This page no longer updated from 31 October 2001. Latest version can be found at Saturn IC C-5A

Gross Mass: 2,217,285 kg. Empty Mass: 131,495 kg. Thrust (vac): 3,901,230 kgf. Isp: 304 sec. Burn time: 160 sec. Propellants: Lox/Kerosene Isp(sl): 265 sec. Diameter: 10.1 m. Span: 19.0 m. Length: 42.9 m. Country: USA. No Engines: 5. F-1 Status: Study 1961. Used as: Saturn C-5A-1. Comments: Final first stage design of Saturn C-5 (November 1961) before selection as Apollo launch vehicle and development in Saturn V.
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 .