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RD-107-11D511

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-107-11D511 Part of RD-107 RD-107 Credit: © Mark Wade Glushko LOx/Kerosene rocket engine. Soyuz 11A511-0, Soyuz 11A511U-0. Design 2000. Diameter is per chamber. First flight 1965. AKA: 11D511. Status: Design 2000. Number: 3008 . Thrust: 992.00 kN (223,010 lbf). Unfuelled mass: 1,200 kg (2,600 lb). Specific impulse: 314 s. Specific impulse sea level: 257 s. Burn time: 118 s. Height: 2.86 m (9.38 ft). Diameter: 0.67 m (2.19 ft). Chambers: 4. Thrust (sl): 821.600 kN (184,703 lbf). Thrust (sl): 83,800 kgf. Engine: 1,200 kg (2,600 lb). Chamber Pressure: 58.50 bar. Thrust to Weight Ratio: 84.27. Oxidizer to Fuel Ratio: 2.47. Country: Russia. Launch Vehicles: Soyuz 11A511, Soyuz-U. Propellants: Lox/Kerosene. Stages: Soyuz 11A511-0, Soyuz 11A511U-0. Agency: Glushko bureau. Bibliography: 173, 225, 287. Photo Gallery R-7 aft end Credit: © Mark Wade 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

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