Motor Manufacturer |
AEROTECH |
Nozzle Throat dia(in) |
0.227 |
Manuf Metric Designation |
H242T-S/M/L |
Exit Cone diameter(in) |
0.422 |
TMT Metric Designation |
H210T-6/10/14 (58% H) |
Samples per sec |
480 |
Testing Date |
10/17/99 |
Burntime eval (%) |
5 |
Certified Until |
12/31/02 |
Calculated burntime(s) |
1.20 |
Motor dimen(in) |
1.5 X 6.073 |
Total Impul lbs-s (N-s) |
56.9 (253.3Ns) |
Motor dimen(mm) |
38 X 154 |
Max Thrust lbs (N) |
64.6 (287.5N) |
Propellant Wt. lbs (g) |
.253 (114.7g) |
Ave Thrust lbs (N) |
47.3 (210.4N) |
Isp lbs-s/lbs |
224.9 |
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