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Centaur IIA
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Gross Mass: 19,073 kg (42,048 lb). Empty Mass: 2,293 kg (5,055 lb). Thrust (vac): 185.012 kN (41,592 lbf). Isp: 449 sec. Burn time: 392 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-4. Status: Out of production. Cost $ : 30.000 million. First Flight: 1992. Last Flight: 2004. No Launched: 53.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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