Motor Manufacturer |
AEROTECH |
Nozzle Throat dia(in) |
0.203 |
Manuf Metric Designation |
H180W-S/M/L |
Exit Cone diameter(in) |
0.43 |
TMT Metric Designation |
H205W-6/10/14 (48% H) |
Samples per sec |
480 |
Testing Date |
6/29/97 |
Burntime eval (%) |
5 |
Certified Until |
12/31/01* |
Calculated burntime(s) |
1.17 |
Motor dimen(in) |
1.125X9.375 |
Total Impul lbs-s (N-s) |
53.2 (236.8) |
Motor dimen(mm) |
29X238 |
Max Thrust lbs (N) |
59.8 (266.3) |
Propellant Wt. lbs (g) |
0.28 (126.8) |
Ave Thrust lbs (N) |
46.0 (204.6) |
Isp lbs-s/lbs |
192.2 |
Representative TMT Thrust Curve
Back to Motor Testing Page
Back
to Certified Motors Page

"Representative" Actual TMT test data
Full size data file - (zipped file)
Short version
WRASP ".eng" file
WRASP comparative graph
Back to Motor Testing Page Back to Certified Motors Page