 322.54 + 0.334 311.907 + 0.498 310.489 + 0.602 308.363 + 0.705 307.654 + 0.802 310.489 + 0.902 310.489 + 1.0 306.236 + 1.025 316.869 + 1.057 309.072 + 1.1 308.363 + 1.139 317.578 + 1.205 307.654 + 1.298 304.109 + 1.336 316.16 + 1.4 299.856 + 1.5 296.312 + 1.55 298.438 + 1.595 306.945 + 1.634 295.603 + 1.652 280.716 + 1.716 253.07 + 1.743 224.006 + 1.8 153.827 + 1.9 62.381 + 1.97 20.558 + 1.971 0.0 +; +; J270W DMS +J270W 38 356.4 14-12-10-8-6 0.381 0.642 AT + 0.007 367.585 + 0.02 325.124 + 0.074 353.027 + 0.136 329.977 + 0.176 343.928 + 0.273 324.518 + 0.33 342.715 + 0.357 326.338 + 0.399 330.584 + 0.473 310.567 + 0.553 325.731 + 0.734 340.895 + 0.744 357.273 + 0.761 315.419 + 0.788 337.256 + 0.897 340.895 + 1.009 333.617 + 1.053 354.24 + 1.105 320.878 + 1.18 345.748 + 1.214 321.485 + 1.249 345.748 + 1.274 314.206 + 1.5 316.026 + 1.601 309.96 + 1.916 303.894 + 1.956 265.073 + 2.0 214.121 + 2.052 179.546 + 2.102 158.923 + 2.201 117.676 + 2.268 106.151 + 2.303 87.953 + 2.369 55.805 + 2.407 49.739 + 2.486 39.427 + 2.558 21.837 + 2.563 0.0 +; +; +G25W-10A 29 152.4 10 0.097 0.17 AT + 0.01 38.046 + 0.029 21.768 + 0.11 30.475 + 0.239 35.775 + 0.496 40.696 + 0.568 42.116 + 0.592 45.429 + 0.749 46.186 + 0.997 45.713 + 1.255 44.198 + 1.498 39.939 + 1.999 31.421 + 2.501 23.093 + 3.006 14.196 + 3.503 7.288 + 3.999 4.07 + 4.371 1.988 + 4.414 0.0 +; +; At DMS G125 +G125T-14A 29 127 14 0.062 0.127 AT + 0.008 89.654 + 0.017 117.24 + 0.027 119.654 + 0.047 111.033 + 0.115 124.826 + 0.2 134.136 + 0.399 149.308 + 0.601 155.17 + 0.8 138.274 + 0.824 133.791 + 0.878 88.964 + 0.914 44.482 + 0.933 22.414 + 0.974 2.069 + 1.001 0.0 +; +; AT H115 Dark Matter DMS +H115DM-14A 29 203 14 0.113 0.20500000000000002 AT + 0.014 89.265 + 0.024 130.742 + 0.036 108.2 + 0.048 101.588 + 0.081 111.206 + 0.202 121.124 + 0.405 123.228 + 0.598 123.829 + 0.8 123.528 + 1.002 122.326 + 1.2 114.211 + 1.269 111.807 + 1.293 111.506 + 1.35 119.32 + 1.367 117.818 + 1.393 111.807 + 1.429 88.964 + 1.467 67.024 + 1.524 44.182 + 1.562 22.842 + 1.583 13.224 + 1.6 6.913 + 1.626 3.306 + 1.662 1.202 + 1.693 0.0 +; +; At DMS I500T +I500T-14A 38 355 14 0.248 0.58 AT + 0.008 447.072 + 0.014 534.306 + 0.028 581.557 + 0.052 504.016 + 0.09 514.92 + 0.11 533.094 + 0.131 524.613 + 0.177 551.268 + 0.202 540.364 + 0.23 552.479 + 0.29 543.998 + 0.399 552.479 + 0.481 553.691 + 0.526 563.384 + 0.565 554.902 + 0.6 564.595 + 0.638 558.537 + 0.728 567.018 + 0.8 560.96 + 0.922 537.94 + 0.979 535.517 + 0.999 546.421 + 1.02 550.056 + 1.043 535.517 + 1.064 444.649 + 1.091 322.28 + 1.11 267.759 + 1.141 225.353 + 1.152 181.737 + 1.16 238.681 + 1.163 149.024 + 1.174 118.735 + 1.2 118.735 + 1.255 86.022 + 1.312 46.04 + 1.335 0.0 +; +; +L1250DM 75 801 P 2.565 5.647 AT + 0.032 1511.087 + 0.049 1295.217 + 0.211 1334.466 + 0.247 