Motor Manufacturer |
AEROTECH |
Nozzle Throat dia(in) |
0.180 |
Manuf Metric Designation |
H123W-6/10/14 |
Exit Cone diameter(in) |
0.435 |
TMT Metric Designation |
H107W-6/10/14 (47% H) |
Samples per sec |
480 |
Testing Date |
10/24/99 |
Burntime eval (%) |
5 |
Certified Until |
12/31/02 |
Calculated burntime(s) |
2.18 |
Motor dimen(in) |
1.5 X 6.073 |
Total Impul lbs-s (N-s) |
52.9 (235.6Ns) |
Motor dimen(mm) |
38 X 154 |
Max Thrust lbs (N) |
35.5 (158.1N) |
Propellant Wt. lbs (g) |
.284 (128.7g) |
Ave Thrust lbs (N) |
24.1 (107.3N) |
Isp lbs-s/lbs |
186.4 |
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