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Saturn V-MLV-1
Saturn V-MLV-1 -

Credit: © Mark Wade. 6,031 bytes. 173 x 853 pixels.

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

MSFC study, 1965. Improved Saturn V configuration studied under contract NAS8-11359. 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 strengthened but with standard 230,000 lbs propellant, 1 J-2 engine.


LEO Payload: 137,250 kg. to: 185 km Orbit. at: 28.0 degrees. Payload: 49,600 kg. to a: Translunar trajectory. Liftoff Thrust: 4,080,890 kgf. Total Mass: 3,501,350 kg. Core Diameter: 10.1 m. Total Length: 111.0 m.


Saturn MLV 1.37Saturn MLV 1.37

Credit: © Mark Wade. 5,187 bytes. 135 x 760 pixels.

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Last update 12 March 2001.
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