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R-40B
Part of R-40 engine series Family
R-40B
R-40B
Credit: Aerojet Redmond
Redmond N2O4/MMH rocket engine. In Production.

Status: In Production. Thrust: 4.00 kN (899 lbf). Unfuelled mass: 7.23 kg (15.93 lb). Specific impulse: 293 s. Burn time: 23,000 s. Height: 0.71 m (2.33 ft). Diameter: 0.40 m (1.32 ft).

Engine: 7.23 kg (15.93 lb). Chamber Pressure: 10.34 bar. Area Ratio: 60. Restarts: 50000.



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

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