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R-36M2-2
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Gross Mass: 41,114 kg (90,640 lb). Empty Mass: 4,374 kg (9,643 lb). Thrust (vac): 760.000 kN (170,850 lbf). Isp: 340 sec. Burn time: 190 sec. Propellants: N2O4/UDMH. Diameter: 3.00 m (9.80 ft). Span: 3.00 m (9.80 ft). Length: 5.70 m (18.70 ft). Country: Ukraine. No Engines: 1. Engine: RD-0255. Cost $ : 3.000 million. First Flight: 1986. Last Flight: 2006. No Launched: 42. Surplus ICBMs; failures based on ICBM tests through 1994.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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