Motor Manufacturer

AEROTECH

Nozzle Throat dia(in)

0.158

Manuf Metric Designation

H112J-6/10/14

Exit Cone diameter(in)

0.31

TMT Metric Designation

H89J-6/10/14 (63% H)

Samples per sec

480

Testing Date

9/13/99

Burntime eval (%)

5

Certified Until

12/31/02

Calculated burntime(s)

2.92

Motor dimen(in)

1.5 X 7.948

Total Impul lbs-s (N-s)

58.7 (261.1Ns)

Motor dimen(mm)

38 X 202

Max Thrust lbs (N)

27.4 (121.7N)

Propellant Wt. lbs (g)

.422 (191.2g)

Ave Thrust lbs (N)

20.1 (89.4N)

Isp lbs-s/lbs

139.0

Representative TMT Thrust Curve            Back to Motor Testing Page   Back to Certified Motors Page

wpe3.jpg (39726 bytes)
"Representative" Actual TMT test data
    Full size data file - (zipped file)
    Short version
    WRASP ".eng" file
    WRASP comparative graph

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