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UR-100 Stage 2
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Gross Mass: 8,611 kg (18,984 lb). Empty Mass: 900 kg (1,980 lb). Thrust (vac): 131.448 kN (29,551 lbf). Isp: 325 sec. Burn time: 184 sec. Propellants: N2O4/UDMH. Diameter: 2.00 m (6.50 ft). Span: 1.30 m (4.20 ft). Length: 6.69 m (21.95 ft). Country: Russia. No Engines: 1. Engine: 8D423. Status: Design 1964. First Flight: 1965. Last Flight: 1984. No Launched: 282. Other designations: 8K84 Stage 2. Orevo has sectioned hardware. Total mass, thrust accurate; Isp, empty mass and burn time estimated. Source: Placard, Orevo.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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