Motor Manufacturer |
AEROTECH |
Nozzle Throat dia(in) |
0.158 |
Manuf Metric Designation |
H112J-6/10/14 |
Exit Cone diameter(in) |
0.31 |
TMT Metric Designation |
H89J-6/10/14 (63% H) |
Samples per sec |
480 |
Testing Date |
9/13/99 |
Burntime eval (%) |
5 |
Certified Until |
12/31/02 |
Calculated burntime(s) |
2.92 |
Motor dimen(in) |
1.5 X 7.948 |
Total Impul lbs-s (N-s) |
58.7 (261.1Ns) |
Motor dimen(mm) |
38 X 202 |
Max Thrust lbs (N) |
27.4 (121.7N) |
Propellant Wt. lbs (g) |
.422 (191.2g) |
Ave Thrust lbs (N) |
20.1 (89.4N) |
Isp lbs-s/lbs |
139.0 |
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