1 specifications
1.1 general characteristics
1.2 components
1.3 performance
specifications
working parts on display @ midland air museum
general characteristics
type: rocket engine
length: 42 in (1,067 mm)
diameter: 12 in (305 mm)
dry weight: 366 lb (166 kg)
fuel: hydrogen peroxide/kerosene
components
pumps:
performance
thrust: 4,000 lbf (18 kn) 30 seconds rated @ 8,000 lbf (35.6 kn)
burn time:
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