;*AEROTECH*AEROTECH*AEROTECH* ; ; Aerotech D7TRC 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. D7TRC 24 70 0 .0105 .0422 AT-RMS 0.036 3.336 0.084 9.326 0.101 10.281 0.143 10.827 0.213 10.990 0.271 10.887 0.359 10.685 0.471 10.130 0.506 10.342 0.535 9.929 0.810 8.697 1.226 6.713 1.589 5.138 1.800 4.861 2.151 4.581 2.649 4.570 2.696 3.887 2.748 2.388 2.807 0.889 2.842 0.207 2.870 0.000 ; ; ; Aerotech D9 RASP.ENG file made from NAR published data ; File produced July 4, 2000 ; The total impulse, peak thrust, average thrust and burn time are ; the same as the averaged static test data on the NAR web site in ; the certification file. The curve drawn with these data points is as ; close to the certification curve as can be with such a limited ; number of points (32) allowed with wRASP up to v1.6. D9W 24 70 4-7 0.0101 0.0471 AT-RMS 0.023 2.204 0.077 1.653 0.177 4.960 0.269 8.817 0.308 9.920 0.315 9.368 0.358 10.604 0.415 11.940 0.515 13.917 0.623 16.675 0.731 19.155 0.792 20.000 0.865 19.155 0.889 19.562 0.923 18.600 1.038 16.120 1.115 14.195 1.185 12.538 1.277 10.336 1.373 7.440 1.485 4.822 1.612 2.755 1.762 1.240 1.880 0.000 ; ; ; Aerotech D13 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. D13W 18 70 4-7-10 0.0098 0.0314 AT-RMS 0.030 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 23.610 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 0.480 19.947 0.507 19.947 0.521 20.509 0.559 18.693 0.580 19.118 0.660 17.578 0.743 15.337 0.861 12.406 0.947 9.329 1.068 5.834 1.155 4.158 1.172 4.720 1.231 2.762 1.328 1.928 1.404 1.093 1.520 0.000 ; ; ; Aerotech D15 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. D15T 24 70 4-6-8 .0089 .0462 AT-RMS 0.014 11.480 0.049 26.272 0.081 30.087 0.107 31.261 0.121 31.249 0.159 31.360 0.208 31.249 0.283 29.583 0.439 23.353 0.551 18.484 0.675 13.430 0.863 6.422 0.938 3.892 1.010 2.335 1.085 0.778 1.142 0.389 1.150 0.000 ; ; ; Aerotech D21 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. D21T 18 70 4-7 .0096 .0250 AT-SU 0.010 1.367 0.021 19.367 0.029 32.120 0.037 31.667 0.051 30.528 0.094 30.074 0.115 31.213 0.133 30.074 0.177 30.760 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 0.940 0.000 ; ; ; AEROTECH D24 RASP.ENG file made from NAR data ; File produced August 22, 2002 ; The total impulse, peak thrust, average thrust and burn time are ; the same as the averaged static test data on the NAR web site in ; the certification file. The curve drawn with these data points is as ; close to the certification curve as can be with such a limited ; number of points (32) allowed with wRASP up to v1.6. D24T 18 70 0-4-7 0.0087 0.0308 AT-RMS 0.010 10.992 0.015 14.575 0.023 18.641 0.041 25.52 0.048 23.419 0.060 22.576 0.108 21.141 0.127 21.853 0.189 21.141 0.245 20.769 0.255 21.01 0.365 20.408 0.421 19.805 0.473 19.324 0.572 17.999 0.676 16.673 0.734 15.71 0.780 14.395 0.803 14.515 0.828 13.07 0.884 11.996 0.940 9.838 0.973 8.163 1.020 5.649 1.070 3.373 1.116 1.936 1.151 0.977 1.220 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. E6TRC 24 70 0 .0215 .0527 AT-RMS 0.047 10.866 0.127 11.693 0.190 11.900 0.316 11.622 0.522 10.593 0.743 9.287 0.996 7.842 1.249 6.190 1.470 5.296 1.787 4.747 2.372 4.471 3.020 4.403 3.747 4.264 4.490 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 0.550 7.120 0.000 ; ; ; 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. E7TRC 24 70 0 .0171 .0484 AT-RMS 0.038 6.636 0.063 10.056 0.087 11.019 0.134 11.420 0.206 11.580 0.312 11.149 0.466 10.738 0.667 9.777 0.940 8.132 1.223 6.281 1.484 5.182 1.709 4.701 2.112 4.423 2.776 4.279 3.310 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 5.360 0.965 5.430 0.000 ; ; ; Aerotech E11J 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. E11J 24 70 4 .0250 .0624 AT-RMS 0.030 7.660 0.094 14.539 0.216 16.874 0.280 17.868 0.298 19.200 0.315 17.759 0.338 18.415 0.373 17.749 0.507 18.633 0.536 19.850 0.571 18.961 0.652 18.295 0.687 18.852 0.745 18.514 0.814 17.957 0.907 17.620 0.994 16.954 1.127 15.612 1.145 16.725 1.191 15.612 1.284 14.608 1.411 13.605 1.504 12.820 1.655 11.706 1.811 10.037 1.945 8.699 2.084 7.362 2.281 4.912 2.501 2.350 2.687 0.566 2.785 0.118 2.830 0.000 ; ; ; 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 0 .0303 .0594 AT-RMS 0.054 16.764 0.095 18.330 0.197 16.545 0.313 16.654 0.360 17.211 0.401 16.316 0.442 17.550 0.476 16.206 0.578 16.316 0.666 16.764 0.700 15.649 0.768 16.316 0.890 16.097 1.019 15.649 1.162 14.983 1.230 14.983 1.250 13.968 1.291 14.754 1.332 13.749 1.373 14.197 1.434 13.530 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 3.050 0.000 ; ; ; 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. E15W 24 70 4-7 .0201 .0501 AT-SU 0.020 23.330 0.036 27.318 0.058 28.840 0.079 27.171 0.139 25.638 0.183 24.263 0.237 24.106 0.297 22.426 0.373 21.964 0.400 20.894 0.443 21.355 0.487 20.442 0.617 19.833 0.742 18.457 0.812 20.000 0.850 18.006 0.899 18.467 1.035 17.711 1.100 16.945 1.160 16.945 1.377 15.736 1.426 14.656 1.436 16.198 1.463 14.813 1.550 14.361 1.572 15.432 1.610 13.752 1.827 12.839 2.126 10.098 2.337 6.116 2.538 1.369 2.640 0.000 ; ; ; Aerotech E16 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. E16W 29 124 4-7-10 .0190 .1086 AT-RMS 0.132 32.223 0.221 37.200 0.255 36.699 0.306 36.699 0.371 35.357 0.414 33.785 0.437 34.906 0.472 33.785 0.530 32.894 0.553 31.772 0.576 32.443 0.638 29.309 0.720 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 1.790 2.000 0.000 ; ; ; Aerotech E18 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. E18W 24 70 4-8 .0270 .0589 AT-RMS 0.016 6.086 0.042 17.004 0.073 26.138 0.098 28.815 0.134 29.357 0.170 29.347 0.195 30.080 0.236 29.347 0.287 29.878 0.338 29.337 0.368 29.878 0.404 28.795 0.424 29.688 0.465 28.976 0.526 28.785 0.592 28.063 0.669 27.341 0.786 25.908 0.908 22.850 1.025 20.163 1.157 17.105 1.284 14.057 1.462 10.638 1.660 6.506 1.838 3.270 2.006 1.109 2.083 0.388 2.140 0.000 ; ; ; Aerotech E23 RASP.ENG file made from NAR published data ; File produced July 4, 2000 ; The total impulse, peak thrust, average thrust and burn time are ; the same as the averaged static test data on the NAR web site in ; the certification file. The curve drawn with these data points is as ; close to the certification curve as can be with such a limited ; number of points (32) allowed with wRASP up to v1.6. E23T 29 124 5-8 .0174 .1039 AT-RMS 0.024 16.299 0.035 21.959 0.067 30.785 0.090 35.774 0.153 37.577 0.200 38.220 0.240 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 16.980 1.187 12.682 1.336 7.471 1.450 3.169 1.497 1.584 1.532 0.679 1.570 0.000 ; ; ; Aerotech E28 RASP.ENG file made from NAR published data ; File produced July 4, 2000 ; The total impulse, peak thrust, average thrust and burn time are ; the same as the averaged static test data on the NAR web site in ; the certification file. The curve drawn with these data points is as ; close to the certification curve as can be with such a limited ; number of points (32) allowed with wRASP up to v1.6. E28T 24 70 2-5-8 .0184 .0545 AT-RMS 0.010 29.8620 0.018 45.1390 0.038 47.5620 0.081 50.5200 0.106 48.9530 0.146 48.2630 0.161 48.9530 0.197 48.9530 0.242 47.5620 0.313 46.1800 0.411 43.0570 0.494 40.6240 0.527 39.5830 0.542 40.2740 0.562 38.5420 0.633 36.4600 0.683 34.3770 0.743 31.2440 0.799 29.1620 0.877 26.0380 0.970 20.8320 1.006 17.3590 1.046 11.4620 1.089 6.9430 1.132 3.8190 1.172 1.7350 1.220 0.0000 ; ; ; Aerotech E30 RASP.ENG file made from NAR published data ; File produced July 4, 2000 ; The total impulse, peak thrust, average thrust and burn time are ; the same as the averaged static test data on the NAR web site in ; the certification file. The curve drawn with these data points is as ; close to the certification curve as can be with such a limited ; number of points (32) allowed with wRASP up to v1.6. E30T 24 70 4-7 .0198 .0433 AT-SU 0.013 38.8470 0.020 45.6210 0.041 48.2700 0.059 46.5020 0.110 46.5020 0.166 45.9120 0.184 46.7920 0.217 45.9120 0.265 45.9120 0.319 45.0310 0.383 44.1500 0.482 42.0890 0.594 38.8470 0.615 39.4370 0.628 37.3760 0.684 35.3140 0.742 33.2630 0.804 30.0210 0.880 25.6070 0.962 20.0140 1.038 12.9490 1.089 7.3580 1.151 3.2370 1.186 1.1760 1.220 0.0000 ; ; ; Aerotech F12 RASP.ENG file made from NAR published data ; File produced July 4, 2000 ; The total impulse, peak thrust, average thrust and burn time are ; the same as the averaged static test data on the NAR web site in ; the certification file. The curve drawn with these data points is as ; close to the certification curve as can be with such a limited ; number of points (32) allowed with wRASP up to v1.6. F12J 24 70 2-5 .0303 .0667 AT-RMS 0.037 20.894 0.054 22.152 0.101 22.152 0.148 22.571 0.165 23.409 0.200 22.421 0.281 22.142 0.369 22.132 0.474 22.271 0.526 23.540 0.549 21.982 0.637 22.122 0.724 21.842 0.800 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 1.790 17.300 1.883 13.936 2.051 11.260 2.220 7.468 2.447 3.671 2.709 1.135 2.930 0.000 ; ; ; Aerotech F13JRC 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. F13JRC 32 107 0 .0323 .1105 AT-RMS 0.048 15.309 0.084 18.629 0.143 19.980 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 2.510 11.084 2.558 12.108 2.641 10.855 2.976 10.736 3.490 10.627 3.873 10.507 3.992 10.965 4.028 10.627 4.410 10.507 4.625 10.736 4.769 9.941 4.829 8.684 4.865 6.742 4.960 3.199 5.020 1.485 5.100 0.000 ; ; ; Aerotech F16JRC 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. F16JRC 32 107 0 .0625 .1404 AT-RMS 0.046 26.350 0.116 22.388 0.139 21.374 0.185 21.886 0.220 20.540 0.301 19.696 0.498 18.350 0.579 19.194 0.637 16.492 0.718 18.350 0.834 18.350 0.950 18.350 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 18.180 2.664 15.659 2.896 15.488 3.290 13.800 3.718 11.611 4.181 9.426 4.888 5.891 5.690 0.000 ; ; ; Aerotech F20 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. F20W 29 73 4-7 .0300 .0746 AT-SU 0.014 52.080 0.032 49.808 0.062 46.979 0.099 45.559 0.153 44.492 0.183 45.549 0.208 43.425 0.244 43.777 0.323 43.767 0.365 44.110 0.444 43.042 0.450 40.576 0.529 39.861 0.620 38.079 0.759 36.296 0.795 37.354 0.844 34.877 0.886 36.991 0.898 33.457 1.031 30.608 1.056 32.017 1.086 29.551 1.225 25.996 1.322 22.452 1.346 23.157 1.364 21.385 1.576 16.421 1.800 11.095 