Motor Manufacturer |
AEROTECH |
Nozzle Throat dia(in) |
0.219 |
Manuf Metric Designation |
H238T-S/M/L |
Exit Cone diameter(in) |
0.44 |
TMT Metric Designation |
H194T-6/10/14 (11% H) |
Samples per sec |
480 |
Testing Date |
6/28/97 |
Burntime eval (%) |
5 |
Certified Until |
12/31/01* |
Calculated burntime(s) |
0.92 |
Motor dimen(in) |
1.125X7.625 |
Total Impul lbs-s (N-s) |
40.1 (178.4) |
Motor dimen(mm) |
29X194 |
Max Thrust lbs (N) |
55.4 (246.6) |
Propellant Wt. lbs (g) |
0.185 (83.8) |
Ave Thrust lbs (N) |
43.6 (194.1) |
Isp lbs-s/lbs |
216.9 |
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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