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Gross Mass: 5,352,400 kg. Empty Mass: 317,400 kg. Thrust (vac): 7,257,500 kgf. Isp: 455 sec. Burn time: 310 sec. Propellants: Lox/LH2 Isp(sl): 367 sec. Diameter: 21.9 m. Span: 21.9 m. Length: 78.6 m. Country: USA. No Engines: 12. CD Module Status: Study 1969. Comments: Boeing study, 1969.
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Last update 12 March 2001.
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© Mark Wade, 2001 .