1396.61 + 0.256 1553.606 + 0.284 1380.257 + 0.491 1354.09 + 1.493 1448.942 + 1.72 1468.567 + 1.862 1478.379 + 2.008 1458.755 + 2.499 1334.466 + 3.002 1174.199 + 3.108 889.644 + 3.156 667.233 + 3.245 444.822 + 3.42 225.682 + 3.505 94.852 + 3.529 62.144 + 3.574 39.249 + 3.663 16.354 + 3.785 6.541 + 3.842 0.0 +; +; +N2220DM 98 1046 P 7.183 11.997 AT + 0.045 2638.366 + 0.067 2528.97 + 0.084 3063.078 + 0.124 2426.009 + 0.186 2548.275 + 0.231 2599.755 + 0.298 2554.71 + 0.371 2644.801 + 0.534 2638.366 + 0.979 2561.145 + 1.142 2606.19 + 2.002 2638.366 + 2.289 2638.366 + 2.761 2580.45 + 3.121 2496.795 + 3.436 2335.919 + 3.678 2213.653 + 3.79 2129.998 + 4.004 1653.805 + 4.415 888.035 + 4.538 630.634 + 4.656 450.453 + 4.82 289.577 + 5.005 135.136 + 5.219 25.74 + 5.371 0.0 +; +; Aerotech L1365 Metalstorm for 75/5120, derived from instruction sheet thrust curve. +L1365M 75 665.5 P 2.648 4.908 AT + 0.009 166.808 + 0.013 618.303 + 0.022 940.799 + 0.03 1018.642 + 0.046 1160.985 + 0.059 1356.707 + 0.063 1496.826 + 0.076 1616.928 + 0.102 1434.551 + 0.15 1430.103 + 0.193 1472.361 + 0.245 1519.067 + 0.258 1541.308 + 0.282 1592.463 + 0.347 1623.6 + 0.393 1610.256 + 0.486 1574.67 + 0.556 1554.653 + 0.627 1539.084 + 0.673 1512.395 + 0.747 1479.033 + 0.779 1481.257 + 0.831 1496.826 + 0.885 1505.722 + 0.94 1523.515 + 0.987 1465.688 + 1.009 1532.412 + 1.026 1494.602 + 1.098 1534.636 + 1.142 1463.464 + 1.185 1505.722 + 1.224 1476.809 + 1.246 1523.515 + 1.296 1483.481 + 1.322 1516.843 + 1.346 1472.361 + 1.441 1501.274 + 1.504 1507.947 + 1.528 1601.359 + 1.589 1510.171 + 1.699 1512.395 + 1.732 1512.395 + 1.801 1463.464 + 1.864 1496.826 + 1.964 1521.291 + 2.007 1510.171 + 2.068 1450.12 + 2.129 1443.447 + 2.201 1510.171 + 2.237 1463.464 + 2.374 1474.585 + 2.457 1416.758 + 2.546 1427.879 + 2.632 1367.828 + 2.687 1403.413 + 2.776 1343.362 + 2.834 1425.655 + 2.897 1307.777 + 2.93 1347.811 + 2.947 1316.673 + 2.982 1361.155 + 3.051 1354.483 + 3.071 1330.018 + 3.14 1129.848 + 3.175 1029.763 + 3.227 842.938 + 3.277 582.717 + 3.307 449.27 + 3.353 329.168 + 3.414 184.601 + 3.479 88.964 + 3.527 48.93 + 3.587 20.017 + 3.663 17.793 + 3.711 8.896 + 3.752 0.0 +; +; F44W Economax +F44W 24 70 4-8 0.0197 0.048 AT + 0.02 2.676 + 0.026 6.02 + 0.034 11.204 + 0.063 24.917 + 0.135 59.031 + 0.15 61.372 + 0.2 63.212 + 0.299 65.218 + 0.4 65.051 + 0.5 63.379 + 0.6 58.529 + 0.668 55.017 + 0.686 53.68 + 0.687 54.014 + 0.7 49.165 + 0.719 43.813 + 0.774 22.074 + 0.795 13.211 + 0.812 7.86 + 0.825 4.515 + 0.854 2.007 + 0.899 0.167 + 0.998 0.0 +; +; G74W Economax +G74W 29 83 4-6-9 0.039299999999999995 0.08700000000000001 AT + 0.023 6.551 + 0.05 21.838 + 0.088 44.852 + 0.124 67.362 + 0.135 71.561 + 0.148 74.417 + 0.197 80.128 + 0.248 85.0 + 0.298 87.52 + 0.397 89.704 + 0.499 91.215 + 0.6 90.375 + 0.699 