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Status: Out of Production. Date: 1976-88. Thrust: 86.30 kN (19,401 lbf). Unfuelled mass: 230 kg (500 lb). Specific impulse: 362 s. Burn time: 680 s. Height: 2.27 m (7.44 ft). Diameter: 1.17 m (3.83 ft).
Engine: 230 kg (500 lb). Chamber Pressure: 79.40 bar. Area Ratio: 189. Thrust to Weight Ratio: 38.26. Oxidizer to Fuel Ratio: 2.42.
Country: Russia. Propellants: Lox/Kerosene. Agency: Korolev bureau. Bibliography: 21, 315, 404, 42, 95. 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 © 1997-2017 Mark Wade - Contact © / Conditions for Use |