This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 2,278,800 kg.
Empty Mass: 127,000 kg. Thrust (vac): 3,948,100 kgf. Isp: 304 sec. Burn time: 161 sec. Propellants: Lox/Kerosene Isp(sl): 265 sec. Diameter: 10.1 m. Span: 19.0 m. Length: 36.5 m. Country: USA. No Engines: 5. F-1 Status: Study MSFC 1965. Comments: Standard S-IC but with reduced length and structural weight through use of 'flat' bulkheads consisting of multiple conical sections.
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 .