SE-7-1 Credit: Boeing / Rocketdyne |
Date: 1965. Thrust: 313 N (70 lbf). Specific impulse: 274 s.
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. |