Motor Manufacturer |
AEROTECH |
Nozzle Throat dia(in) |
0.18 |
Manuf Metric Designation |
I154J-S/M |
Exit Cone diameter(in) |
0.43 |
TMT Metric Designation |
I127J-6/10 (18% I) |
Samples per sec |
480 |
Testing Date |
10/24/99 |
Burntime eval (%) |
5 |
Certified Until |
12/31/02 |
Calculated burntime(s) |
2.99 |
Motor dimen(in) |
1.5 X 9.823 |
Total Impul lbs-s (N-s) |
84.9 (378.0Ns) |
Motor dimen(mm) |
38 X 250 |
Max Thrust lbs (N) |
38.3 (170.5N) |
Propellant Wt. lbs (g) |
.558 (252.8g) |
Ave Thrust lbs (N) |
28.4 (126.5N) |
Isp lbs-s/lbs |
152.2 |
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