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Aerojet 2
Aerojet N2O4/MMH rocket engine. In Production. Mixture Ratio(O/F): 1.65.

Status: In Production. Thrust: 2.00 N (0.40 lbf). Unfuelled mass: 0.27 kg (0.59 lb). Specific impulse: 265 s.

Engine: 0.27 kg (0.59 lb). Area Ratio: 150. Thrust to Weight Ratio: .75.



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

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