2.012 6.476 2.194 3.627 2.388 1.132 2.680 0.000 ; ; F21W 24 96 0-4-6-8 0.03000 0.06400 AT-SU 0.01 48.00 0.13 36.00 0.25 36.00 0.38 36.00 0.50 36.00 0.63 35.00 0.75 34.00 0.88 32.00 1.00 31.00 1.13 27.00 1.25 25.00 1.38 18.00 1.50 16.00 1.63 13.00 1.75 12.00 1.88 8.00 2.00 5.00 2.13 4.00 2.25 2.00 2.38 1.00 2.40 0.00 ; ; ; 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. F22J 29 125 4-7 .0463 .1342 AT-RMS 0.014 11.527 0.075 20.126 0.157 26.572 0.293 29.113 0.382 30.278 0.450 29.690 0.539 30.667 0.614 30.089 0.662 31.150 0.771 30.478 0.948 29.890 0.996 28.714 1.078 28.136 1.187 27.738 1.289 26.761 1.337 26.960 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 16.210 2.402 13.480 2.640 8.791 2.961 3.320 3.310 0.000 ; ; ; Aerotech F23 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. F23FJ-old 29 73 4-7 .0320 .0786 AT-SU 0.029 48.700 0.049 43.106 0.083 41.409 0.102 42.258 0.132 40.840 0.175 39.422 0.229 38.853 0.268 38.853 0.302 37.436 0.312 38.574 0.361 37.715 0.429 36.587 0.502 36.018 0.560 36.018 0.595 34.601 0.687 33.183 0.770 32.614 0.853 31.196 0.936 29.499 1.038 27.792 1.179 24.388 1.204 25.237 1.248 22.970 1.374 20.984 1.535 16.731 1.691 12.478 1.827 9.075 1.954 5.105 2.071 2.269 2.220 0.000 ; ; ;F23FJ Motor Thrust Curve created by Tim Van Milligan ;for RockSim Users - www.rocksim.com ;file produced March 2, 2005 ;Based on data supplied by Aerotech for the newer molded case F23 econojet. F23FJ 29 83 4-7 0.033 0.0839 AT-SU 0.03 48.7 0.05 43.11 0.08 41.41 0.1 42.26 0.13 40.84 0.17 39.42 0.23 38.85 0.27 38.85 0.3 37.44 0.31 38.57 0.36 37.72 0.43 36.59 0.5 36.02 0.56 36.02 0.59 34.6 0.69 33.18 0.77 32.61 0.85 31.2 0.94 29.5 1.04 27.79 1.18 24.39 1.2 25.24 1.25 22.97 1.37 20.98 1.53 16.73 1.69 12.48 1.83 9.07 1.95 5.11 2.07 2.27 2.22 0 ; ; ; Aerotech F23WRCSK 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. F23WRCSK 32 107 0 .0378 .1287 AT-RMS 0.042 22.644 0.133 28.191 0.161 27.261 0.189 29.570 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 36.000 0.938 34.656 1.015 34.656 1.071 34.197 1.120 33.038 1.218 32.578 1.267 29.810 1.351 29.340 1.393 27.731 1.540 26.802 1.645 24.263 1.799 21.255 1.862 19.866 2.051 15.479 2.317 11.552 2.618 6.700 2.884 3.234 3.185 1.386 3.470 0.000 ; ; ; Aerotech F24 RASP.ENG file made from NAR published data ; File produced July 4, 2000 ; The total impulse, peak thrust, average thrust and burn time are ; the same as the averaged static test data on the NAR web site in ; the certification file. The curve drawn with these data points is as ; close to the certification curve as can be with such a limited ; number of points (32) allowed with wRASP up to v1.6. F24W 24 70 4-7 .0190 .0625 AT-RMS 0.033 15.942 0.112 40.146 0.125 40.950 0.180 40.427 0.245 40.126 0.281 40.417 0.355 39.524 0.438 39.213 0.543 37.727 0.603 36.532 0.658 33.279 0.685 34.163 0.726 29.434 0.772 29.716 0.951 26.453 1.071 24.666 1.107 22.588 1.185 20.811 1.383 16.644 1.649 10.410 1.828 5.369 1.938 2.403 1.988 1.806 2.048 0.912 2.130 0.000 ; ; ; Aerotech F25 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. F25W-old 29 97 4-6-9 .0356 .0898 AT-SU 0.029 29.073 0.071 41.739 0.126 44.040 0.147 46.624 0.175 46.790 0.216 45.752 0.258 46.036 0.320 44.019 0.382 42.003 0.409 43.432 0.513 41.121 0.623 40.544 0.706 39.956 0.823 38.801 0.989 36.196 1.196 31.859 1.223 33.582 1.265 30.704 1.410 28.383 1.589 25.495 1.775 23.175 2.031 19.983 2.217 16.517 2.458 12.180 2.596 8.422 2.693 4.672 2.775 2.650 2.872 0.915 3.050 0.000 ; ; ;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-SU 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 ; ; ;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-SU 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 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. F32W 24 124 5-10-15 .0377 .0814 AT-SU 0.025 46.699 0.031 51.846 0.061 55.640 0.085 52.868 0.126 47.370 0.245 45.637 0.340 44.946 0.394 42.873 0.447 42.873 0.572 41.140 0.720 39.408 0.744 40.780 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 27.280 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 13.820 2.382 7.281 2.525 2.457 2.720 0.000 ; ; ; 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. F37W 29 99 6-10-14 .0282 .1086 AT-RMS 0.018 7.251 0.053 13.626 0.088 22.331 0.106 25.227 0.141 26.385 0.183 28.411 0.260 37.685 0.310 41.449 0.422 44.035 0.524 45.183 0.590 46.470 0.682 45.153 0.864 43.386 0.934 40.471 1.042 35.230 1.151 29.699 1.246 25.037 1.354 19.796 1.445 13.397 1.498 7.586 1.540 3.226 1.600 0.000 ; ; ; Aerotech F39 RASP.ENG file made from NAR published data ; File produced July 4, 2000 ; The total impulse, peak thrust, average thrust and burn time are ; the same as the averaged static test data on the NAR web site in ; the certification file. The curve drawn with these data points is as ; close to the certification curve as can be with such a limited ; number of points (32) allowed with wRASP up to v1.6. F39T 24 70 3-6-9 .0227 .0600 AT-RMS 0.010 45.057 0.016 54.131 0.046 58.321 0.079 59.470 0.103 58.311 0.130 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 0.480 47.041 0.680 41.059 0.716 39.649 0.752 38.944 0.809 36.487 0.860 34.382 0.893 33.324 0.917 32.619 1.000 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 2.500 1.330 0.000 ; ; ; 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. F40W 29 124 4-7-10 .0400 .1260 AT-RMS 0.015 17.776 0.049 41.016 0.089 58.793 0.124 62.900 0.148 65.173 0.183 62.442 0.242 68.070 0.292 60.617 0.321 61.524 0.415 60.617 0.524 58.334 0.741 52.412 0.870 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 3.190 2.060 0.000 ; ; ;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-SU 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 F50 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. F50T-old 29 98 4-6-9 .0379 .0836 AT-SU 0.012 51.377 0.023 61.197 0.026 66.117 0.044 66.564 0.082 69.685 0.152 73.264 0.208 75.053 0.237 77.279 0.254 76.832 0.272 77.726 0.307 77.726 0.330 76.832 0.336 78.621 0.342 76.832 0.354 79.590 0.363 76.385 0.371 77.756 0.395 76.385 0.447 75.937 0.523 73.711 0.652 68.344 0.810 60.302 0.828 62.539 0.836 58.076 0.901 53.603 1.079 37.074 1.158 29.480 1.196 25.464 1.246 16.976 1.301 9.380 1.430 0.000 ; ; ;Aerotech F50 RASP.ENG file made by Tim Van Milligan ;For RockSim www.RockSim.com ;File Created March 2, 2005 ;Thrust curve supplied by Aerotech for the molded case F50T motors. F50T 29 98 4-6-9 0.0336 0.0898 AT-SU 0.013 73.762 0.0326 70.383 0.267 69.82 0.518 67.005 0.792 56.87 0.906 50.676 1 44.482 1.036 39.978 1.107 23.649 1.199 6.194 1.316 1.126 1.43 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. F52T 29 124 5-8-11 .0366 .1214 AT-RMS 0.012 46.899 0.033 61.778 0.056 69.441 0.097 73.483 0.115 76.636 0.130 74.381 0.153 74.820 0.168 78.422 0.182 78.950 0.206 77.963 0.238 77.504 0.258 73.892 0.314 72.974 0.390 72.046 0.428 70.679 0.501 65.699 0.565 62.975 0.688 58.874 0.749 56.150 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 1.420 0.000 ; ; F62T 29 99 0-6-10-14 0.02500 0.10900 AT-RMS 0.01 45.00 0.10 52.00 0.20 66.75 0.50 66.75 0.70 52.00 0.80 39.00 0.90 39.00 1.00 0.00 ; ; ; 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. F72T 24 124 5-10-15 .0368 .0742 AT-SU 0.012 62.586 0.017 84.986 0.020 98.780 0.030 94.748 0.050 90.152 0.069 82.688 0.089 85.556 0.104 80.390 0.136 83.255 0.146 80.960 0.176 82.688 0.198 78.672 0.213 80.960 0.253 80.390 0.315 80.960 0.380 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 0.980 40.195 1.012 29.864 1.034 20.092 1.089 11.480 1.210 0.000 ; ; F101T 24 122 0-5-10-15 0.04830 0.08100 AT-SU 0.01 84.66 0.03 79.66 0.10 79.88 0.30 89.22 0.60 89.22 0.90 74.67 0.96 10.20 0.99 0.00 ; ; ; Aerotech G12TRC 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. G12TRC 32 107 0 .0511 .1310 AT-RMS 0.030 18.549 0.117 19.960 0.239 20.640 0.362 20.111 0.519 18.982 0.694 17.138 0.886 15.020 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 8.550 0.000 ; ; ; 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. G25W 29 124 5-10-15 .0625 .1197 AT-SU 0.035 30.499 0.047 36.712 0.059 41.180 0.130 40.669 0.177 38.969 0.295 38.969 0.343 40.947 0.413 40.380 0.437 38.690 0.484 39.824 0.532 37.845 0.650 37.557 0.721 38.969 0.803 38.690 0.850 37.279 0.980 39.535 1.063 36.434 1.098 38.124 1.252 37.845 1.370 37.279 1.583 37.000 1.819 35.300 1.984 33.610 2.185 31.344 2.315 28.809 2.622 24.286 3.024 18.917 3.390 13.838 3.839 7.624 4.323 4.518 4.783 2.541 5.300 0.000 ; ; ; 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. G33J 29 124 5-7 .0722 .1593 AT-RMS 0.027 22.642 0.061 42.201 0.117 47.354 0.243 46.678 0.340 46.339 0.438 47.384 0.480 50.920 0.508 46.359 0.543 47.732 0.662 45.693 0.851 42.280 1.039 41.266 1.116 42.987 1.193 39.226 1.221 42.310 1.312 38.888 1.326 40.609 1.479 38.221 1.675 35.157 1.843 32.770 1.878 36.888 1.899 32.093 1.997 30.382 2.130 26.622 2.263 23.547 2.444 19.110 2.591 13.977 2.752 8.502 2.892 4.743 3.053 2.014 3.270 0.000 ; ; ; Aerotech G35 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. G35W 29 98 4-7 .0500 .1005 AT-SU 0.013 39.137 0.020 76.220 0.050 64.463 0.134 57.542 0.206 57.532 0.236 64.432 0.248 57.058 0.350 56.121 0.427 55.195 0.476 57.492 0.505 52.414 0.547 53.331 0.757 50.541 0.907 50.057 1.111 44.960 1.321 41.242 1.549 35.681 1.597 36.135 1.627 33.364 1.669 34.281 1.801 30.121 2.005 25.023 2.143 21.316 2.227 19.462 2.298 15.765 2.406 9.761 2.526 6.519 2.652 3.737 2.742 1.881 2.910 0.000 ; ; ; Aerotech G38 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. G38FJ-old 29 98 4-7 .0550 .1062 AT-SU 0.013 66.705 0.018 78.190 0.040 65.480 0.066 56.531 0.163 51.658 0.229 51.658 0.339 51.658 0.423 50.841 0.480 53.282 0.507 51.658 0.560 51.658 0.621 51.658 0.740 50.024 0.899 48.808 0.952 47.592 0.969 48.400 1.048 47.184 1.093 47.991 1.115 45.550 1.242 42.709 1.383 40.677 1.489 37.010 1.590 34.169 1.612 32.535 1.643 32.535 1.828 26.028 1.916 21.962 1.956 15.455 2.013 8.948 2.079 4.474 2.180 0.000 ; ; ;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-SU 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 ; ; ; Aerotech G40 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. G40W-old 29 124 4-7-10 .0624 .1146 AT-SU 0.027 50.310 0.041 66.850 0.096 59.456 0.178 54.878 0.287 53.056 0.390 53.056 0.451 