; AMW L1060 RASP.ENG file made from NAR published 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.
L1060 75 497 0-10-15 1.9188 3.9388 AMW
0.020 258.773
0.024 368.235
0.032 328.386
0.076 427.96
0.100 567.284
0.116 751.352
0.128 791.202
0.169 816.071
0.225 816.071
0.309 875.795
0.518 985.257
0.763 1079.639
1.024 1174.519
1.308 1229.45
1.606 1288.375
1.782 1298.25
1.983 1293.369
2.256 1239.437
2.525 1184.506
2.822 1129.576
3.038 1069.651
3.111 1044.683
3.135 995.145
3.183 835.946
3.239 552.303
3.299 268.661
3.327 164.193
3.339 84.593
3.360 44.783
3.400 0

; AeroTech M1315W
; Copyright Tripoli Motor Testing 1999 (www.tripoli.org)
; provided by ThrustCurve.org (www.thrustcurve.org)
M1315W 75 801 0 3.4496 5.6448 AT
0.116 1728.683
0.349 1673.336
0.582 1686.810
0.816 1696.068
1.049 1663.167
1.282 1631.243
1.516 1620.471
1.749 1619.702
1.982 1621.042
2.216 1615.320
2.449 1567.089
2.682 1493.722
2.916 1420.079
3.149 1358.660
3.382 1292.507
3.616 1224.806
3.849 1171.995
4.082 928.809
4.316 577.949
4.549 395.445
4.782 314.006
5.016 228.273
5.249 159.803
5.482 118.348
5.716 109.782
5.949 0.000
; AMW L1060 RASP.ENG file made from NAR published 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.
L1060 75 497 0 1.9188 3.9388 AMW
0.020 258.773
0.024 368.235
0.032 328.386
0.076 427.96
0.100 567.284
0.116 751.352
0.128 791.202
0.169 816.071
0.225 816.071
0.309 875.795
0.518 985.257
0.763 1079.639
1.024 1174.519
1.308 1229.45
1.606 1288.375
1.782 1298.25
1.983 1293.369
2.256 1239.437
2.525 1184.506
2.822 1129.576
3.038 1069.651
3.111 1044.683
3.135 995.145
3.183 835.946
3.239 552.303
3.299 268.661
3.327 164.193
3.339 84.593
3.360 44.783
3.400 0

; AMW L777 RASP.ENG file
; File produced SEPT 4, 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.

L777 75 497 0 1.7623 3.6987 AMW
0.025 140.882
0.064 209.474
0.108 360.055
0.204 652.185
0.360 641.518
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

; AMW K950 RASP.ENG file made from NAR published data
; File produced SEPT 4, 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.
K950 54 492 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 0.0000

; AMW K670 RASP.ENG file made from NAR published data
; File produced SEPT 4, 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.
K670 54 492 0 1.0140 1.9145 AMW
0.016 294.05
0.035 398.577
0.086 506.292
0.153 496.428
0.264 506.093
0.461 558.108
0.722 629.553
0.983 688.044
1.116 714.051
1.193 785.795
1.409 788.784
1.737 804.56
2.074 781.41
2.195 764.87
2.226 781.211
2.277 764.77
2.398 751.517
2.440 744.941
2.468 718.834
2.484 666.521
2.525 418.107
2.551 218.818
2.573 120.768
2.595 52.143
2.620 0
;