This page no longer updated from 31 October 2001.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


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.


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Last update 12 March 2001.
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© Mark Wade, 2001 .