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RD-190

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-190 Part of RD-120 Glushko LOx/LCH4 rocket engine. Riksha-0 stage 1. Developed 1996-. The RD-190 consists of 6 RD-169 engines. Each chamber can be gimbaled individually in two planes by +/- 8 degree. Status: Developed 1996-. Date: 1996-. Thrust: 1,000.00 kN (224,800 lbf). Unfuelled mass: 1,470 kg (3,240 lb). Specific impulse: 351 s. Specific impulse sea level: 309 s. Height: 1.70 m (5.50 ft). Diameter: 2.40 m (7.80 ft). Chambers: 6. Engine: 1,470 kg (3,240 lb). Chamber Pressure: 147.00 bar. Thrust to Weight Ratio: 69.36. Oxidizer to Fuel Ratio: 3.4. Country: Russia. Launch Vehicles: Riksha. Propellants: Lox/LCH4. Agency: Glushko bureau. Bibliography: 325. 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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