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R-36-0-2
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Gross Mass: 48,000 kg (105,000 lb). Empty Mass: 5,000 kg (11,000 lb). Thrust (vac): 955.991 kN (214,915 lbf). Isp: 317 sec. Burn time: 160 sec. Propellants: N2O4/UDMH. Diameter: 3.00 m (9.80 ft). Span: 3.00 m (9.80 ft). Length: 9.40 m (30.80 ft). Country: Ukraine. No Engines: 1. Engine: RD-252. Status: Out of production. Cost $ : 2.000 million. First Flight: 1965. Last Flight: 1971. No Launched: 25.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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