R-29-1

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Model: Vysota-1. Gross Mass: 20,000 kg (44,000 lb). Thrust (vac): 682.000 kN (153,319 lbf). Burn time: 74 sec. Propellants: N2O4/UDMH. Diameter: 1.90 m (6.20 ft). Length: 7.70 m (25.20 ft). Country: Russia. No Engines: 1. Motor: RD R-29 (1). Status: Retired 1996. First Flight: 1969. Last Flight: 1996. No Launched: 30. Used as: R-29. Release conditions: Makeev. Model: R-29-1. Gross Mass: 20,000 kg (44,000 lb). Thrust (vac): 682.000 kN (153,319 lbf). Burn time: 74 sec. Propellants: N2O4/UDMH. Diameter: 1.90 m (6.20 ft). Length: 7.70 m (25.20 ft). Country: Russia. No Engines: 1. Motor: RD-0244. Status: Active. First Flight: 1983. Last Flight: 2007. No Launched: 33. Used as: R-29. Release conditions: Makeev. Model: Volna-1. Gross Mass: 20,000 kg (44,000 lb). Thrust (vac): 682.000 kN (153,319 lbf). Burn time: 74 sec. Propellants: N2O4/UDMH. Diameter: 1.90 m (6.20 ft). Length: 7.70 m (25.20 ft). Country: Russia. No Engines: 1. Motor: RD R-29R (1). Status: Out of production. Used as: R-29. Release conditions: Makeev. Used on Launch Vehicles: R-29. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted.