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Aerojet 445
Aerojet N2O4/MMH rocket engine. In Production. Mixture Ratio(O/F): 1.65.

Status: In Production. Thrust: 445 N (100 lbf). Unfuelled mass: 1.86 kg (4.10 lb). Specific impulse: 309 s.

Engine: 1.86 kg (4.10 lb). Area Ratio: 150. Thrust to Weight Ratio: 24.39.



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

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