This page no longer updated from 31 October 2001.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

Family: Saturn V. Country: USA. Status: Study 1966.

NASA study, 1966. No-height-limitation stretched Saturn with Titan UA1207 motors for thrust augmentation.


LEO Payload: 200,000 kg. to: 185 km Orbit. at: 28.0 degrees. Payload: 67,000 kg. to a: Translunar trajectory. Liftoff Thrust: 6,056,370 kgf. Total Mass: 5,172,820 kg. Core Diameter: 10.1 m. Total Length: 124.0 m. Flyaway Unit Cost $: 97.44 million. in 1985 unit dollars.


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 .