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astronautix.com Saturn MLV-V-2


Saturn V-MLV-2Saturn V-MLV-2

Credit: © Mark Wade. 3,167 bytes. 990 x 162 pixels.



Family: Saturn V. Country: USA. Status: Study 1965.

MSFC study, 1965. Saturn IC stretched 240 inches with 5.6 million pounds propellant and 5 F-1A engines; S-II stretched 41 inches with 1.0 million pounds propellant and 5 J-2 engines; S-IVB stretched 198 inches with 350,000 lbs propellant, 1 HG-3 engine.


Specifications

LEO Payload: 137,250 kg. to: 185 km Orbit. at: 28.0 degrees. Payload: 53,550 kg. to a: Translunar trajectory. Liftoff Thrust: 4,080,890 kgf. Total Mass: 3,557,450 kg. Core Diameter: 10.1 m. Total Length: 117.0 m.



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Last update 12 March 2001.
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