90.375 + 0.751 89.536 + 0.8 87.856 + 0.9 84.496 + 0.954 82.144 + 0.971 81.808 + 0.987 79.96 + 1.002 76.433 + 1.023 67.194 + 1.065 44.516 + 1.094 22.174 + 1.107 15.287 + 1.126 6.887 + 1.138 3.36 + 1.157 1.344 + 1.18 0.168 + 1.192 0.0 +; +; From AT DMS announcement May 2014. +H45 38 202.7 10 0.18 0.364 AT + 0.04 84.004 + 0.854 86.004 + 1.377 84.804 + 2.046 79.204 + 2.69 66.003 + 3.286 51.603 + 4.414 28.401 + 5.042 16.001 + 5.429 9.2 + 6.113 6.4 + 6.186 0.0 +; +; From AT DMS announcement May 2014. +H182 29 203.2 14 0.115 0.20700000000000002 AT + 0.007 82.404 + 0.031 159.208 + 0.091 158.408 + 0.186 182.409 + 0.5 192.009 + 0.904 188.809 + 1.054 175.209 + 1.106 180.809 + 1.144 200.81 + 1.163 162.408 + 1.201 36.802 + 1.212 16.801 + 1.235 0.0 +; +; From AT DMS announcement May 2014. +I65 54 218 10 0.377 0.752 AT + 0.023 148.274 + 0.211 196.341 + 0.398 167.827 + 0.797 149.903 + 1.395 135.239 + 2.238 122.204 + 3.199 99.392 + 4.711 69.249 + 5.367 48.882 + 6.246 29.329 + 6.926 15.479 + 7.395 11.406 + 8.496 0.0 +; +; From AT DMS announcement May 2014. +I205 29 304.8 14 0.188 0.315 AT + 0.008 377.299 + 0.028 241.932 + 0.36 256.333 + 0.711 246.252 + 0.861 233.292 + 1.121 230.411 + 1.146 214.571 + 1.242 211.69 + 1.349 141.127 + 1.404 125.286 + 1.489 72.004 + 1.602 41.762 + 1.712 11.521 + 1.787 12.961 + 1.892 0.0 +; +; From AT DMS announcement May 2014. +J425 38 356.4 14 0.364 0.631 AT + 0.018 267.857 + 0.062 368.062 + 0.242 420.092 + 0.524 443.216 + 0.902 452.851 + 1.225 448.997 + 1.389 433.581 + 1.502 452.851 + 1.53 420.092 + 1.542 356.5 + 1.599 67.446 + 1.618 28.905 + 1.648 0.0 +; +; revised per AT post on TRF 5/19/14 +K535 54 358.1 14 0.745 1.264 AT + 0.015 467.288 + 0.063 642.221 + 0.104 613.465 + 0.23 627.843 + 0.419 620.654 + 0.883 623.05 + 1.335 599.087 + 1.646 555.953 + 1.843 500.837 + 2.017 450.513 + 2.258 404.983 + 2.488 366.641 + 2.6 230.049 + 2.611 172.537 + 2.648 124.61 + 2.696 81.476 + 2.789 40.738 + 2.837 9.585 + 2.952 0.0 +; +; per AT announcement 5/8/14 +L1000 54 635 18 1.4000000000000001 2.194 AT + 0.004 10.664 + 0.011 1268.961 + 0.04 1322.279 + 0.195 1226.307 + 0.249 1268.961 + 0.296 1242.303 + 0.372 1252.966 + 0.416 1215.644 + 0.6 1226.307 + 0.788 1215.644 + 1.066 1183.653 + 1.261 1167.658 + 1.507 1125.004 + 1.746 1087.681 + 1.865 1050.359 + 1.995 1045.027 + 2.093 911.733 + 2.158 746.448 + 2.263 554.504 + 2.389 405.215 + 2.577 191.944 + 2.693 85.308 + 2.761 42.654 + 3.0 0.0 +; +; AT H550 ST DMS +H550 38 206 14 0.176 0.316 AT + 0.008 445.411 + 0.009 533.786 + 0.01 565.601 + 0.013 586.812 + 0.015 623.34 + 0.021 639.837 + 0.036 606.843 + 0.045 629.232 + 0.057 615.092 + 0.061 635.123 + 0.067 619.805 + 0.101 637.48 + 0.116 622.162 + 0.157 643.372 + 0.174 623.34 + 0.196 623.34 + 0.205 639.837 + 0.231 631.588 + 0.234 618.627 + 0.255 611.557 + 