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RD-108-8D75PS

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-108-8D75PS Part of RD-107 RD-107 Credit: © Mark Wade Glushko LOx/Kerosene rocket engine. Sputnik 8K71PS-1. Out of Production. Diameter is per chamber. First flight 1957. AKA: 8D75PS. Status: Out of Production. Number: 32 . Thrust: 912.00 kN (205,025 lbf). Unfuelled mass: 1,250 kg (2,750 lb). Specific impulse: 308 s. Specific impulse sea level: 241 s. Burn time: 340 s. Height: 2.86 m (9.38 ft). Diameter: 0.67 m (2.19 ft). Chambers: 4. Thrust (sl): 713.600 kN (160,424 lbf). Thrust (sl): 72,768 kgf. Engine: 1,250 kg (2,750 lb). Chamber Pressure: 53.00 bar. Area Ratio: 18.9. Thrust to Weight Ratio: 74.4. Country: Russia. Launch Vehicles: Sputnik 8K71PS. Propellants: Lox/Kerosene. Stages: Sputnik 8K71PS-1. Agency: Glushko bureau. 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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