55.793 0.485 50.310 0.533 54.425 0.574 51.225 0.711 53.056 0.909 51.678 1.087 50.762 1.148 51.678 1.251 48.941 1.401 47.110 1.600 42.994 1.675 40.248 1.709 41.616 1.771 37.963 1.900 34.301 2.051 30.186 2.276 25.155 2.454 20.576 2.516 16.461 2.632 11.430 2.769 7.318 2.871 4.116 3.060 0.000 ; ; ;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-SU 0.024 74.325 0.057 67.005 0.252 65.879 0.500 63.063 0.765 60.248 1.000 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 ; ; ; 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. G54W 29 124 6-10-14 .0460 .1365 AT-RMS 0.018 10.953 0.042 39.215 0.083 66.888 0.140 72.075 0.223 74.958 0.250 76.694 0.282 80.156 0.315 79.577 0.336 79.577 0.354 81.640 0.365 77.841 0.374 80.724 0.389 76.694 0.455 76.116 0.523 74.390 0.639 70.928 0.722 67.467 0.820 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 1.510 0.000 ; ; ; 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. G55W 24 177 5-10-15 .0625 .1148 AT-SU 0.009 81.136 0.014 84.650 0.034 80.557 0.084 77.064 0.130 71.823 0.180 72.422 0.206 68.919 0.342 69.538 0.483 68.989 0.513 66.663 0.543 68.420 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 63.310 1.209 62.741 1.325 61.593 1.395 59.277 1.456 57.541 1.486 58.129 1.587 52.320 1.708 40.094 1.824 26.110 1.950 15.630 2.112 7.498 2.258 3.446 2.440 0.000 ; ; G61W 38 106 0-6-10-14 0.06800 0.19400 AT-RMS 0.07 66.89 0.11 74.68 0.21 77.11 0.51 78.57 0.89 76.14 1.18 69.08 1.34 54.73 1.45 40.14 1.50 34.05 1.58 34.54 1.63 27.00 1.67 16.30 1.74 7.05 1.80 2.43 1.85 1.46 1.93 2.68 2.04 0.00 ; ; ; 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. G64W 29 124 4-8-10 .0625 .1512 AT-RMS 0.014 54.325 0.032 81.488 0.059 98.310 0.101 85.021 0.165 83.847 0.274 85.614 0.370 87.390 0.476 86.798 0.503 91.516 0.517 85.614 0.585 83.847 0.723 80.896 0.745 82.070 0.773 77.945 0.883 75.576 0.988 74.401 1.093 69.673 1.262 61.412 1.280 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 2.090 0.000 ; ; ;G67R Data Entered by Tim Van Milligan ;For RockSim: www.RockSim.com ;Based on Aerotech's Reload Kit Instruction Sheet. ;Not Officially Approved by TRA or Aerotech G67R 38 106 0-6-10-14 0.0576 0.191 AT-RMS 0.041 11.795 0.098 57.288 0.119 71.329 0.15 75.822 0.2 80.877 0.3 88.74 0.4 89.301 0.497 90.425 0.606 89.301 0.791 85.932 1.003 75.26 1.19 64.589 1.299 58.411 1.399 55.041 1.423 52.233 1.456 47.74 1.497 22.466 1.518 12.356 1.562 2.808 1.6 0 ; ; G75J 29 194 0-6-10 0.10872 0.22790 AT-RMS 0.01 58.00 0.03 80.00 0.10 71.00 1.08 76.00 1.10 83.30 1.12 76.00 1.90 67.00 2.00 35.00 2.10 9.00 2.20 0.00 ; ; ;G77R Data Entered by Tim Van Milligan ;For RockSim: www.RockSim.com ;Based on Aerotech's Reload Kit Instruction Sheet. ;Not Officially Approved by TRA or Aerotech G77R 29 150 0-6-10-14 0.0554 0.155 AT-RMS 0.04 45.143 0.071 53.951 0.096 60.558 0.139 68.265 0.198 75.972 0.294 83.679 0.396 89.185 0.51 91.387 0.6 93.589 0.801 96.892 1.002 93.589 1.1 89.185 1.134 83.679 1.168 77.073 1.199 59.456 1.236 34.132 1.277 13.213 1.34 0 ; ; G79W 29 150 0-6-10-14 0.06300 0.15700 AT-RMS 0.08 76.51 0.12 85.22 0.17 87.40 0.39 87.94 0.62 88.22 0.91 87.40 1.10 85.77 1.16 87.40 1.21 83.59 1.26 65.62 1.32 23.69 1.36 7.90 1.38 3.27 1.42 0.00 ; ; ; Aerotech G80 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. G80T-old 29 124 4-7-10 .0574 .1049 AT-SU 0.006 101.291 0.013 105.180 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 92.650 0.510 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 0.960 80.388 1.071 74.564 1.207 62.878 1.296 52.639 1.350 37.252 1.382 20.397 1.418 10.139 1.457 4.281 1.500 0.000 ; ; ;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-SU 0.016 110.761 0.049 100.648 0.195 98.537 0.472 96.425 0.635 90.091 0.798 82.348 0.990 63.345 1.121 38.711 1.215 18.3 1.287 5.560 1.41 0 ; ; G80FW 29 124 0-4-7-10 0.06250 0.10550 AT-SU 0.01 111.00 0.02 96.00 0.25 103.00 0.60 103.00 1.40 36.00 1.50 0.00 ; ; G104T 29 124 0-6-10-14 0.04080 0.13560 AT-RMS 0.01 124.60 0.10 117.00 0.20 117.00 0.30 109.91 0.40 109.91 0.50 105.68 0.60 84.56 0.70 71.83 0.80 59.20 0.90 0.00 ; ; G125T 29 124 0-5-10-15 0.05710 0.10500 AT-SU 0.01 118.00 0.02 116.00 0.30 127.00 0.60 122.00 0.80 116.00 0.98 102.00 1.00 0.00 ; ; H45W 38 194 0-10-15 0.19740 0.30700 AT-SU 0.02 76.00 0.04 58.00 1.00 71.00 1.70 71.00 2.40 64.00 3.20 53.00 3.70 44.50 4.80 22.25 5.70 10.00 6.93 0.00 ; ; H55W 29 191 0-6-10-14 0.09300 0.18200 AT-SU 0.01 98.00 0.05 102.00 0.10 98.00 0.25 93.00 0.50 98.00 0.90 98.00 1.30 80.00 1.60 40.00 1.85 22.25 2.20 11.00 2.87 0.00 ; ; H70W 29 229 0-6-10-14 0.12600 0.22100 AT-SU 0.01 102.00 0.05 142.00 0.20 125.00 0.80 125.00 1.20 111.00 1.60 83.00 1.90 42.00 2.20 12.00 2.46 0.00 ; ; H73J 38 152 0-6-10 0.14270 0.29330 AT-RMS 0.08 76.00 0.10 76.00 0.15 72.00 0.50 89.00 0.90 96.00 1.20 96.00 1.50 89.00 1.80 78.00 2.25 44.50 2.40 13.00 2.60 0.00 ; ; H97J 29 238 0-6-10 0.13700 0.28150 AT-RMS 0.01 93.00 0.02 84.00 0.08 107.00 0.11 98.00 0.88 103.00 0.90 108.00 0.92 103.00 1.75 90.00 1.85 96.00 1.90 78.00 2.00 22.00 2.10 0.00 ; ; H112J 38 191 0-6-10 0.19280 0.39000 AT-RMS 0.10 133.42 0.20 109.02 0.50 123.73 0.69 123.73 0.71 129.15 1.00 128.25 1.50 111.19 2.00 90.51 2.50 62.03 2.70 8.14 2.79 0.00 ; ; H123W 38 152 0-6-10-14 0.13140 0.29330 AT-RMS 0.06 146.67 0.11 166.61 0.40 183.00 0.70 183.00 0.91 164.83 1.65 68.28 1.75 22.76 1.85 0.00 ; ; H124FJ 29 247 0-6-10-14 0.16470 0.25000 AT-SU 0.06 48.68 0.12 158.75 0.18 182.64 0.24 188.16 0.30 181.65 0.36 181.31 0.42 181.06 0.48 180.90 0.55 180.84 0.61 180.86 0.67 180.96 0.73 175.26 0.79 175.53 0.85 175.85 0.91 170.44 0.97 165.11 1.03 154.11 1.09 148.91 1.15 138.04 1.21 127.21 1.27 122.08 1.33 111.30 1.39 100.50 1.46 95.34 1.51 90.14 1.58 79.33 1.64 74.08 1.70 57.61 1.76 41.02 1.82 24.29 1.88 12.96 1.94 7.09 2.00 0.00 ; ; H125W 29 330 0-5-10-15 0.18570 0.35300 AT-SU 0.05 307.10 0.08 302.18 0.12 274.29 0.40 218.50 0.69 180.53 1.26 129.40 1.60 89.88 2.00 44.94 2.60 0.00 ; ; H128W 29 194 0-6-10-14 0.09440 0.21450 AT-RMS 0.07 162.71 0.09 183.05 0.20 179.66 0.29 186.80 1.00 150.60 1.14 22.76 1.20 0.00 ; ; H148R 38 152 0-6-10-14 0.150 0.313 AT-RMS 0.027 77.232 0.088 174.296 0.148 185.046 0.208 190.458 0.268 192.497 0.327 191.996 0.388 188.790 0.448 187.548 0.509 182.697 0.570 178.151 0.630 172.906 0.690 169.607 0.750 164.510 0.810 158.375 0.870 153.019 0.930 146.810 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 1.504 0.000 ; ; H165R 29 194 0-6-11-14 0.09100 0.20400 AT-RMS 0.02 55.05 0.06 157.26 0.10 168.51 0.14 173.22 0.19 179.24 0.23 183.95 0.27 187.87 0.31 188.13 0.36 188.92 0.40 190.49 0.44 187.35 0.48 189.18 0.53 186.55 0.57 185.52 0.61 180.81 0.65 177.67 0.69 170.60 0.74 167.20 0.78 158.83 0.82 155.69 0.86 153.33 0.91 136.32 0.95 73.53 0.99 20.67 1.03 4.45 1.05 0.00 ; ; H180W 29 238 0-6-10-14 0.12680 0.26360 AT-RMS 0.05 232.53 0.07 219.23 0.29 266.30 0.32 254.69 0.77 225.68 0.90 235.25 1.10 29.02 1.17 0.00 ; ; ; Aerotech H210 RASP.ENG file made from NAR published data ; File produced Oct 43 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. H210R 29 239 6-10-14 0.1108 0.2470 AT-RMS 0.007 13.977 0.012 80.220 0.022 149.357 0.034 198.849 0.039 207.457 0.052 207.457 0.071 202.077 0.101 208.533 0.163 225.747 0.237 235.431 0.309 245.016 0.396 250.396 0.516 253.623 0.552 250.396 0.574 251.472 0.605 264.920 0.616 254.699 0.634 250.396 0.688 240.810 0.751 232.203 0.790 225.747 0.835 222.520 0.857 218.216 0.872 205.305 0.886 163.344 0.902 108.570 0.919 54.813 0.936 32.248 0.955 13.977 0.990 0.000 ; ; ; Aerotech H220 RASP.ENG file made from NAR published data ; File produced July 4, 2000 ; The total impulse, peak thrust, average thrust and burn time are ; the same as the averaged static test data on the NAR web site in ; the certification file. The curve drawn with these data points is as ; close to the certification curve as can be with such a limited ; number of points (32) allowed with wRASP up to v1.6. H220T 29 238 6-10-14 .1064 .2460 AT-RMS 0.007 214.072 0.013 251.967 0.024 275.730 0.032 265.065 0.036 269.464 0.058 250.567 0.098 250.567 0.165 256.466 0.269 259.566 0.408 259.766 0.449 256.966 0.463 261.366 0.483 254.066 0.576 248.367 0.657 244.168 0.688 245.668 0.742 245.668 0.756 241.368 0.775 222.471 0.793 210.872 0.813 187.575 0.834 161.379 0.852 135.182 0.866 98.817 0.880 65.351 0.897 47.903 0.917 36.285 0.939 23.206 0.964 11.598 1.000 0.00 ; ; H238T 29 194 0-6-10-14 0.08380 0.20210 AT-RMS 0.01 200.27 0.05 211.82 0.09 199.63 0.12 208.61 0.29 220.92 0.35 222.72 0.38 241.82 0.40 246.60 0.43 242.42 0.45 229.28 0.60 223.31 0.68 201.82 0.75 201.55 0.92 0.00 ; ; H242T 38 152 0-6-10-14 0.14480 0.27910 AT-RMS 0.01 210.56 0.03 194.63 0.06 195.32 0.20 211.94 0.34 217.48 0.50 215.40 1.23 132.29 1.26 132.98 1.41 13.16 1.45 0.00 ; ; H268R 29 333 0-6-10-14 0.184 0.362 AT-RMS 0.022 268.095 0.069 332.446 0.116 312.429 0.164 306.810 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 0.590 323.315 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 1.183 0.000 ; ; ; AEROTECH I65 RASP.ENG file made from NAR published data ; File produced OCT 3, 2002 ; The total impulse, peak thrust, average thrust and burn time are ; the same as the averaged static test data on the NAR web site in ; the certification file. The curve drawn with these data points is as ; close to the certification curve as can be with such a limited ; number of points (32) allowed with wRASP up to v1.6. I65W 54 235 0 .3697 .7761 AT-SU 0.086 55.739 0.099 90.267 0.148 113.911 0.296 113.911 0.542 121.767 0.579 123.588 0.825 128.953 0.973 132.593 1.022 138.725 1.071 132.593 1.330 138.629 1.502 139.875 1.724 150.070 2.019 141.886 2.733 131.923 3.140 119.181 3.213 122.151 3.275 114.295 3.570 103.948 3.977 88.791 4.051 93.036 4.100 84.547 4.432 74.229 4.912 58.440 5.725 34.758 6.119 24.430 6.611 13.489 7.166 6.787 7.596 3.729 7.978 1.886 8.114 0.665 8.260 0.000 ; ; I132W 38 335 0-10-15 0.37640 0.51200 AT-SU 0.03 283.37 0.17 176.33 1.78 176.33 2.43 159.18 3.14 115.95 4.00 39.79 4.77 0.00 ; ; I154J 38 250 0-6-10 0.25620 0.49100 AT-RMS 0.07 167.28 0.14 136.09 1.20 135.28 1.71 127.59 2.19 112.19 2.75 77.36 2.98 7.70 3.04 0.00 ; ; I161W 38 191 0-6-10-14 0.19320 0.38480 AT-RMS 0.13 253.07 0.15 209.01 0.35 209.01 0.57 217.82 0.80 217.82 0.97 203.34 1.96 67.36 2.12 0.00 ; ; I195J 38 298 0-6-10 0.31860 