MR-UR-100-1

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Model: MR-UR-100 St 1. Gross Mass: 59,000 kg (130,000 lb). Empty Mass: 5,000 kg (11,000 lb). Thrust (vac): 1,236.000 kN (277,863 lbf). Propellants: N2O4/UDMH. Diameter: 2.25 m (7.38 ft). Length: 14.30 m (46.90 ft). Country: Ukraine. No Engines: 1. Motor: RD-268. Status: Retired 1988. First Flight: 1971. Last Flight: 1984. No Launched: 87. Used as: MR-UR-100. Release conditions: Yuzhnoe. Model: Perimetr Stage 1. Gross Mass: 59,000 kg (130,000 lb). Empty Mass: 5,000 kg (11,000 lb). Thrust (vac): 1,236.000 kN (277,863 lbf). Propellants: N2O4/UDMH. Diameter: 2.25 m (7.38 ft). Length: 14.90 m (48.80 ft). Country: Ukraine. No Engines: 1. Motor: RD-268. Status: Retired 1988. First Flight: 1979. Last Flight: 1988. No Launched: 11. Used as: MR-UR-100. Release conditions: Yuzhnoe. Used on Launch Vehicles: MR-UR-100. 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.