This page no longer updated from 31 October 2001. Latest version can be found at Saturn V-23(L)

Saturn MLV 5-23L
Saturn MLV 5-23L -

Credit: © Mark Wade. 6,659 bytes. 162 x 839 pixels.

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

Boeing study, 1967. 4 260 inch liquid propellant boosters (each with 2 F-1's!).; Saturn IC stretched 240 inches with 5.6 million pounds propellant and 5 F-1 engines; S-II strengthened but with standard 930,000 pounds propellant and 5 J-2 engines; S-IVB stretched 198 inches with 350,000 lbs propellant, 1 J-2 engine.


LEO Payload: 262,670 kg. to: 185 km Orbit. at: 28.0 degrees. Payload: 99,850 kg. to a: Translunar trajectory. Liftoff Thrust: 8,946,730 kgf. Total Mass: 7,178,900 kg. Core Diameter: 10.1 m. Total Length: 115.0 m.


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