0.58240 AT-RMS 0.03 221.79 0.07 345.76 0.13 372.88 0.28 304.12 0.41 265.18 0.49 265.18 0.70 309.08 0.76 391.28 0.86 232.45 1.46 185.96 1.90 127.85 2.23 18.40 2.30 0.00 ; ; I200W 29 333 0-6-10-14 0.18730 0.36400 AT-RMS 0.00 479.50 0.01 305.00 0.02 297.00 0.03 282.00 0.15 276.00 0.20 272.00 0.30 265.00 0.40 252.00 0.50 240.00 0.60 223.00 0.80 221.00 1.00 221.00 1.10 218.00 1.20 177.00 1.40 89.00 1.58 44.00 1.63 0.00 ; ; I211W 38 248 0-6-10-14 0.25300 0.47630 AT-RMS 0.05 378.98 0.09 421.67 0.12 316.51 0.40 315.47 1.28 238.43 1.60 132.23 1.90 0.00 ; ; I218R 38 191 0-6-10-14 0.192 0.375 AT-RMS 0.027 136.078 0.088 275.030 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 0.570 266.041 0.630 261.907 0.690 256.366 0.750 250.565 0.810 242.206 0.870 234.607 0.930 225.488 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 1.504 0.000 ; ; I284W 38 298 0-6-10-14 0.31790 0.56780 AT-RMS 0.10 490.32 0.31 490.32 0.45 519.73 0.55 526.15 0.80 482.52 0.85 445.30 1.25 284.89 1.32 275.91 1.50 42.35 1.57 0.00 ; ; I285R 38 250 0-6-10-14 0.254 0.498 AT-RMS 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 0.507 361.900 0.568 351.928 0.628 346.109 0.687 340.993 0.749 329.382 0.810 321.625 0.870 310.856 0.930 295.955 0.990 283.704 1.050 269.655 1.110 253.419 1.170 240.222 1.230 224.116 1.290 204.118 1.350 118.730 1.410 23.483 1.471 2.046 1.502 0.000 ; ; ; Aerotech I300 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. I300T 38 250 6-10-14 .2216 .4445 AT-RMS 0.012 257.509 0.018 389.185 0.024 460.765 0.037 474.430 0.063 437.895 0.113 409.382 0.231 386.710 0.380 366.909 0.507 355.722 0.669 327.406 0.822 299.091 0.958 279.290 1.120 253.846 1.177 245.332 1.199 245.332 1.219 228.204 1.247 188.206 1.276 151.080 1.311 128.210 1.333 99.697 1.359 68.243 1.384 33.948 1.420 0.000 ; ; I357T 38 203 0-6-10-14 0.17440 0.36350 AT-RMS 0.02 356.19 0.05 355.07 0.34 343.79 0.66 306.60 1.03 233.33 1.15 199.51 1.22 85.67 1.30 18.04 1.37 0.00 ; ; I366R 38 298 0-6-10-14 0.318 0.562 AT-RMS 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 0.570 430.236 0.630 421.524 0.690 411.757 0.750 398.876 0.810 387.496 0.870 375.430 0.930 361.325 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 1.504 0.000 ; ; I435T 38 298 0-6-10-14 0.28430 0.52690 AT-RMS 0.04 845.88 0.10 666.83 0.59 574.21 1.00 358.11 1.12 146.13 1.26 0.00 ; ; I600R 38 337 0-6-10-14 0.32370 0.61700 AT-RMS 0.01 23.78 0.01 457.95 0.03 797.84 0.05 758.92 0.51 611.89 0.98 396.78 1.00 363.71 1.01 261.21 1.04 99.19 1.07 19.84 1.09 0.00 ; ; J90W 54 243 0-6-10-14 0.42600 0.83410 AT-RMS 0.10 133.00 0.17 139.74 0.51 166.10 1.00 187.41 1.48 187.41 2.11 169.49 3.28 122.03 4.08 82.59 5.02 45.38 5.88 19.97 6.85 0.00 ; ; J125W 54 368 0-20 0.63870 1.10000 AT-SU 0.12 233.41 0.20 233.41 0.53 259.24 0.86 274.40 1.21 284.75 1.53 283.37 2.04 277.85 5.11 90.32 6.75 22.06 7.75 0.00 ; ; J135W 54 368 0-6-10-14 0.63300 1.12570 AT-RMS 0.09 250.60 0.14 237.53 1.20 257.87 1.59 256.42 2.24 246.63 3.02 211.04 4.33 115.51 6.00 23.57 6.83 0.00 ; ; J180T 54 230 0-6-10-14 0.43710 0.84090 AT-RMS 0.09 321.55 0.12 300.24 0.39 316.71 0.53 318.64 0.65 316.71 1.04 290.56 2.39 165.62 3.29 75.55 4.08 16.47 4.50 0.00 ; ; J275W 54 230 0-6-10-14-18 0.47200 0.86420 AT-RMS 0.10 295.34 0.26 295.34 0.87 336.92 1.06 341.17 1.47 332.68 2.44 223.20 2.62 185.01 2.98 152.76 3.48 0.00 ; ; J315R 54 243 0-6-10-14-18 0.429 0.863 AT-RMS 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 0.780 372.962 0.884 368.988 0.989 366.978 1.093 358.752 1.197 351.302 1.301 339.336 1.406 325.202 1.510 311.322 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 2.604 0.000 ; ; J350W 38 337 0-6-10-14 0.38110 0.66500 AT-RMS 0.02 913.32 0.10 666.05 0.60 445.52 1.46 291.82 1.62 51.23 1.78 0.00 ; ; J415W 54 326 0-6-10-14-18 0.69330 1.19890 AT-RMS 0.05 577.97 0.08 422.03 0.51 533.90 1.20 542.37 2.54 364.41 2.57 364.41 2.91 35.59 3.03 0.00 ; ; J420R 38 337 0-6-10-14 0.381 0.659 AT-RMS 0.031 61.083 0.095 563.470 0.160 525.283 0.224 521.242 0.288 527.371 0.352 537.088 0.418 535.138 0.481 534.623 0.545 530.245 0.610 526.447 0.674 517.203 0.738 510.279 0.802 500.887 0.868 479.450 0.931 460.675 0.995 438.594 1.060 409.647 1.124 383.454 1.188 361.024 1.252 339.741 1.318 319.194 1.381 296.714 1.445 195.191 1.510 61.984 1.575 7.220 1.608 0.000 ; ; J460T 54 230 0-6-10-14-18 0.41540 0.83290 AT-RMS 0.03 645.76 0.05 489.83 0.29 533.90 0.51 545.76 0.80 545.76 1.07 511.86 1.49 413.56 1.60 398.31 1.75 140.68 1.91 0.00 ; ; J540R 54 314 0-6-10-14-18 0.62100 1.10000 AT-RMS 0.04 498.76 0.13 639.62 0.22 649.32 0.31 657.97 0.40 664.02 0.49 666.92 0.58 663.70 0.68 658.40 0.77 651.23 0.85 638.51 0.94 626.40 1.03 612.56 1.13 590.09 1.22 562.39 1.31 536.88 1.40 511.61 1.49 490.35 1.58 468.98 1.67 451.34 1.76 430.18 1.85 414.55 1.94 398.12 2.03 305.88 2.12 55.54 2.21 1.52 2.25 0.00 ; ; J570W 38 479 0-6-10-14 0.55200 0.88610 AT-RMS 0.02 1870.20 0.05 1006.60 0.07 1085.10 0.09 1080.48 0.10 1269.79 0.11 1265.18 0.13 1052.77 0.15 1001.98 0.20 1131.27 0.24 1001.98 0.28 1071.24 0.29 1029.69 0.31 1066.63 0.70 646.44 1.28 355.54 1.29 429.42 1.30 262.64 1.83 0.00 ; ; J800T 54 314 0-6-10-14-18 0.61940 1.13390 AT-RMS 0.04 1317.31 0.10 722.40 0.20 781.24 0.45 797.58 0.75 781.24 1.20 725.67 1.53 624.33 1.60 624.33 1.81 98.06 1.88 0.00 ; ; K185W 54 410 0-6-10-14 0.78280 1.41750 AT-RMS 0.14 300.00 0.19 322.07 0.27 316.35 0.30 300.82 0.44 300.82 0.86 334.55 1.19 342.00 1.65 335.38 2.33 317.16 3.07 269.96 3.62 226.07 4.10 180.52 4.66 136.63 5.29 90.26 6.12 40.58 6.87 0.00 ; ; K250W 54 673 0-20 1.54310 2.24400 AT-SU 0.07 356.34 0.26 380.18 0.46 424.10 0.54 405.28 1.02 405.28 1.10 506.91 1.23 404.02 1.31 414.06 3.00 416.57 5.04 303.64 7.61 97.87 9.35 0.00 ; ; K458W 98 275 0-20 1.45000 3.10620 AT-RMS 0.07 330.57 0.37 365.93 1.10 512.00 2.01 615.01 3.00 631.92 4.15 442.81 5.12 221.40 5.95 119.93 6.08 16.91 6.14 0.00 ; ; K550W 54 410 0-6-10-14-18 0.88910 1.51510 AT-RMS 0.01 572.20 0.06 665.15 0.09 665.15 0.11 634.17 0.51 751.91 0.80 799.42 1.16 803.55 1.44 646.56 1.91 448.25 2.48 245.82 2.83 26.85 2.93 0.00 ; ; K560W 75 396 0-20 1.42490 2.77400 AT-RMS 0.03 516.61 0.18 648.18 0.21 624.96 0.50 672.50 0.75 720.50 1.02 762.34 1.50 799.10 2.00 799.00 2.50 634.50 3.00 460.00 3.50 360.00 4.08 249.60 4.41 25.15 4.50 0.00 ; ; K650T 98 289 0-20 1.28000 2.95700 AT-RMS 0.03 559.74 0.48 643.61 0.98 705.60 1.59 742.06 1.90 747.53 2.22 743.88 2.72 674.60 3.43 561.56 3.50 561.56 3.67 0.00 ; ; K695R 54 410 0-6-10-14-18 0.93100 1.50600 AT-RMS 0.04 618.61 0.13 727.84 0.22 752.00 0.31 812.48 0.40 900.13 0.50 884.76 0.58 873.46 0.68 864.56 0.77 849.67 0.86 838.89 0.95 822.55 1.04 806.24 1.13 781.34 1.22 753.97 1.31 728.47 1.40 697.63 1.49 672.98 1.58 646.66 1.67 620.90 1.76 595.57 1.85 571.72 1.94 546.82 2.03 272.82 2.12 57.95 2.21 4.51 2.25 0.00 ; ; K700W 54 579 0-20 1.23200 2.05900 AT-RMS 0.03 1018.73 0.07 1206.97 0.09 1098.23 0.12 1021.68 0.71 1021.68 1.30 906.85 2.31 577.09 2.76 338.60 2.96 156.05 3.20 0.00 ; ; K780R 75 289 0-20 1.26784 2.9344 AT-RMS 0.053 383.290 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 1.013 947.130 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 2.217 812.360 2.337 779.614 2.457 747.866 2.578 726.819 2.697 729.258 2.817 279.891 2.940 10.969 3.063 0.000 ; ; K1050W 54 676 0-20 1.36220 2.25900 AT-SU 0.04 1949.17 0.05 1336.13 0.15 1247.05 0.40 1325.65 0.90 1346.61 1.71 1121.30 1.78 1121.30 2.27 0.00 ; ; K1100T 54 398 0-6-10-14-18 0.77330 1.36800 AT-RMS 0.05 1995.16 0.11 1249.40 0.20 1152.54 0.69 1133.17 1.03 1016.95 1.35 915.25 1.40 799.03 1.43 576.27 1.56 72.64 1.60 0.00 ; ; K1275R 54 569 0-20 1.30800 2.06100 AT-RMS 0.04 1282.62 0.12 1557.99 0.20 1540.20 0.28 1526.78 0.36 1500.69 0.44 1456.58 0.52 1425.79 0.60 1390.42 0.68 1355.11 0.76 1323.31 0.84 1282.83 0.92 1247.80 1.00 1194.42 1.08 1150.98 1.16 1108.22 1.24 1068.75 1.32 1036.92 1.40 997.44 1.48 964.57 1.56 933.30 1.64 889.99 1.72 599.47 1.80 134.56 1.88 5.63 1.96 0.20 2.00 0.00 ; ; L850W 75 531 0-20 2.09480 3.74100 AT-RMS 0.05 903.39 0.10 1284.26 0.12 1101.69 0.24 1057.98 0.36 1066.59 0.47 1091.47 0.55 1113.23 0.63 1131.89 0.73 1153.66 0.83 1173.44 0.92 1187.86 1.01 1203.41 1.72 1203.41 1.82 1178.54 1.91 1123.09 2.01 1088.07 2.10 1043.40 2.20 1013.17 2.30 974.94 2.40 934.75 2.50 904.66 2.60 872.45 2.69 837.26 2.79 792.59 2.89 762.62 2.99 727.96 3.09 702.93 3.18 660.77 3.28 631.23 3.38 605.48 3.48 580.03 3.58 563.68 3.67 526.34 3.77 432.02 3.87 301.35 3.97 191.54 4.07 106.58 4.16 73.99 4.26 40.42 4.34 15.55 4.43 0.00 ; ; L952W 98 443 0-20 2.72800 5.01200 AT-RMS 0.00 1.51 0.20 799.03 0.40 801.94 1.18 947.22 2.00 1089.59 2.41 1133.17 2.80 1133.17 3.40 1034.25 5.75 351.57 6.00 313.80 6.46 0.00 ; ; L1120W 75 665 0-20 2.77780 4.70800 AT-RMS 0.08 1599.30 0.14 1456.66 0.20 1440.00 0.76 1557.39 1.25 1557.39 1.80 1476.03 2.14 1305.57 2.69 1069.25 3.21 856.17 3.77 666.34 4.36 61.99 4.43 0.00 ; ; L1150R 75 531 0-20 2.06528 3.6736 AT-RMS 0.053 935.855 0.175 1292.642 0.300 1260.926 0.425 1241.482 0.550 1257.058 0.675 1272.287 0.800 1287.605 0.925 1301.012 1.048 1309.708 1.170 1308.417 1.295 1304.830 1.420 1285.265 1.545 1267.657 1.670 1255.624 1.795 1227.212 1.920 1202.443 2.043 1182.617 2.165 1150.712 2.290 1117.909 2.415 1081.739 2.540 1037.547 2.665 1007.091 2.790 1008.911 2.915 643.124 3.040 64.371 3.165 0.000 ; ; L1500T 98 443 0-20 2.66000 5.01110 AT-RMS 0.09 1378.70 0.37 1508.85 0.66 1598.57 1.10 1684.21 1.70 1684.14 2.00 1647.51 2.41 1570.02 2.75 1455.84 3.11 1292.72 3.19 1341.66 3.43 48.94 3.47 0.00 ; ; M1297W 75 666 0-20 2.73280 4.63680 AT-RMS 0.01 1334.61 0.05 2048.98 0.20 1827.47 0.38 1827.47 0.48 1733.33 1.80 1594.88 3.20 1035.57 3.40 991.26 3.60 537.16 3.88 271.35 4.17 0.00 ; ; M1315W 75 801 0-20 3.49940 5.67500 AT-RMS 0.08 2269.63 0.11 1720.29 0.15 1980.50 0.23 1720.29 1.02 1720.29 1.18 1683.39 2.15 1655.24 2.94 1440.98 3.60 1205.31 3.72 1205.31 4.46 471.35 5.40 0.00 ; ; M1419W 98 597 0-20 3.99000 6.93070 AT-RMS 0.00 0.22 0.10 1380.80 0.21 1221.47 0.38 1221.47 1.79 1468.28 2.51 1510.90 3.35 1495.40 4.10 1282.32 4.66 1057.63 5.53 685.71 6.31 526.88 6.84 100.73 7.08 0.00 ; ; M1550R 75 800 0-20 3.49300 5.71500 AT-RMS 0.07 1720.76 0.21 2125.33 0.36 1995.95 0.50 1908.44 0.65 1868.71 0.79 1835.50 0.94 1808.66 1.08 1796.30 1.22 1785.42 1.37 1773.15 1.51 1746.59 1.66 1715.71 1.80 1689.63 1.95 1660.72 