This page no longer updated from 31 October 2001. Latest version can be found at Saturn MS-II-3B

Gross Mass: 643,200 kg. Empty Mass: 53,500 kg. Thrust (vac): 1,270,100 kgf. Isp: 447 sec. Burn time: 204 sec. Propellants: Lox/LH2 Isp(sl): 200 sec. Diameter: 10.1 m. Span: 10.1 m. Length: 29.6 m. Country: USA. No Engines: 5. Toroidal 400k Status: Study Boeing 1967. Comments: S-II with 15.5 foot stretch, 1.29 million pounds propellant, 7 x 400,000 lb thrust toroidal engines.
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 .