0.268 628.053 + 0.314 595.06 + 0.334 600.952 + 0.362 571.493 + 0.386 565.601 + 0.401 556.175 + 0.426 518.468 + 0.445 503.15 + 0.493 447.768 + 0.505 447.768 + 0.511 456.016 + 0.519 451.303 + 0.535 357.036 + 0.545 266.304 + 0.551 179.107 + 0.559 91.91 + 0.565 42.42 + 0.572 12.962 + 0.579 0.0 +; +; AT M1350W DMS +M1350W 75 622 p 1.97 4.808 AT + 0.03 1428.886 + 0.044 1724.734 + 0.056 1548.484 + 0.078 1620.873 + 0.115 1589.399 + 0.178 1642.904 + 0.455 1749.913 + 0.496 1724.734 + 0.54 1737.324 + 1.132 1746.766 + 1.499 1731.029 + 1.639 1715.292 + 2.505 1334.466 + 3.086 1051.207 + 3.179 985.113 + 3.227 928.461 + 3.315 670.38 + 3.419 446.92 + 3.46 396.563 + 3.545 298.996 + 3.697 173.103 + 3.737 173.103 + 3.845 81.83 + 3.996 0.0 +; +; +H225R 29 291 10 0.133 0.316 KBA +0.025 104.61 +0.091 141.936 +0.104 177.297 +0.16 195.96 +0.26 219.534 +0.336 229.848 +0.345 225.919 +0.43 251.949 +0.562 267.174 +0.668 268.156 +0.742 268.156 +0.794 262.754 +0.818 262.263 +0.89322 256.917 +0.957 272.576 +0.971 275.523 +0.982 271.594 +0.991 230.339 +1.025 162.072 +1.055 72.687 +1.078 32.414 +1.121 0 +; +;Animal Compatible. +J740G 38 370 1000 0.308 0.724 KBA +0.003 84.03 +0.009 94.757 +0.015 459.483 +0.026 661.512 +0.039 740.178 +0.044 763.42 +0.054 775.935 +0.07 783.087 +0.078 792.026 +0.087 827.784 +0.167 884.996 +0.323 918.965 +0.495 911.814 +0.568 915.389 +0.589 920.753 +0.634 947.571 +0.649 956.51 +0.659 949.359 +0.7 870.693 +0.715 831.359 +0.727 781.299 +0.751 548.876 +0.765 362.938 +0.772 185.938 +0.78 286.059 +0.793 116.212 +0.807 59 +0.844 0 +; +; +K520F 38 368 6-10-14 0.327 0.722 KBA +0.018 696.864 +0.024 547.629 +0.031 737.092 +0.039 529.461 +0.051 524.27 +0.054 415.263 +0.063 547.629 +0.079 613.811 +0.094 543.735 +0.106 533.354 +0.127 546.331 +0.146 546.331 +0.191 548.926 +0.379 560.605 +0.558 591.75 +0.629 599.536 +0.787 596.941 +0.892 587.857 +0.971 572.285 +1.015 582.666 +1.026 582.666 +1.039 552.819 +1.1 330.913 +1.12 275.112 +1.145 254.349 +1.161 224.502 +1.209 77.862 +1.227 32.442 +1.255 0 +; +; +K700F 54 406 6-10-14 0.734 1.503 KBA +0.011 789.955 +0.045 831.342 +0.057 753.966 +0.118 741.37 +0.422 800.752 +0.454 818.746 +0.748 872.729 +0.798 870.93 +0.853 890.724 +0.923 903.32 +1.084 908.718 +1.209 897.921 +1.395 843.938 +1.517 786.356 +1.565 777.359 +1.587 775.559 +1.61 786.356 +1.635 753.966 +1.678 543.431 +1.71 446.262 +1.753 300.507 +1.796 131.359 +1.814 50.384 +1.85 0 +; +;Animal Compatible +L2300G 54 728 1000 1.31 2.63 KBA +0.013 2930.02 +0.019 2243.45 +0.029 2277.3 +0.033 2499.71 +0.054 2533.55 +0.11 2451.36 +0.207 2480.37 +0.443 2654.43 +0.636 2842.99 +0.664 2891.34 +0.757 2833.32 +0.794 2780.14 +0.804 2852.66 +0.812 2789.81 +0.874 2577.07 +0.912 2509.38 +0.943 2461.03 +0.977 2354.66 +0.991 2224.11 +0.997 2354.66 +1.042 1426.33 +1.074 498.007 +1.096 