h220.eng

Spacecraft Engineering Toolbox

; 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.
H220 29 238 6-10-14 .1064 .2460 A
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 0.000