Motor Manufacturer |
AEROTECH |
Nozzle Throat dia(in) |
0.267 |
Manuf Metric Designation |
I211W-S/M/L |
Exit Cone diameter(in) |
0.435 |
TMT Metric Designation |
I210W-6/10/14 (36% I) |
Samples per sec |
480 |
Testing Date |
9/11/99 |
Burntime eval (%) |
5 |
Certified Until |
12/31/02 |
Calculated burntime(s) |
2.10 |
Motor dimen(in) |
1.5 X 9.438 |
Total Impul lbs-s (N-s) |
97.7 (434.5Ns) |
Motor dimen(mm) |
38 X 240 |
Max Thrust lbs (N) |
81.5 (362.7N) |
Propellant Wt. lbs (g) |
.555 (251.3g) |
Ave Thrust lbs (N) |
47.1 (209.6N) |
Isp lbs-s/lbs |
176.1 |
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