This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 67,100 kg.
Empty Mass: 67,100 kg. Thrust (vac): 3,157,300 kgf. Isp: 304 sec. Burn time: 154 sec. Propellants: Lox/Kerosene Isp(sl): 265 sec. Diameter: 10.1 m. Span: 19.0 m. Length: 42.1 m. Country: USA. No Engines: 4. F-1 Status: Study 1967. Comments: Boeing studies, 1967:'Stage and a half' S-1C with four outboard F-1's jettisoned and inboard F-1 functioning as sustainer as in Atlas. Booster half stage recoverable. Mass estimated based on double mass of four F-1's (based on Atlas example).
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 .