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Centaur C-X
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Gross Mass: 19,138 kg (42,192 lb). Empty Mass: 2,358 kg (5,198 lb). Thrust (vac): 110.800 kN (24,909 lbf). Isp: 450 sec. Burn time: 660 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: 1. Engine: RL-10C-X. Status: Development 1998. Cost $ : 21.000 million. First Flight: 2001.
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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