This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 950,000 kg.
Empty Mass: 60,000 kg. Thrust (vac): 1,578,650 kgf. Isp: 304 sec. Burn time: 170 sec. Propellants: Lox/Kerosene Isp(sl): 265 sec. Diameter: 8.4 m. Span: 8.4 m. Length: 35.0 m. Country: USA. No Engines: 2. F-1 Status: Study.
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 .