2.09 1633.28 2.23 1606.04 2.38 1570.22 2.52 1534.71 2.67 1503.35 2.81 1461.32 2.96 1427.57 3.10 1393.23 3.24 939.96 3.39 268.50 3.53 4.99 3.61 0.00 ; ; M1600R 98 579 0-20 4.08200 7.00400 AT-RMS 0.09 1370.36 0.27 1626.63 0.45 1672.65 0.63 1720.60 0.81 1763.29 0.99 1801.28 1.17 1829.83 1.35 1845.15 1.53 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 1726.90 2.97 1689.29 3.15 1641.58 3.33 1581.59 3.51 1511.04 3.69 1431.40 3.87 1361.03 4.05 1234.57 4.23 621.21 4.41 42.47 4.50 0.00 ; ; M1939W 98 751 0-20 5.74000 9.12000 AT-RMS 0.00 1.33 0.11 2185.23 0.16 2003.63 0.38 2003.63 0.95 2130.75 1.52 2209.44 2.75 2191.28 3.00 2136.80 4.22 1573.85 4.85 1192.49 5.53 944.31 5.76 587.17 5.89 484.26 5.97 169.49 6.20 0.00 ; ; M2000R 98 732 0-20 5.72900 9.09900 AT-RMS 0.09 1530.96 0.28 2186.27 0.47 2166.70 0.66 2187.24 0.84 2219.07 1.03 2248.07 1.22 2273.74 1.41 2298.31 1.60 2309.75 1.78 2315.71 1.97 2316.16 2.16 2306.31 2.35 2282.23 2.54 2252.10 2.73 2209.64 2.92 2168.80 3.10 2117.18 3.29 2067.53 3.48 2004.51 3.67 1934.44 3.86 1831.48 4.04 1745.63 4.23 1504.27 4.42 649.80 4.61 58.18 4.70 0.00 ; ; M2400T 98 597 0-20 3.99000 6.78880 AT-RMS 0.05 2816.80 0.10 2503.07 0.14 2503.07 0.48 2619.01 0.90 2694.04 1.20 2714.50 1.54 2694.04 2.07 2530.35 2.60 2225.00 2.91 1998.36 3.00 1998.36 3.05 1398.17 3.14 900.29 3.20 0.00 ; ; M2500T 98 751 0-20 4.71120 8.84450 AT-RMS 0.00 1.33 0.04 3001.21 0.07 2732.45 0.54 2813.07 1.15 2839.95 1.78 2813.07 3.38 2418.89 3.47 2436.80 3.55 1648.43 3.71 161.26 3.85 0.00 ; ; N2000W 98 1046 0-20 7.75400 11.65300 AT-RMS 0.05 3383.53 0.12 2938.98 0.30 2831.96 0.50 2864.89 4.88 1802.91 5.00 1786.44 5.47 1169.01 6.07 592.74 6.56 362.23 6.90 0.00 ; ; N4800T 98 1194 0-20 9.7664 14.784 AT-RMS 0.098 4752.717 0.301 6007.533 0.506 5594.225 0.710 5270.361 0.914 5150.120 1.119 5108.054 1.324 5086.206 1.528 5031.651 1.731 4941.811 1.936 4800.400 2.140 4664.876 2.344 4527.840 2.549 4401.003 2.754 4263.565 2.958 4120.406 3.161 3971.136 3.366 3876.421 3.570 3916.232 3.774 3913.510 3.979 3312.758 4.184 1649.267 4.388 523.361 4.591 327.209 4.796 251.041 5.001 128.177 5.206 0.000 ; ;*AMW*AMW*AMW* ;Animal Motor Works, Inc. ; ;WRasp Reload 0erformance Data ;Revision 4A released June 8, 2004 ; ;Special thanks to the people who have contributed ; ; ; 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 0-20 0.5481 1.2101 AMW 0.02 129.64 0.03 205.95 0.05 265.00 0.06 316.51 0.09 326.05 0.13 314.60 0.18 301.25 0.24 299.34 0.35 312.69 0.50 326.05 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 2.60 347.03 2.65 335.59 2.69 310.79 2.75 249.73 2.81 175.43 2.84 108.65 2.90 53.38 2.92 20.98 2.95 0.00 ; 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 0-20 0.5983 1.2491 AW 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 2.820 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 0-20 0.558 1.2314 AMW 00.043 246.550 00.060 317.381 00.081 344.709 00.107 358.372 00.150 356.062 00.201 365.204 00.308 392.532 00.568 435.734 00.863 458.339 01.094 469.240 01.209 467.180 01.466 460.148 01.705 443.972 01.923 423.275 02.132 409.411 02.303 413.831 02.402 420.563 02.470 413.831 02.517 395.445 02.543 347.421 02.568 265.238 02.598 128.198 02.615 68.801 02.632 25.398 02.660 0.000 ; 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 0-20 0.5331 1.1964 AMW 0.009 251.586 0.016 376.074 0.030 413.450 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 1.299 563.180 1.334 555.319 1.470 560.042 1.588 559.841 1.764 546.980 1.921 516.838 1.993 496.743 2.025 499.154 2.047 479.160 2.086 414.354 2.115 344.525 2.141 252.290 2.177 140.161 2.213 82.780 2.239 50.347 2.271 27.861 2.296 12.860 2.330 0.000 ; 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 0-20 0.5560 1.2131 AMW 0.015 225.429 0.041 348.180 0.071 388.127 0.194 422.453 0.385 459.490 0.699 502.347 0.968 528.042 1.200 536.573 1.454 543.150 1.674 533.763 1.887 522.321 2.044 519.410 2.108 525.131 2.164 528.042 2.197 488.095 2.250 419.543 2.283 333.928 2.328 231.150 2.354 176.950 2.392 111.309 2.418 68.501 2.436 37.106 2.490 0.000 ; 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 0-20 0.3265 0.0 AMW 0.008 448.516 0.027 506.086 0.048 448.426 0.080 450.851 0.101 498.901 0.117 532.131 0.163 563.565 0.227 616.105 0.285 666.398 0.312 668.643 0.320 692.444 0.362 728.024 0.442 757.108 0.493 771.477 0.528 778.578 0.576 779.000 0.631 778.662 0.706 716.631 0.754 620.146 0.770 598.591 0.813 526.293 0.887 439.895 0.973 343.841 1.074 230.949 1.095 238.089 1.111 214.110 1.130 185.279 1.194 98.836 1.255 36.368 1.300 0.000 ; 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 0-20 0.946 2.3456 AMW 0.049 138.157 0.068 381.241 0.084 454.750 0.106 481.536 0.164 488.182 0.291 514.867 0.435 545.982 0.666 561.490 0.868 565.730 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 2.501 411.350 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 4.510 0.000 ; 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 75 000 0-20 0.8816 2.8349 AMW 0.030 78.903 0.045 227.900 0.064 449.955 0.069 508.417 0.094 555.187 0.151 563.956 0.362 625.442 0.562 651.850 0.825 660.620 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 3.325 232.940 3.510 171.757 3.732 107.650 3.861 58.018 3.959 40.550 4.036 20.149 4.110 0.000 ; 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 0-20 0.826 0.0 AMW 0.028 699.309 0.039 799.337 0.090 765.845 0.157 770.311 0.258 785.941 0.410 804.000 0.572 794.425 0.707 794.425 0.886 792.192 0.998 783.261 1.150 752.002 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 3.270 78.058 3.433 55.686 3.478 48.987 3.556 28.909 3.700 0.000 ; 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 0-20 0.7286 1.4925 AW 0.022 127.831 0.041 386.016 0.063 548.326 0.096 521.308 0.134 499.129 0.180 486.830 0.285 486.830 0.478 501.649 0.731 523.727 1.096 553.266 1.433 577.962 1.601 588.290 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 2.599 331.980 2.620 297.501 2.670 226.226 2.707 157.370 2.740 98.353 2.799 49.176 2.853 17.208 2.940 0.000 ;; 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 0-20 0.7967 1.6160 AW 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 0.326 508.660 0.542 564.745 0.755 613.831 1.010 645.423 1.170 657.230 1.273 648.922 1.510 638.425 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 2.040 564.745 2.132 536.652 2.207 540.251 2.291 522.656 2.357 487.566 2.420 375.297 2.478 242.033 2.529 140.361 2.583 66.651 2.660 0.000 ; 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 0-20 0.750 1.5866 AMW 0.023 229.130 0.046 415.135 0.059 485.264 0.078 512.268 0.106 525.670 0.154 523.050 0.211 528.390 0.261 536.451 0.369 560.734 0.511 587.738 0.657 603.860 0.770 612.022 1.096 625.730 1.358 620.083 1.627 612.022 1.839 603.860 2.057 590.459 2.218 598.520 2.335 609.301 2.385 601.240 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 2.620 0.000 ; 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 0-20 0.9146 1.8151 AMW 0.020 364.42 0.030 664.79 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 1.430 651.24 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 3.040 0.00 ; 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 0-20 1.2233 2.9129 AW 0.010 412.229 0.029 522.21 0.059 547.215 0.083 524.8 0.122 497.305 0.181 484.852 0.333 495.113 0.690 560.464 1.195 643.548 1.400 673.833 1.420 708.799 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 4.070 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 0-20 1.231 2.7688 AMW 0.030 165.845 0.053 309.120 0.077 361.916 0.142 392.042 0.527 501.412 0.988 606.905 1.515 682.370 2.101 730.593 2.355 737.580 2.692 731.289 3.000 712.497 3.361 671.036 3.503 663.479 3.586 659.701 3.645 633.353 3.692 573.000 3.734 444.838 3.775 297.785 3.828 162.066 3.864 98.015 3.905 41.471 3.950 0.000 ; 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 0-20 0.931 1.8087 AMW 0.022 308.257 0.045 566.480 0.058 620.440 0.081 639.668 0.135 639.668 0.229 643.494 0.351 662.823 0.594 701.380 0.810 724.434 0.999 743.763 1.151 751.220 1.381 747.588 1.610 736.001 1.835 709.031 2.073 685.876 2.244 674.400 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 2.770 0.000 ; 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 0-20 1.0140 1.9145 AW 0.016 294.054 0.035 398.582 0.086 506.299 0.153 496.434 0.264 506.100 0.461 558.114 0.722 629.560 0.983 688.052 1.116 714.060 1.193 785.805 1.409 788.794 1.737 804.560 2.074 781.420 2.195 764.879 2.226 781.221 2.277 764.779 2.398 751.527 2.440 744.950 2.468 718.843 2.484 666.529 2.525 418.112 2.551 218.821 2.573 120.770 2.595 52.144 2.620 0.000 ; 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 0-20 0.754 1.4831 AMW 0.014 359.559 0.022 625.425 0.030 737.756 0.047 771.505 0.082 786.516 0.106 771.505 0.144 775.233 0.272 786.516 0.477 812.710 0.693 842.632 0.970 847.060 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 1.950 393.208 1.982 337.093 2.035 292.160 2.073 228.489 2.111 153.535 2.155 86.137 2.193 37.446 2.240 0.000 ; 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 0-20 0.9140 1.7866 AMW 0.017 516.316 0.035 745.845 0.046 817.592 0.090 860.560 0.191 889.338 0.270 908.424 0.438 918.017 0.689 945.892 0.996 955.090 1.325 922.713 1.557 894.035 1.726 874.949 1.849 884.542 1.920 894.035 1.954 894.035 1.984 855.863 2.011 741.048 2.049 592.859 2.079 492.433 2.113 430.280 2.154 377.719 2.196 329.854 2.237 243.818 2.275 152.986 2.309 71.716 2.339 33.465 2.380 0.000 ; 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 0-20 0.8874 1.7949 AMW 0.011 771.836 0.025 1204.520 0.039 1083.244 0.053 1158.054 0.067 1036.364 0.085 1110.176 0.099 1022.399 0.135 982.102 0.220 968.835 0.404 1010.430 0.566 1044.343 0.701 1079.254 0.867 1106.186 0.995 1134.115 1.211 1114.166 1.313 1101.199 1.430 1067.285 1.529 1020.404 1.579 993.772 1.642 892.430 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 1.970 0.000 ; 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 0-20 1.3573 2598.5 AMW 0.017 526.644 0.029 901.850 0.038 1098.918 0.046 1151.722 0.076 1112.867 0.130 1060.063 0.219 1053.089 0.336 1053.089 0.479 1059.066 0.609 1091.944 0.866 1136.778 1.046 1176.630 1.164 1175.634 1.202 1228.437 1.239 1208.511 1.315 1215.486 1.353 1267.293 1.387 1228.437 1.487 1241.389 1.538 1260.319 1.634 1290.900 1.723 1281.241 1.794 1266.297 1.836 1207.515 1.933 1049.103 1.992 851.437 