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Aerojet 21
Aerojet N2O4/MMH rocket engine. In Production. Mixture Ratio(O/F): 1.60.

Status: In Production. Thrust: 21 N (5 lbf). Unfuelled mass: 0.57 kg (1.25 lb). Specific impulse: 285 s.

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



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

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