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Aerojet 62
Aerojet N2O4/MMH rocket engine. In Production. Mixture Ratio(O/F): 1.65.

Status: In Production. Thrust: 62 N (13 lbf). Unfuelled mass: 1.13 kg (2.49 lb). Specific impulse: 287 s.

Engine: 1.13 kg (2.49 lb). Area Ratio: 150. Thrust to Weight Ratio: 5.59.

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