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-854
RD-854 Credit: via Dietrich Haeseler |
Yuzhnoye N2O4/UDMH rocket engine. R-36orb (SS-X-10) orbital stage. Out of Production. Thrust vector control by 4 nozzles fed from gas generator.
Status: Out of Production. Date: 1962-67. Thrust: 75.50 kN (16,973 lbf). Unfuelled mass: 100 kg (220 lb). Specific impulse: 312 s. Burn time: 70 s. Height: 1.51 m (4.94 ft). Diameter: 1.53 m (5.01 ft).
Chambers: 1 + 4. Engine: 100 kg (220 lb). Chamber Pressure: 85.30 bar. Thrust to Weight Ratio: 76.99. Oxidizer to Fuel Ratio: 2.02.
Family:
Storable liquid.
Country:
Ukraine.
Launch Vehicles:
R-36O 8K69.
Propellants:
N2O4/UDMH.
Agency:
Yuzhnoye.
Bibliography:
348.
Back to top of page
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
© 1997-2019 Mark Wade - Contact
© / Conditions for Use