Motor Manufacturer |
AEROTECH |
Nozzle Throat dia(in) |
0.125 |
Manuf Metric Designation |
H73J-S/M |
Exit Cone diameter(in) |
0.32 |
TMT Metric Designation |
H72J-6/10 (18% H) |
Samples per sec |
480 |
Testing Date |
6/29/97 |
Burntime eval (%) |
5 |
Certified Until |
12/31/01* |
Calculated burntime(s) |
2.6 |
Motor dimen(in) |
1.5X6 |
Total Impul lbs-s (N-s) |
42.4 (188.6) |
Motor dimen(mm) |
38X152 |
Max Thrust lbs (N) |
21.8 (97.1) |
Propellant Wt. lbs (g) |
0.32 (142.7) |
Ave Thrust lbs (N) |
16.3 (72.4) |
Isp lbs-s/lbs |
132.5 |
Representative TMT Thrust Curve
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"Representative" Actual TMT test data
Full size data file - (zipped file)
Short version
WRASP ".eng" file
WRASP comparative graph
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