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Aerojet 21

Engine · USA

Original archive entry. The text, images and links below are kept as they were written.

Aerojet N2O4/MMH rocket engine. In Production. Mixture Ratio(O/F): 1.60.

Engine: 0.57 kg (1.25 lb). Area Ratio: 75. Thrust to Weight Ratio: 3.81.

Country
USA
Propellants
N2O4/MMH
Agency
Aerojet