This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 52,144 kg.
Empty Mass: 6,801 kg. Thrust (vac): 90,686 kgf. Isp: 420 sec. Burn time: 207 sec. Propellants: Lox/LH2 Isp(sl): 200 sec. Diameter: 5.6 m. Span: 5.6 m. Length: 15.4 m. Country: USA. No Engines: 1. J-2 Status: Study 1961. Used as: Saturn C-3B-3. Comments: Final common third stage design for Saturn C-3B (November 1961).
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 .