246.586 +1.117 149.886 +1.136 106.37 +1.172 48.35 +1.249 0 +; 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+;Pro24-3G White Thunder 74-F85 +F85-WT-15A 24 133 15-12-10-8-6 0.042 0.096 CTI +0.01 76.074 +0.023 100.185 +0.04 92.425 +0.118 100.878 +0.283 102.402 +0.51 96.443 +0.688 87.436 +0.787 25.912 +0.852 7.206 +0.873 0 +; +;Pro24-6G Skidmark 114-G100 +G100-SK-14A 24 228 14-11-9-7-5 0.073 0.159 CTI +0.009 148.468 +0.024 178.207 +0.061 145.289 +0.475 117.367 +0.63 106.243 +0.833 85.131 +0.961 51.759 +1.024 29.966 +1.125 13.848 +1.186 0 +; +;Pro24-6G RL 137-G127 +G127-RL-14A 24 228 14-11-9-7-5 0.081 0.166 CTI +0.018 164.454 +0.029 175.478 +0.042 172.103 +0.14 179.753 +0.378 158.83 +0.578 138.583 +0.763 121.485 +0.838 97.638 +0.9 62.317 +0.966 32.621 +1.056 13.048 +1.081 0 +; +;Pro54-2G White 867-J244 +J244-WH-14A 54 236 14-11-9-7-5 0.511 0.911 CTI +0.029 154.144 +0.1 262.541 +0.161 235.691 +0.484 256.575 +0.853 261.215 +1.348 266.519 +1.904 262.541 +2.422 251.934 +2.855 235.691 +3.176 223.094 +3.252 221.768 +3.362 184.972 +3.5 0 +; +;Pro54-3G White 1281-K360 +K360-WH-13A 54 236 13-10-8-6-4 0.747 1.232 CTI +0.034 289.25 +0.077 362.318 +0.463 387.514 +1.106 398.6 +1.564 405.151 +2.063 398.6 +2.57 383.483 +3.101 354.759 +3.18 343.673 +3.417 105.319 +3.5 0 +; 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+;Pro-54-1G C-Star 518-I165-17A +;Ejection adjustable from 7 to 17 +I165-CS-17A 54 69 17-15-13-11-9-7 0.267 0.594 CTI +0.027 133.424 +0.056 174.831 +0.067 179.973 +0.497 188.633 +1.018 184.032 +1.704 169.959 +2.95 129.364 +3.05 130.717 +3.168 44.655 +3.213 17.862 +3.271 3.518 +3.5 0 +; +;CTI 30,795-O25000-VM-P +O25000-VM-P 132 1407 1000 14.705 23.558 CTI +0.008 21113.4 +0.022 24705.9 +0.042 26281.5 +0.067 24390.8 +0.201 24044.1 +0.56 25052.5 +0.927 24075.6 +1.202 22815.1 +1.25 23602.9 +1.297 4852.94 +1.32 0 +; +;Smoky Sam 24mm 1G +;24-E22-SS-13A +E22-SS-13A 24 69 13-10-8-6-4 0.0203 0.0565 CTI +0.008 18.292 +0.026 30 +0.038 30.792 +0.067 18.708 +0.101 21.875 +0.33 26.083 +0.528 28.042 +0.716 27.875 +0.841 23.542 +0.912 17.833 +0.987 7 +1.016 3.333 +1.065 1.083 +1.087 0 +; +;White 24mm 1G +;26-E31-WH-15A +E31-WH-15A 24 69 15-12-10-8-6 0.0169 0.052 CTI +0.02 43.824 +0.027 39.964 +0.049 26.781 +0.113 32.601 +0.193 34.739 +0.282 35.808 +0.5 34.442 +0.727 29.276 +0.771 22.743 +0.807 9.561 +0.84 3.563 +0.87 0 +; 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+; diff --git a/core/resources/datafiles/thrustcurves/RASAero/README.txt b/core/resources/datafiles/thrustcurves/RASAero/README.txt new file mode 100644 index 000000000..c3df9c448 --- /dev/null +++ b/core/resources/datafiles/thrustcurves/RASAero/README.txt @@ -0,0 +1,2 @@ +This directory contains thrust curves used in RASAero. +Last updated: 2018-07-31 \ No newline at end of file