2.080 666.923 2.118 640.521 2.193 462.582 2.269 212.311 2.378 119.854 2.510 0.000 ; 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 0-20 1.297 2.5560 AMW 0.019 1155.063 0.045 1426.120 0.094 1248.230 0.161 1112.988 0.239 1128.015 0.343 1113.990 0.377 1149.053 0.440 1121.003 0.544 1221.182 0.633 1178.105 0.674 1221.182 0.737 1193.131 0.883 1200.144 1.009 1194.133 1.057 1236.208 1.188 1137.031 1.299 1145.045 1.396 1087.943 1.516 954.104 1.631 855.228 1.717 827.077 1.777 650.061 1.848 465.932 1.930 303.141 2.023 147.463 2.083 83.879 2.132 41.484 2.180 0.000 ;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 0-20 1.3999 2.6658 AW 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 1092.053 0.878 1220.294 1.077 1269.387 1.158 1311.466 1.235 1293.432 1.448 1330.501 1.577 1318.479 1.672 1319.481 1.721 1337.515 1.759 1337.515 1.805 1337.515 1.829 1331.503 1.856 1384.670 1.889 1277.402 1.906 1216.287 1.938 1052.980 1.960 871.338 1.988 659.239 2.027 453.352 2.062 301.967 2.115 138.460 2.168 41.608 2.200 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 0-20 1.1931 0.000 AMW 0.024 221.872 0.033 399.330 0.048 467.560 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 2.258 821.140 2.582 817.853 2.912 801.072 3.136 773.941 3.255 750.126 3.322 743.393 3.370 729.828 3.418 688.830 3.461 593.368 3.499 484.140 3.532 368.179 3.570 248.802 3.618 149.824 3.661 61.135 3.720 0.000 ;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 0-20 1.7623 3.6987 AMW 0.025 140.882 0.064 209.474 0.108 360.055 0.204 652.185 0.360 641.518 0.373 693.745 0.418 683.28 0.528 730.073 0.670 761.268 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 3.550 705.72 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 4.050 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 0-20 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 1.260 1041.158 1.284 1071.366 1.378 1053.241 1.607 1101.573 1.917 1142.857 2.208 1173.560 2.413 1160.982 2.624 1107.615 2.866 976.211 3.053 886.897 3.208 839.270 3.314 827.388 3.382 809.465 3.432 720.252 3.495 547.564 3.570 345.273 3.627 214.273 3.714 77.382 3.790 0.000 ; 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 0-20 1.9188 3.9388 AW 0.020 258.765 0.024 368.224 0.032 328.375 0.076 427.947 0.100 567.267 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 1079.605 1.024 1174.482 1.308 1229.412 1.606 1288.335 1.782 1298.25 1.983 1293.329 2.256 1239.399 2.525 1184.47 2.822 1129.541 3.038 1069.618 3.111 1044.650 3.135 995.114 3.183 835.92 3.239 552.286 3.299 268.652 3.327 164.187 3.339 84.59 3.360 44.782 3.400 0.000 ; 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 0-20 1.717 3.5922 AMW 0.024 406.295 0.043 812.489 0.052 895.202 0.088 929.641 0.314 991.550 0.626 1087.695 0.988 1163.440 1.346 1218.986 1.638 1246.254 1.864 1257.910 2.247 1254.839 2.600 1218.986 2.766 1211.917 2.851 1197.778 2.942 1204.847 3.002 1226.056 3.033 1204.847 3.089 1040.228 3.124 874.499 3.150 660.999 3.191 461.336 3.232 275.408 3.268 144.622 3.303 75.744 3.339 41.316 3.390 0.000 ; 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 0-20 1.346 2.5881 AMW 0.013 681.489 0.029 1116.882 0.041 1196.301 0.079 1210.375 0.147 1203.338 0.257 1218.417 0.366 1225.454 0.567 1254.608 0.824 1282.756 1.059 1311.909 1.267 1340.230 1.459 1311.909 1.622 1297.835 1.713 1290.798 1.785 1268.682 1.830 1218.417 1.886 1080.692 1.969 819.214 2.048 558.240 2.108 376.985 2.156 246.498 2.205 144.963 2.269 72.501 2.350 0.000 ; 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 0-20 1.642 0.0 AMW 0.012 947.531 0.034 1002.766 0.055 956.063 0.109 947.531 0.238 986.151 0.485 1058.001 0.732 1138.834 1.027 1232.239 1.312 1317.562 1.527 1359.774 1.624 1372.798 1.726 1379.400 1.866 1368.307 1.930 1343.159 2.075 1296.007 2.275 1211.134 2.469 1130.301 2.609 1066.534 2.738 998.724 2.760 964.595 2.803 934.957 2.879 790.357 2.928 624.652 2.993 433.483 3.031 254.979 3.080 140.243 3.100 67.989 3.140 0.000 ; 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 0-20 1.314 2.5454 AMW 0.014 710.467 0.025 1247.640 0.039 1384.132 0.053 1447.829 0.074 1420.530 0.120 1447.829 0.276 1474.116 0.475 1519.614 0.712 1555.001 0.942 1586.740 1.147 1562.078 1.360 1534.779 1.484 1551.967 1.537 1551.967 1.569 1497.370 1.590 1406.376 1.604 1451.873 1.615 1333.580 1.640 1168.778 1.689 986.687 1.753 767.749 1.824 512.503 1.891 275.512 1.933 147.816 1.987 74.737 2.060 0.000 ; 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 0-20 2.9673 5.6322 AMW 0.026 728.705 0.046 1381.698 0.066 1609.638 0.092 1662.710 0.151 1609.638 0.242 1592.567 0.478 1592.567 1.041 1592.567 1.710 1635.746 2.299 1643.779 2.672 1601.605 3.092 1508.220 3.197 1500.186 3.249 1423.872 3.301 1338.520 3.386 1067.402 3.524 788.050 3.721 440.617 3.779 389.807 3.838 381.272 3.904 364.402 3.976 305.058 4.055 194.903 4.140 93.214 4.230 0.000 ; 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 0-20 3.000 5.5248 AMW 0.022 713.002 0.032 1254.682 0.055 1473.369 0.078 1569.108 0.156 1569.108 0.352 1559.030 0.642 1597.326 0.974 1644.691 1.289 1702.135 1.520 1739.422 1.918 1796.866 2.279 1814.830 2.481 1796.866 2.707 1739.422 2.968 1644.691 3.058 1616.473 3.135 1520.735 3.218 1378.638 3.284 1217.394 3.332 1065.220 3.344 1140.803 3.368 1016.846 3.410 741.522 3.500 522.935 3.613 275.727 3.691 171.120 3.768 66.553 3.850 0.000 ; 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 0-20 3.375 5.8510 AMW 0.012 1326.734 0.018 894.224 0.069 1177.465 0.099 1244.682 0.211 1319.317 0.271 1535.340 0.434 1714.277 0.642 1990.101 0.779 2012.353 1.069 2191.291 1.257 2263.514 1.460 2267.928 1.658 2269.000 1.959 2268.484 2.254 2258.044 2.508 2183.873 2.564 2235.792 2.595 2153.741 2.687 2124.073 2.733 2064.272 2.779 1833.415 2.820 1468.123 2.857 1118.128 2.903 752.835 2.970 424.814 3.042 201.235 3.149 59.614 3.200 0.000 ; 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 0-20 2.733 5.4225 AMW 0.018 1109.215 0.044 1761.753 0.061 1910.647 0.085 1938.624 0.159 1929.634 0.290 1956.615 0.409 2031.562 0.438 1974.602 0.569 2011.576 0.815 2104.510 1.073 2197.444 1.401 2280.386 1.688 2324.700 1.905 2297.374 2.073 2241.413 2.254 2138.486 2.397 2063.539 2.479 2016.572 2.540 2025.566 2.581 2006.579 2.630 1885.666 2.716 1493.942 2.805 1120.207 2.887 840.605 2.972 569.996 3.046 299.488 3.119 150.193 3.168 56.829 3.230 0.000 ; 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 0-20 3.766 7.0098 AMW 0.020 972.329 0.049 1612.840 0.101 1601.779 0.243 1701.325 0.482 1878.295 0.571 1889.356 0.802 2088.447 0.997 2254.356 1.073 2254.356 1.227 2486.629 1.426 2574.109 1.616 2651.533 1.681 2751.079 1.782 2839.564 1.831 2817.443 1.961 2916.988 2.070 2979.380 2.155 2939.110 2.196 2961.231 2.256 2872.746 2.321 2839.564 2.374 2684.715 2.422 2331.781 2.483 1568.597 2.524 1215.663 2.584 1093.996 2.674 1060.814 2.747 961.268 2.868 740.358 2.953 464.043 3.046 165.708 3.110 0.000 ; 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 0-20 4.248 7.5515 AW 0.026 1288.791 0.053 2021.398 0.079 2140.011 0.123 2105.125 0.207 2117.086 0.540 2309.458 0.971 2560.637 1.265 2727.094 1.480 2836.736 1.678 2920.462 1.757 2980.267 1.946 2995.51 2.047 2959.335 2.240 2889.563 2.310 2854.677 2.486 2820.788 2.526 2880.593 2.592 2773.941 2.653 2821.785 2.706 2752.012 2.758 2752.012 2.807 2763.973 2.842 2504.82 2.886 2115.092 2.930 1630.674 2.987 1051.565 3.040 437.571 3.057 284.072 3.079 142.434 3.097 83.497 3.110 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 0-20 3.819 7.5515 AMW 0.014 2721.017 0.032 2553.372 0.096 2601.843 0.220 2722.796 0.353 2807.731 0.476 2928.240 0.518 3048.750 0.577 3061.200 0.760 3314.225 0.944 3519.669 1.140 3772.694 1.315 3942.118 1.511 4039.504 1.617 4088.419 1.708 4115.000 1.791 4089.754 1.837 4006.153 1.873 3814.494 1.951 3359.583 2.002 2784.608 2.052 2257.658 2.111 1587.075 2.162 1108.151 2.221 629.227 2.308 318.126 2.395 139.052 2.446 67.503 2.5 0.000 ; ; ;*APOGEE*APOGEE*APOGEE* ; ; 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 10 38 2-4 .0008 .0036 Apogee 0.007 0.162 0.023 0.650 0.041 1.463 0.058 2.519 0.074 3.738 0.079 3.900 0.088 4.915 0.097 5.119 0.106 5.400 0.110 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 0.180 2.397 0.194 1.625 0.207 1.056 0.218 0.406 0.230 0.000 ; ; ; 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 10 38 2-4-6 .0015 .0044 Apogee 0.007 0.190 0.045 1.494 0.078 3.152 0.088 3.805 0.093 3.805 0.100 3.970 0.105 3.696 0.110 3.071 0.117 2.554 0.123 2.582 0.132 2.310 0.163 2.146 0.200 1.984 0.242 1.902 0.253 2.01 0.275 1.929 0.342 1.929 0.403 1.929 0.410 1.848 0.420 1.902 0.467 1.902 0.528 1.929 0.565 1.929 0.580 1.902 0.593 1.848 0.603 1.657 0.610 1.141 0.615 0.597 0.622 0.244 0.630 0.000 ; ; ; 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 10 58 0-3-5-7 .0030 .0067 Apogee 0.014 0.241 0.036 0.895 0.064 2.618 0.100 4.820 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 1.040 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 1.290 1.412 1.293 0.688 1.300 0.275 1.310 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 10 88 0-3-5-7-9 .0060 .0106 Apogee 0.057 1.637 0.093 4.091 0.121 5.480 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 1.710 1.841 1.888 1.882 2.095 1.800 2.230 1.800 2.295 1.677 2.423 1.759 2.444 1.637 2.466 0.982 2.494 0.327 2.530 0.000 ; ; ; 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 .0028 .0091 Apogee 0.007 5.708 0.013 7.211 0.032 6.111 0.045 8.116 0.056 7.717 0.069 9.020 0.078 12.122 0.087 14.760 0.106 13.832 0.117 13.733 0.125 12.636 0.155 12.438 0.168 11.836 0.200 11.243 0.209 11.737 0.219 10.739 0.266 9.846 0.290 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 0.740 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 .0045 .0170 Apogee 0.018 3.230 0.041 6.874 0.147 8.779 0.294 10.683 0.365 11.310 0.388 10.521 0.412 8.779 0.441 7.040 0.465 4.555 0.529 3.479 0.629 2.981 0.653 3.230 0.718 2.816 0.853 2.733 1.065 2.650 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 2.350 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 .0070 .0151 Apogee 0.008 13.958 0.016 21.100 0.022 15.511 0.030 12.831 0.052 14.800 0.081 15.927 0.092 14.658 0.114 16.069 0.125 14.658 0.136 15.369 0.168 14.800 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 11.420 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 