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Gross Mass: 84,000 kg. Empty Mass: 6,000 kg. Thrust (vac): 107,200 kgf. Isp: 373 sec. Burn time: 271 sec. Propellants: Lox/LH2 Isp(sl): 316 sec. Diameter: 5.0 m. Span: 5.0 m. Length: 20.0 m. Country: USA. No Engines: 16. RL-10A-5 Status: Study 1993.
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Last update 12 March 2001.
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© Mark Wade, 2001 .