This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com

astronautix.com Saturn V-24(L)


Family: Saturn V. Country: USA. Status: Study 1967.

Boeing study, 1967. 4 260 inch liquid propellant boosters (each with 2 F-1A).; Saturn IC stretched 336 inches with 6.0 million pounds propellant and 5 F-1A engines; S-II stretched 156 inches with 1.2 million pounds propellant and 5 HG-3 engines; S-IVB stretched 198 inches with 350,000 lbs propellant, 1 HG-3 engine. Not studied in detail since vehicle height of 600 feet with payload exceeded study limit of 410 feet.


Specifications

LEO Payload: 435,300 kg. to: 185 km Orbit. at: 28.0 degrees. Payload: 185,900 kg. to a: Translunar trajectory. Liftoff Thrust: 9,587,310 kgf. Total Mass: 7,386,760 kg. Core Diameter: 10.1 m. Total Length: 180.0 m.



Bibliography:



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 .