Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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
RD-0231
Kosberg N2O4/UDMH rocket engine. P-700 Granit. Out of Production. Staged combustion cycle. First flight 1970.

Status: Out of Production. Date: 1968-70. Thrust: 29.00 kN (6,519 lbf). Unfuelled mass: 28 kg (61 lb). Specific impulse: 275 s. Burn time: 16 s. Height: 0.60 m (1.96 ft). Diameter: 0.15 m (0.49 ft).

Engine: 28 kg (61 lb). Chamber Pressure: 123.00 bar. Thrust to Weight Ratio: 105.71.



Family: Storable liquid. Country: Russia. Spacecraft: Granat. Propellants: N2O4/UDMH. Agency: Kosberg bureau. Bibliography: 307.

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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
© 1997-2017 Mark Wade - Contact
© / Conditions for Use