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SE-7-1
SE-7-1
SE-7-1
Credit: Boeing / Rocketdyne
Rocketdyne N2O4/MMH rocket engine. S-IVB Stage APS Ullage Control Engine (propellant settling). Pressure-fed. First flight 1966.

Date: 1965. Thrust: 313 N (70 lbf). Specific impulse: 274 s.



Subtopics

SE-7-100 Rocketdyne N2O4/MMH rocket engine. Gemini Orbit Attitude and Maneuvering System (100 lb thrust). Pressure-fed. First flight 1964.

SE-7-85 Rocketdyne N2O4/MMH rocket engine. Gemini Orbit Attitude and Maneuvering System (85 lb thrust). Pressure-fed. First flight 1964.

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

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