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Centaur II
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Gross Mass: 18,833 kg (41,519 lb). Empty Mass: 2,053 kg (4,526 lb). Thrust (vac): 146.800 kN (33,002 lbf). Isp: 444 sec. Burn time: 488 sec. Propellants: Lox/LH2. Isp(sl): 0 sec. Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft). Length: 10.10 m (33.10 ft). Country: USA. No Engines: 2. Engine: RL-10A-3A. Status: Out of production. Cost $ : 25.000 million. First Flight: 1991. Last Flight: 1998. No Launched: 10.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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