Encyclopedia Astronautica 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-108-8D75K  R-7 aft end Credit: � Mark Wade AKA: 8D75K. Number: 488 . Thrust: 941.00 kN (211,545 lbf). Unfuelled mass: 1,252 kg (2,760 lb). Specific impulse: 315 s. Specific impulse sea level: 248 s. Burn time: 340 s. Height: 2.86 m (9.38 ft). Diameter: 0.67 m (2.19 ft).
Chambers: 4. Thrust (sl): 740.400 kN (166,449 lbf). Thrust (sl): 75,504 kgf. Engine: 1,252 kg (2,760 lb). Chamber Pressure: 51.00 bar. Area Ratio: 18.9. Thrust to Weight Ratio: 76.59.
Country: Russia. Launch Vehicles: R-7A, Molniya 8K78, Voskhod 11A57, Vostok 8A92, Sputnik 11A59, Vostok 8A92M. Propellants: Lox/Kerosene. Stages: Molniya 8K78-1, R-7A 8K74-1, Vostok 8A92-1, Voskhod 11A57-1, Vostok 8A92M-1. Agency: Glushko bureau.
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 � 1997-2016 Mark Wade - Contact � / Conditions for Use |
