SE-7-85

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SE-7-85

Part of SE-7-1

SE-7/85 lb thrust
Credit: Boeing / Rocketdyne

Rocketdyne N2O4/MMH rocket engine. Gemini Orbit Attitude and Maneuvering System (85 lb thrust). Pressure-fed. First flight 1964.

Date: 1963. Thrust: 372 N (83 lbf). Specific impulse: 295 s.

Family: Storable liquid. Country: USA. Propellants: N2O4/MMH. Agency: Rocketdyne.

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