This page no longer updated from 31 October 2001. Latest version can be found at Saturn S-II-8

Gross Mass: 770,835 kg. Empty Mass: 63,480 kg. Thrust (vac): 842,822 kgf. Isp: 425 sec. Burn time: 338 sec. Propellants: Lox/LH2 Isp(sl): 306 sec. Diameter: 10.1 m. Span: 10.1 m. Length: 42.7 m. Country: USA. No Engines: 8. J-2 Status: Study NASA Feb 62.
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 .