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SE-9-5
SE-9-3 / SE-9-5
SE-9-3 / SE-9-5
Credit: Boeing / Rocketdyne
Rocketdyne N2O4/Aerozine-50 rocket engine. Titan III Transtage. Pressure-fed. System included two modules of three engines plus two additional SE-9-5 separate engines, tanks, and a pressurization system. First flight 1964.

Date: 1964. Thrust: 196 N (44 lbf). Specific impulse: 300 s.

Family: Storable liquid. Country: USA. Propellants: N2O4/Aerozine-50. Agency: Rocketdyne.
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