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SE-6

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SE-6 Credit: Boeing / Rocketdyne

Date: 1963. Thrust: 107 N (24 lbf). Specific impulse: 277 s.

SE-7-25 Rocketdyne N2O4/MMH rocket engine. Gemini Orbit Attitude and Maneuvering System (25 lb thrust). Pressure-fed. First flight 1964.

SE-9-3 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.