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R-40B


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A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z R-40B Part of R-40 engine series
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. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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