This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 40,000 kg.
Empty Mass: 4,000 kg. Thrust (vac): 32,000 kgf. Isp: 427 sec. Burn time: 480 sec. Propellants: Lox/LH2 Diameter: 5.8 m. Span: 5.8 m. Length: 13.1 m. Country: USA. No Engines: 5. RL-10 Status: Study General Dynamics 1960. Comments: .
Back to Index
Last update 12 March 2001.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .