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-108-11D512  R-7 aft end Credit: � Mark Wade AKA: 11D512. Status: Design 2000. Number: 752 . Thrust: 997.00 kN (224,134 lbf). Unfuelled mass: 1,400 kg (3,000 lb). Specific impulse: 315 s. Specific impulse sea level: 248 s. Burn time: 286 s. Height: 2.86 m (9.38 ft). Diameter: 0.67 m (2.19 ft).
Chambers: 4. Thrust (sl): 746.400 kN (167,797 lbf). Thrust (sl): 76,100 kgf. Engine: 1,400 kg (3,000 lb). Chamber Pressure: 51.00 bar. Thrust to Weight Ratio: 72.59.
Country: Russia. Launch Vehicles: Soyuz 11A511, Soyuz-U. Propellants: Lox/Kerosene. Stages: Soyuz 11A511-1, Soyuz 11A511U-1. Agency: Glushko bureau. Bibliography: 173, 21, 225, 287.
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 |
