Motor Manufacturer

AEROTECH

Nozzle Throat dia(in)

0.156

Manuf Metric Designation

G75J-S/M

Exit Cone diameter(in)

0.32

TMT Metric Designation

G66J-6/10 (82% G)

Samples per sec

480

Testing Date

6/28/97

Burntime eval (%)

5

Certified Until

12/31/01*

Calculated burntime(s)

2.2

Motor dimen(in)

1.125X7.625

Total Impul lbs-s (N-s)

32.7 (145.6)

Motor dimen(mm)

29X194

Max Thrust lbs (N)

18.7 (83.3)

Propellant Wt. lbs (g)

0.24 (108.72)

Ave Thrust lbs (N)

14.9 (66.1)

Isp lbs-s/lbs

136.3

Representative TMT Thrust Curve  

wpe1.jpg (40548 bytes)

Representative Actual TMT test data (zipped file)          Back to Motor Testing Page