This page no longer updated from 31 October 2001. Latest version can be found at Saturn V-4X(U)

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

Boeing study, 1968. Four core vehicles from Saturn V-25(S) study lashed together to obtain million-pound payload using existing hardware. First stage consisted of 4 Saturn IC's stretched 498 inches with 6.64 million pounds propellant and 5 F-1 engines; second stage 4 Saturn II standard length stages with 5 J-2 engines


LEO Payload: 527,600 kg. to: 486 km Orbit. at: 28.0 degrees. Liftoff Thrust: 16,329,230 kgf. Total Mass: 15,504,720 kg. Core Diameter: 10.1 m. Total Length: 95.0 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 .