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Gross Mass: 63,000 kg.
Empty Mass: 5,000 kg. Thrust (vac): 46,000 kgf. Isp: 427 sec. Burn time: 533 sec. Propellants: Lox/LH2 Diameter: 6.7 m. Span: 6.7 m. Length: 18.3 m. Country: USA. No Engines: 7. RL-10 Status: Study General Dynamics 1960. Comments: .
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Last update 12 March 2001.
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© Mark Wade, 2001 .