1.320 0.000 ; ; ; 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 .0049 .0176 Apogee 0.010 2.712 0.019 5.842 0.029 17.116 0.037 25.720 0.051 22.535 0.070 20.446 0.106 18.983 0.164 17.085 0.188 17.085 0.200 15.824 0.216 16.036 0.255 15.602 0.293 14.350 0.343 13.503 0.394 12.655 0.410 11.605 0.434 11.605 0.521 9.287 0.631 6.340 0.741 4.021 0.851 2.119 0.911 1.480 0.945 1.264 0.960 0.000 ; ; ; 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 .0098 .0249 Apogee 0.050 6.790 0.168 8.788 0.318 10.460 0.385 10.070 0.402 7.909 0.469 5.432 0.486 3.914 0.687 3.115 1.122 2.876 2.060 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 6.390 0.000 ; ; ; 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 .0098 .0259 Apogee 0.011 14.506 0.018 25.130 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 21.760 0.233 20.938 0.255 21.970 0.276 20.938 0.352 20.728 0.402 20.107 0.420 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 0.990 8.083 1.026 8.498 1.123 6.011 1.231 2.487 1.342 0.829 1.400 0.000 ; ; ; Apogee/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 0-2-4-6-8 .0215 .0463 Apogee 0.056 18.590 0.112 20.120 0.168 17.575 0.307 14.380 0.531 10.450 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 6.060 0.000 ; ; ; Apogee/Aerotech F10 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. F10 29 93 2-4-6-8 .0407 .0841 Apogee 0.015 28.220 0.077 26.082 0.201 24.934 0.310 22.806 0.464 20.183 0.573 17.886 0.789 16.075 1.068 13.946 1.393 12.630 1.718 11.155 2.166 9.844 2.677 9.515 3.311 9.187 3.683 8.859 3.791 9.679 4.101 9.679 4.658 9.515 5.168 9.023 5.725 9.023 6.112 8.531 6.329 8.859 6.499 7.546 6.685 5.742 6.778 4.921 6.917 2.625 7.025 1.312 7.130 0.000 ; ; ;*CTI*CTI*CTI* G69 38 127 3-5-7-9-12 0.08400 0.20510 CTI 0.06 80.77 0.20 84.50 0.41 82.74 0.59 80.11 0.81 76.82 1.00 72.87 1.20 68.92 1.40 64.31 1.61 59.48 1.82 50.92 1.90 21.40 1.93 0.00 ; ; H153 38 186 4-6-8-10-13 0.14390 0.30390 CTI 0.13 149.36 0.17 173.70 0.23 171.77 0.39 179.91 0.60 188.30 0.81 180.40 1.01 168.25 1.18 160.91 1.29 149.64 1.41 136.95 1.60 105.37 1.69 23.58 1.75 0.00 ; ; I205 38 245 5-7-9-11-14 0.20610 0.40220 CTI 0.10 181.50 0.13 213.30 0.20 210.10 0.40 226.61 0.60 235.80 0.80 234.00 1.00 232.80 1.20 227.70 1.40 216.80 1.60 197.21 1.74 183.13 1.80 87.30 1.88 0.00 ; ; I285 38 303 6-8-10-12-15 0.27240 0.50590 CTI 0.10 350.60 0.15 318.73 0.20 312.30 0.40 322.37 0.60 330.57 0.80 329.40 1.00 319.64 1.20 294.14 1.40 271.90 1.60 239.90 1.66 178.10 1.80 44.80 1.91 0.00 ; ; J285 38 367 6-8-10-12-15 0.31250 0.59500 CTI 0.06 351.01 0.15 346.01 0.25 357.64 0.50 363.90 0.75 369.26 1.03 343.33 1.27 337.07 1.51 317.40 1.75 282.53 1.93 127.86 2.02 84.94 2.25 11.02 2.26 0.00 ; ; J330 38 421 7-9-11-13-16 0.37500 0.70200 CTI 0.05 459.32 0.16 448.20 0.27 440.41 0.51 437.08 0.75 427.07 1.02 412.61 1.26 387.03 1.50 360.34 1.69 321.41 1.79 300.28 1.91 126.79 1.99 107.88 2.23 22.56 2.26 0.00 ; ; G79SS 38 127 13-10-8-6-4 0.08500 0.22600 CTI 0.00 9.07 0.03 54.45 0.07 76.33 0.09 70.95 0.11 65.92 0.17 68.59 0.20 70.64 0.30 74.89 0.40 80.39 0.50 83.76 0.60 86.45 0.70 88.65 0.81 91.40 0.90 93.06 1.00 93.99 1.10 95.81 1.20 90.70 1.30 86.92 1.40 81.98 1.50 76.54 1.55 58.92 1.60 16.41 1.62 5.16 1.63 0.00 ; ; H143SS 38 186 4-6-8-10-13 0.16540 0.34700 CTI 0.06 114.68 0.19 134.25 0.40 149.61 0.60 158.10 0.80 163.77 1.00 167.00 1.21 160.93 1.40 148.80 1.60 128.59 1.63 117.26 1.65 106.35 1.70 35.63 1.73 0.00 ; ; I212SS 38 245 5-7-9-11-14 0.24810 0.47500 CTI 0.04 189.66 0.20 207.11 0.40 222.41 0.60 236.62 0.80 249.60 0.95 255.15 1.01 250.22 1.21 233.54 1.40 208.99 1.55 183.99 1.60 168.08 1.63 134.62 1.69 25.86 1.71 0.00 ; ; I287SS 38 303 6-8-10-12-15 0.33080 0.60500 CTI 0.05 275.86 0.20 292.53 0.41 309.20 0.61 327.53 0.80 341.70 0.90 344.20 1.01 331.70 1.20 311.70 1.40 280.03 1.53 245.02 1.58 176.62 1.60 141.76 1.64 68.99 1.69 17.48 1.70 0.00 ; ; I350SS 38 367 7-9-11-13-16 0.41350 0.78200 CTI 0.05 399.74 0.13 390.06 0.19 386.19 0.40 388.13 0.60 388.13 0.80 388.13 1.00 389.91 1.20 387.38 1.33 368.77 1.44 350.38 1.52 320.37 1.60 164.79 1.68 36.77 1.71 0.00 ; ; J400SS 38 421 7-9-11-13-16 0.48960 0.70200 CTI 0.05 451.79 0.20 461.14 0.31 465.81 0.44 463.47 0.60 477.48 0.80 482.15 1.00 461.31 1.20 433.12 1.35 402.76 1.40 382.92 1.47 321.04 1.55 258.00 1.60 178.62 1.73 14.58 1.75 0.00 ; ; I540WT 38 367 7-9-11-13-16 0.32880 0.59820 CTI 0.03 597.86 0.04 611.31 0.06 605.64 0.12 612.36 0.24 624.54 0.36 626.00 0.48 623.63 0.60 616.42 0.72 598.14 0.84 583.16 0.95 568.92 0.96 558.53 0.98 533.45 1.02 436.53 1.06 303.15 1.09 184.92 1.13 74.27 1.18 0.00 ; ; J210 54 236 6-16 0.08270 0.84200 CTI 0.04 335.00 0.16 270.92 0.41 269.30 0.80 268.49 1.18 256.32 1.62 236.85 2.03 214.14 2.38 193.86 2.79 174.39 3.20 163.85 3.60 157.36 3.75 135.46 3.86 85.17 3.99 0.00 ; ; J295 54 329 6-16 0.59400 1.11900 CTI 0.04 450.52 0.28 428.70 0.54 423.25 1.00 391.61 1.48 352.34 1.99 304.35 2.51 266.17 3.00 243.26 3.50 216.92 3.67 126.54 3.82 64.36 4.00 0.00 ; ; K445 54 404 7-17 0.79200 1.39800 CTI 0.05 664.83 0.19 640.68 0.48 622.98 1.00 576.29 1.51 515.12 2.00 442.68 2.50 392.26 3.02 350.93 3.13 339.66 3.31 210.88 3.47 78.88 3.67 0.00 ; ; K570 54 488 7-17 0.99000 1.68500 CTI 0.04 892.67 0.50 797.99 1.00 738.68 1.50 659.37 2.00 585.96 2.50 512.88 2.97 417.16 3.20 224.79 3.47 67.00 3.59 0.00 ; ; K660 54 572 7-17 1.17700 1.94900 CTI 0.07 1078.90 0.23 1006.47 0.40 966.76 0.80 897.52 1.20 842.72 1.60 794.15 2.01 744.52 2.40 692.27 2.54 671.37 2.68 439.08 2.80 400.68 3.01 386.90 3.20 234.31 3.45 106.65 3.60 44.03 3.69 0.00 ; ; L730 54 6490 0 1.35100 2.24700 CTI 0.00 81.36 0.01 1079.71 0.02 1216.59 0.04 1154.68 0.20 1127.51 0.45 1055.11 0.60 1028.17 0.75 995.24 1.00 959.33 1.50 898.71 2.00 830.70 2.50 730.76 2.60 592.55 2.70 510.96 2.90 487.88 3.00 405.72 3.10 299.80 3.20 296.09 3.30 251.85 3.40 171.70 3.50 165.26 3.60 139.38 3.65 117.77 3.76 45.38 3.77 0.00 ; ; J280SS 54 236 6-16 0.51200 0.95400 CTI 0.10 259.43 0.30 278.91 0.60 293.07 0.90 306.85 1.20 319.19 1.50 321.10 1.80 310.85 2.11 279.89 2.35 286.70 2.40 269.17 2.44 178.24 2.49 42.80 2.54 0.00 ; ; J380SS 54 320 6-16 0.76900 1.29330 CTI 0.05 368.48 0.30 348.31 0.60 378.83 0.90 400.93 1.20 419.52 1.50 433.09 1.80 434.60 2.10 408.81 2.40 369.92 2.56 410.58 2.59 297.80 2.71 45.25 2.73 0.00 ; ; K530SS 54 404 6-16 1.02500 1.63980 CTI 0.05 533.59 0.09 503.98 0.29 514.09 0.60 534.31 0.90 557.41 1.20 577.63 1.50 587.74 1.80 596.40 2.10 535.44 2.31 502.54 2.47 551.63 2.56 393.94 2.60 274.37 2.64 137.19 2.67 0.00 ; ; K650SS 54 488 6-16 1.28100 1.98990 CTI 0.04 664.52 0.12 645.90 0.31 642.24 0.60 664.78 0.91 684.59 1.22 712.82 1.50 723.41 1.80 728.70 2.10 664.52 2.40 614.68 2.51 680.53 2.55 534.62 2.61 268.19 2.66 0.00 ; ; K510 75 350 0 1.19700 2.59000 CTI 0.04 394.38 0.07 617.68 0.10 645.17 0.21 658.16 0.35 669.23 0.53 667.72 0.82 661.58 1.18 626.92 1.72 588.46 2.15 557.69 2.39 542.31 2.90 492.86 3.07 470.31 3.56 426.81 3.98 398.96 4.32 393.98 4.48 380.63 4.60 364.22 4.65 290.91 4.80 91.23 4.83 45.82 4.84 0.00 ; ; L800 75 486 0 1.79500 3.51100 CTI 0.00 27.28 0.01 402.41 0.10 1285.54 0.12 1056.51 0.26 1041.73 0.71 1026.95 1.28 998.38 2.05 901.36 2.41 849.64 2.83 763.51 3.25 707.06 3.65 655.14 3.80 651.74 4.00 624.07 4.10 601.34 4.19 536.17 4.31 415.67 4.41 270.17 4.52 140.20 4.60 76.92 4.65 54.94 4.67 40.16 4.68 0.00 ; ; L1115 75 621 0 2.39400 4.40400 CTI 0.01 45.46 0.05 522.52 0.08 984.04 0.10 1256.10 0.15 1389.85 0.18 1713.25 0.24 1515.65 0.30 1474.74 0.40 1443.28 0.42 1446.25 0.50 1430.02 0.76 1392.85 1.00 1361.70 1.28 1339.45 1.84 1259.35 2.25 1201.50 3.00 1076.11 3.50 990.86 3.92 832.85 4.00 607.78 4.10 434.99 4.22 288.73 4.38 156.49 4.48 86.39 4.49 0.00 ; ; M1400 75 757 0 2.99200 5.30200 CTI 0.02 991.61 0.07 1939.66 0.11 2291.75 0.14 1976.39 0.19 1962.48 0.29 1936.13 0.52 1881.02 0.75 1833.40 1.00 1778.08 1.25 1738.57 1.70 1654.82 2.40 1502.39 2.85 1389.48 3.25 1283.00 3.40 1232.23 3.53 1199.64 3.65 1083.69 3.70 909.39 3.90 641.50 4.00 502.82 4.03 463.03 4.22 336.09 4.43 138.68 4.47 93.21 4.48 0.00 ; ; M520 98 548 0 3.71300 6.69300 CTI 0.01 1077.00 0.25 1062.83 0.38 1065.66 0.50 971.00 0.71 938.12 0.93 915.45 1.23 878.61 2.07 906.95 2.61 901.28 3.03 892.78 3.50 872.94 3.93 836.09 4.96 756.73 6.08 657.54 7.05 549.84 7.79 461.98 8.39 391.12 9.06 323.10 10.01 243.74 11.01 172.89 12.00 116.20 13.95 0.00 ; ; M2505 98 548 0 3.42300 6.25800 CTI 0.12 2600.00 0.21 2482.00 0.60 2715.00 0.90 2876.00 1.20 2938.00 1.50 2889.00 1.80 2785.00 2.10 2573.00 2.40 2349.00 2.70 2182.00 2.99 85.00 3.00 0.00 ; ; N1100 98 1010 0 4.51700 11.64400 CTI 0.16 2624.00 0.33 2708.00 0.91 2055.00 1.22 1886.00 2.44 1713.00 3.66 1535.00 4.88 1332.00 6.12 1088.00 7.41 824.85 9.77 464.00 12.18 111.20 12.19 0.00 ; ; N2500 98 1010 0 6.77800 11.66800 CTI 0.02 773.70 0.05 3356.60 0.06 3657.80 0.10 3546.80 0.25 3403.80 0.40 3309.20 0.80 3262.50 1.00 3206.10 1.50 3088.50 2.00 2940.40 2.50 2792.60 3.00 2598.40 3.50 2402.50 4.00 2227.00 4.25 2152.50 4.40 2102.50 4.50 2007.00 4.60 1683.80 4.75 1269.50 5.00 767.30 5.41 341.30 5.42 0.00 ; ; ;*ELLIS*ELLIS*ELLIS* I150EM 38 229 0-20 0.17180 0.39830 EM 0.00 101.15 0.10 155.94 0.15 155.94 0.30 177.01 0.40 181.23 0.70 198.09 0.90 198.09 1.10 181.23 1.90 160.15 2.00 147.51 2.10 126.44 2.30 21.07 2.40 8.43 2.67 0.00 ; ; I160EM 38 280 0-20 0.23190 0.48670 EM 0.01 205.72 0.01 192.73 0.20 192.73 0.40 201.39 0.50 199.22 0.75 199.22 0.76 197.06 0.95 194.89 1.50 203.55 2.20 199.22 2.35 155.91 2.40 41.14 2.70 42.88 3.25 0.00 ; ; I230EM 38 331 0-20 0.29200 0.57510 EM 0.00 309.64 0.00 305.28 0.10 346.71 0.15 322.72 0.50 290.01 1.00 283.47 1.50 270.39 1.70 252.94 2.00 218.05 2.25 82.86 2.40 78.50 2.45 47.97 2.60 43.61 2.80 4.36 2.83 0.00 ; ; J270EM 38 384 0-20 0.34710 0.68680 EM 0.00 308.91 0.10 419.24 0.15 441.30 0.20 397.17 0.30 375.11 0.33 353.04 1.50 330.98 1.90 286.85 2.00 165.49 2.10 110.33 2.50 66.19 2.65 22.07 2.90 0.00 ; ; J330EM 38 433 0-20 0.41190 0.78000 EM 0.05 541.77 0.07 520.10 0.20 485.43 0.50 507.10 1.00 455.09 1.25 433.42 1.50 379.24 1.77 216.71 2.00 104.02 2.10 99.69 2.20 86.68 2.50 73.68 2.75 0.00 ; ; J148EM 54 356 0-20 0.50900 1.17900 EM 0.03 182.30 0.11 157.66 0.48 151.26 1.50 160.62 3.02 161.11 5.47 146.33 6.07 19.22 6.10 0.00 ; ; K475EM 54 664 0-20 1.13300 2.16800 EM 0.01 885.90 0.12 713.51 0.21 629.71 0.31 