This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 16,320 kg.
Empty Mass: 7,200 kg. Thrust (vac): 26,800 kgf. Isp: 373 sec. Burn time: 127 sec. Propellants: Lox/LH2 Isp(sl): 316 sec. Diameter: 3.1 m. Span: 3.7 m. Length: 11.9 m. Country: USA. No Engines: 4. RL-10A-5 Status: Dev 1991.
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Last update 12 March 2001.
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© Mark Wade, 2001 .