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astronautix.com Saturn MLV-V-1/J-2T/250K


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

MSFC study, 1965. Improved Saturn V configuration studied under contract NAS8-11359. Variant of MLV-V-1 with toroidal J-2T-250K engines replacing standard J-2 engines in upper stages.


Specifications

at: 28.0 degrees. Liftoff Thrust: 4,080,890 kgf. Total Mass: 3,216,150 kg. Core Diameter: 10.1 m. Total Length: 89.0 m.



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Last update 12 March 2001.
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