591.40 3.01 591.40 3.17 584.22 3.57 426.19 3.96 306.47 4.46 193.94 4.80 86.20 5.10 0.00 ; ; L330EM 75 381 0-20 1.48990 2.39590 EM 0.05 343.00 0.25 381.58 0.50 362.29 1.00 360.15 2.50 390.16 3.50 392.30 6.50 325.85 7.50 321.56 7.60 317.27 8.00 150.06 8.50 64.31 8.90 21.44 9.35 0.00 ; ; L600EM 75 584 0-20 2.47280 3.80460 EM 0.05 886.09 0.10 1113.94 0.20 1149.38 0.40 962.04 0.50 865.83 1.00 860.77 7.00 384.82 7.10 379.75 7.20 313.93 7.50 278.48 8.50 50.63 8.90 10.13 9.03 0.00 ; ; M1000EM 75 787 0-20 3.47514 5.57760 EM 0.16 1897.85 0.48 1606.84 0.80 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 3.70 1075.88 4.02 1045.73 4.34 1010.71 4.67 951.57 4.99 860.89 5.31 727.66 5.63 595.90 5.96 519.12 6.28 440.08 6.60 347.88 6.92 239.48 7.24 144.67 7.57 75.14 7.89 33.55 8.21 0.00 ; ; E12EM 24 101 0-6-10 0.02800 0.05320 EM 0.01 31.17 0.13 24.43 0.17 23.34 1.50 14.83 2.00 10.28 2.50 4.80 2.91 2.30 2.92 0.00 ; ; F20EM 24 139 0-6-10 0.04760 0.07560 EM 0.01 24.19 0.05 39.00 0.07 39.14 0.13 34.58 1.00 26.94 2.00 19.52 2.40 14.00 2.70 7.96 3.00 4.46 3.55 1.27 3.58 0.00 ; ; G37EM 24 181 0-6-10 0.06800 0.11330 EM 0.01 68.00 0.14 61.75 0.23 51.46 0.32 48.34 0.51 45.21 1.00 41.17 1.50 37.86 2.00 33.82 2.28 30.88 2.50 26.83 2.73 19.30 2.89 11.58 3.02 2.57 3.10 0.00 ; ; G20EM 29 149 0-3-7 0.07290 0.11790 EM 0.02 46.00 0.22 32.45 0.50 26.98 1.01 26.23 2.03 24.74 3.05 22.75 3.60 20.64 4.07 17.90 4.48 12.93 4.82 7.83 5.07 4.10 5.47 0.00 ; ; G35EM 29 165 0-6-10 0.08200 0.13000 EM 0.01 51.12 0.04 56.20 0.11 44.35 2.00 32.96 2.73 27.49 3.31 27.49 3.72 6.84 3.80 5.32 3.90 0.00 ; ; H50EM 29 279 0-6-10 0.16300 0.29000 EM 0.01 63.67 0.17 108.90 0.27 94.90 0.47 81.43 0.79 71.02 1.27 64.90 1.97 60.61 2.56 56.94 3.01 52.04 3.52 45.31 3.97 34.90 4.50 17.37 4.97 4.90 5.28 0.00 ; ; H275EM 29 275 0-6-10 0.14200 0.25500 EM 0.00 641.00 0.02 376.29 0.03 374.56 0.03 341.61 0.08 322.53 0.47 319.07 0.80 270.51 0.89 249.70 0.92 163.00 0.97 93.64 1.03 41.62 1.09 19.07 1.10 0.00 ; ; I69EM 29 406 0-10 0.23600 0.41000 EM 0.05 78.67 0.10 149.70 0.25 133.50 0.49 111.51 0.75 100.00 1.07 93.18 1.48 87.83 2.00 82.49 2.50 78.00 2.99 73.32 3.50 64.50 3.99 48.88 4.50 29.79 4.99 9.17 5.30 0.00 ; ; H48EM 38 200 0-8-20 0.15400 0.29200 EM 0.05 101.50 0.10 101.50 0.21 92.18 0.46 86.48 0.74 83.38 1.00 80.00 1.49 74.57 1.99 68.36 2.48 63.18 2.99 56.45 3.20 34.18 3.50 18.00 3.69 13.46 4.00 11.00 4.36 7.77 4.40 0.00 ; ; I134EM 38 355 0-15-20 0.30050 0.58120 EM 0.10 268.80 0.20 138.00 1.00 116.00 2.00 102.00 3.00 85.00 4.00 67.00 4.65 16.46 4.82 6.86 5.07 6.86 5.15 0.00 ; ; J228EM 38 562 0-6-20 0.56910 0.83910 EM 0.01 616.00 0.02 426.21 0.06 424.54 0.23 354.62 0.60 354.62 1.33 291.35 2.15 248.06 3.00 221.43 3.48 189.79 3.79 153.17 4.13 98.23 4.55 43.29 5.00 0.00 ; ; J110EM 54 276 0-20 0.45359 0.87540 EM 0.02 154.80 0.10 222.00 0.33 180.00 0.43 178.80 0.57 147.60 1.20 145.20 2.09 136.80 3.04 126.60 4.11 109.80 5.04 82.80 5.64 58.20 6.24 38.40 6.78 24.00 6.80 0.00 ; ; ;*ESTES*ESTES*ESTES* ; ; 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 .00083 .0061 Estes 0.016 0.243 0.044 1.164 0.080 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 4.950 0.139 4.815 0.143 4.814 0.149 4.660 0.157 4.289 0.173 3.548 0.187 2.808 0.194 2.592 0.197 2.130 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 0.250 0.000 ; ; ; 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 .002 .0066 Estes 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 6.870 0.117 7.021 0.126 7.620 0.137 7.472 0.146 6.870 0.153 6.118 0.159 5.065 0.166 4.363 0.179 3.660 0.197 2.908 0.222 2.256 0.250 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 0.350 0.651 0.360 0.000 ; ; ; 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 .0033 .0085 Estes 0.024 0.195 0.048 0.899 0.086 2.658 0.110 4.183 0.140 5.830 0.159 5.395 0.180 4.301 0.199 3.635 0.215 2.736 0.234 2.267 0.258 2.150 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 2.150 0.953 2.072 0.966 1.719 0.977 1.173 0.993 0.547 1.010 0.000 ; ; ; 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 0-3 .0038 .00525 Estes 0.026 0.478 0.055 1.919 0.093 4.513 0.124 8.165 0.146 10.956 0.166 12.640 0.179 11.046 0.194 7.966 0.203 6.042 0.209 3.154 0.225 1.421 0.260 1.225 0.333 1.410 0.456 1.206 0.575 1.195 0.663 1.282 0.760 1.273 0.811 1.268 0.828 0.689 0.850 0.000 ; ; ; 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 .0026 .0138 Estes 0.031 0.404 0.064 1.258 0.096 2.263 0.124 3.467 0.149 4.720 0.172 6.023 0.196 7.027 0.210 7.528 0.225 7.860 0.235 7.482 0.244 6.683 0.254 5.685 0.263 4.487 0.269 4.087 0.279 3.039 0.290 1.790 0.297 1.042 0.306 0.593 0.314 0.344 0.330 0.000 ; ; ; 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 .0033 .01635 Estes 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 9.730 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 0.730 0.000 ; ; ; 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 2-4-6 .0060 .0189 Estes 0.020 0.418 0.040 1.673 0.065 4.076 0.085 6.690 0.105 9.304 0.119 11.496 0.136 12.750 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 0.940 3.449 0.991 3.449 1.002 2.404 1.010 1.254 1.030 0.000 ; ; ; Estes B6 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. B6 18 70 0-2-4-6 .0056 .01822 Estes 0.023 0.688 0.057 2.457 0.089 4.816 0.116 7.274 0.148 9.929 0.171 12.140 0.191 11.695 0.200 10.719 0.209 9.240 0.230 7.667 0.255 6.488 0.305 5.505 0.375 4.816 0.477 4.620 0.580 4.620 0.671 4.521 0.746 4.226 0.786 4.325 0.802 3.145 0.825 1.572 0.860 0.000 ; ; ; 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 .0113 .0248 Estes 0.042 2.195 0.107 9.118 0.159 16.213 0.210 21.850 0.233 18.407 0.270 13.677 0.289 9.793 0.303 7.092 0.326 5.065 0.401 4.390 0.550 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 1.730 0.000 ; ; ; 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 .0108 .0231 Estes 0.031 0.946 0.092 4.826 0.139 9.936 0.192 14.090 0.209 11.446 0.231 7.381 0.248 6.151 0.292 5.489 0.370 4.921 0.475 4.448 0.671 4.258 0.702 4.542 0.723 4.164 0.850 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 1.860 0.000 ; ; ; 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 .012 .0353 Estes 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 21.730 0.306 20.206 0.323 17.321 0.337 14.931 0.358 13.236 0.385 11.947 0.413 11.650 0.468 10.946 0.539 10.450 0.619 10.648 0.683 10.648 0.715 10.648 0.726 10.053 0.740 8.163 0.758 5.773 0.778 3.185 0.795 1.394 0.810 0.000 ; ; ; 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 0 .0245 .0448 Estes 0.033 2.393 0.084 5.783 0.144 12.170 0.214 20.757 0.261 24.350 0.289 26.010 0.311 23.334 0.325 18.532 0.338 14.536 0.356 12.331 0.398 10.720 0.480 9.303 0.618 8.676 0.761 8.247 0.955 8.209 1.222 7.955 1.402 8.319 1.540 8.291 1.701 8.459 1.784 8.442 1.803 6.239 1.834 3.033 1.860 0.000 ; ; ; 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 .0211 .0426 Estes 0.049 2.569 0.116 9.369 0.184 17.275 0.237 24.258 0.282 29.730 0.297 27.010 0.311 22.589 0.322 17.990 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 8.310 1.590 8.294 1.612 4.613 1.650 0.000 ; ; ; ESTES E9 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. E9 24 95 0-4-6-8 .0358 .0646 Estes 0.039 1.623 0.087 5.360 0.135 9.746 0.178 13.971 0.216 16.810 0.269 19.470 0.299 17.141 0.329 14.292 0.364 12.427 0.413 10.802 0.507 9.989 0.649 9.421 0.810 8.852 1.138 8.771 1.178 8.527 1.457 8.527 1.579 8.608 1.809 8.608 2.044 8.527 2.284 8.608 2.499 8.689 2.597 8.608 2.710 9.014 2.803 8.689 2.891 9.096 2.959 9.258 3.008 9.339 3.023 7.227 3.034 4.466 3.049 1.623 3.090 0.000 ; ; ;*LOKI*LOKI*LOKI* ; ; PRELIMINARY THRUST DATA ; LIKELY TO BE UPDATED IN THE NEAR FUTURE ; please check www.lokiresearch.com for up to date files. ; ; 9/16/2004 ; J528 38 406 5-8-10-13-17 0.37200 0.75200 Loki 0.03 272.83 0.06 758.38 0.10 763.01 0.14 742.20 0.17 739.88 0.21 732.95 0.50 735.26 0.60 732.95 0.70 730.64 0.80 698.27 0.90 670.52 1.00 460.12 1.10 245.09 1.20 53.18 1.25 0.00 ; ; I305 38 406 5-8-10-13-17 0.37200 0.75200 Loki 0.03 163.19 0.06 498.38 0.08 505.00 0.08 469.77 0.11 466.17 0.15 461.80 0.26 453.33 0.35 453.33 0.47 426.56 0.57 395.55 0.67 360.45 0.77 341.53 0.87 297.74 0.97 271.47 1.07 208.71 1.17 154.71 1.27 121.14 1.37 96.33 1.47 56.92 1.57 27.73 1.70 0.00 ; ; H144 38 178 5-8-10-13-17 0.12000 0.33500 Loki 0.02 245.66 0.07 242.05 0.15 234.10 0.25 222.54 0.31 219.65 0.40 215.32 0.45 212.43 0.50 204.48 0.61 194.36 0.70 180.64 0.81 164.74 0.90 148.79 1.01 127.83 1.10 103.21 1.21 72.14 1.31 66.36 1.41 51.91 1.49 34.57 1.60 19.39 1.70 0.00 ; ; ;*NORTH_COAST*NORTH_COAST*NORTH_COAST* ; ; NCR F62 RASP.ENG file made from NAR published data ; File produced December 7, 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. F62 29 103 4-6 .0515 .1113 NCR 0.006 27.705 0.018 23.181 0.028 36.176 0.040 51.435 0.064 57.085 0.127 64.969 0.179 70.041 0.206 71.716 0.221 73.978 0.227 72.842 0.269 75.652 0.323 78.453 0.353 79.001 0.387 78.991 0.429 78.971 0.498 80.410 0.546 78.353 0.591 77.765 0.606 78.323 0.618 74.357 0.667 73.779 0.757 68.078 0.868 59.547 0.998 48.744 1.100 37.950 1.130 33.416 1.142 27.755 1.154 19.832 1.169 11.351 1.187 6.249 1.211 2.846 1.240 0.000 ; ; ;*QUEST*QUEST*QUEST* ; MAXXI 6 16 1 0.00040 0.00107 Quest 0.01 0.24 0.06 1.24 0.11 0.27 0.12 0.22 0.81 0.14 0.82 0.00 ; ; ; QUEST MICROMAXX II RASP.ENG file made from NAR published data ; File produced Dec 29, 2001 ; 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. MAXXII 6 16 1 .0005 .0012 Quest 0.008 0.160 0.018 0.482 0.024 0.993 0.030 1.534 0.034 2.032 0.036 2.397 0.040 2.543 0.046 3.025 0.052 3.210 0.059 2.864 0.069 2.191 0.080 1.094 0.087 0.539 0.092 0.378 0.106 0.304 0.139 0.260 0.177 0.303 0.223 0.287 0.258 0.243 0.288 0.198 0.346 0.270 0.402 0.298 0.411 0.254 0.430 0.312 0.465 0.282 0.503 0.238 0.516 0.281 0.562 0.280 0.621 0.294 0.641 0.279 0.647 0.176 0.660 0.000 ; ; A6Q 18 70 4 0.00350 0.01530 Quest 0.10 4.80 0.20 11.82 0.23 7.90 0.30 4.80 0.41 0.00 ; ; B6Q 18 70 0-4 0.00650 0.01620 Quest 0.10 7.00 0.18 14.38 0.20 10.20 0.24 6.60 0.30 6.00 0.40 6.10 0.50 6.20 0.60 6.30 0.65 6.60 0.70 3.00 0.75 0.00 ; ; C6Q 18 70 0-3-5 0.01100 0.02040 Quest 0.05 3.80 0.10 6.50 0.15 11.75 0.20 13.40 0.25 9.25 0.30 7.00 0.40 5.60 0.50 5.20 0.60 5.05 0.70 4.80 0.80 4.50 0.90 4.60 1.00 4.45 1.20 4.20 1.35 4.00 1.62 4.00 1.63 0.00 ;