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RD-704

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-704 Glushko LOx/Kerosene/LH2 tripropellant engine. Developed 1990's. 452 s. Tripropellant engine, single chamber, derived from RD-701 project. Chamber pressure 294 / 124 bar. First flight 1999. Status: Developed 1990's. Date: 1990's. Thrust: 1,966.00 kN (441,974 lbf). Unfuelled mass: 2,422 kg (5,339 lb). Specific impulse: 407 s. Specific impulse sea level: 356 s. Height: 3.81 m (12.49 ft). Diameter: 1.77 m (5.80 ft). Mass excluding sensors, gimbal actuators and heat shield. Mass excluding sensors, gimbal actuators and heat shield. Throttled thrust(vac): 782.000 kN (175,800 lbf). Thrust (sl): 1,720.100 kN (386,694 lbf). Thrust (sl): 175,403 kgf. Engine: 2,422 kg (5,339 lb). Chamber Pressure: 294.00 bar. Thrust to Weight Ratio: 82.77. Country: Russia. Propellants: Lox/Kerosene/LH2, Lox/LH2. Agency: Glushko bureau. Bibliography: 319, 7527. 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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