This page no longer updated from 31 October 2001.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

Family: Saturn V. Country: USA. Status: Study 1968.

MSFC study, 1968. S-ID stage-and-a-half first stage and Saturn IVB second stage. Centaur available as third stage for deep space missions. 30% performance improvement over Saturn V-A/Saturn INT-20 with standard Saturn IC first stage.


LEO Payload: 81,600 kg. to: 185 km Orbit. at: 28.0 degrees. Payload: 20,400 kg. to a: Translunar trajectory. Liftoff Thrust: 3,440,290 kgf. Total Mass: 2,504,020 kg. Core Diameter: 10.1 m. Total Length: 72.0 m.


Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .