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R-42
R-42
R-42
Credit: Aerojet Redmond
Redmond N2O4/MMH rocket engine. In Production.

Status: In Production. Thrust: 890 N (200 lbf). Unfuelled mass: 4.53 kg (9.98 lb). Specific impulse: 303 s. Burn time: 3,940 s. Height: 0.79 m (2.59 ft). Diameter: 0.39 m (1.27 ft).

Engine: 4.53 kg (9.98 lb). Chamber Pressure: 7.10 bar. Area Ratio: 160. Restarts: 134.



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

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