Motor Manufacturer |
AEROTECH |
Nozzle Throat dia(in) |
0.265 |
Manuf Metric Designation |
H125W-6/10/14 |
Exit Cone diameter(in) |
0.45 |
TMT Metric Designation |
I124W-6/10/14 (1% I) |
Samples per sec |
480 |
Testing Date |
10/11/97 |
Burntime eval (%) |
5 |
Certified Until |
12/31/01* |
Calculated burntime(s) |
2.6 |
Motor dimen(in) |
1.125X13 |
Total Impul lbs-s (N-s) |
72.3 (321.8) |
Motor dimen(mm) |
29X330 |
Max Thrust lbs (N) |
69.0 (307.1) |
Propellant Wt. lbs (g) |
0.41 (185.7) |
Ave Thrust lbs (N) |
27.8 (123.8) |
Isp lbs-s/lbs |
176.4 |
Representative TMT Thrust Curve
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Representative Actual TMT test data (zipped file)
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