Motor Manufacturer |
AEROTECH |
Nozzle Throat dia(in) |
0.292 |
Manuf Metric Designation |
I200W-S/M/L |
Exit Cone diameter(in) |
0.685 |
TMT Metric Designation |
I199W-6/10/14 (1% I) |
Samples per sec |
480 |
Testing Date |
9/11/99 |
Burntime eval (%) |
5 |
Certified Until |
12/31/02 |
Calculated burntime(s) |
1.65 |
Motor dimen(in) |
1.125 X 13.1 |
Total Impul lbs-s (N-s) |
72.9 (324.5Ns) |
Motor dimen(mm) |
29 X 333 |
Max Thrust lbs (N) |
104.1 (463.3N) |
Propellant Wt. lbs (g) |
.412 (186.5g) |
Ave Thrust lbs (N) |
44.6 (198.6N) |
Isp lbs-s/lbs |
177.2 |
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
I200w long delay
Short version
WRASP ".eng" file
WRASP comparative graph
