Motor Manufacturer |
AEROTECH |
Nozzle Throat dia(in) |
0.156 |
Manuf Metric Designation |
G75J-S/M |
Exit Cone diameter(in) |
0.32 |
TMT Metric Designation |
G66J-6/10 (82% G) |
Samples per sec |
480 |
Testing Date |
6/28/97 |
Burntime eval (%) |
5 |
Certified Until |
12/31/01* |
Calculated burntime(s) |
2.2 |
Motor dimen(in) |
1.125X7.625 |
Total Impul lbs-s (N-s) |
32.7 (145.6) |
Motor dimen(mm) |
29X194 |
Max Thrust lbs (N) |
18.7 (83.3) |
Propellant Wt. lbs (g) |
0.24 (108.72) |
Ave Thrust lbs (N) |
14.9 (66.1) |
Isp lbs-s/lbs |
136.3 |
Representative TMT Thrust Curve

Representative Actual TMT test data (zipped file)
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