This page no longer updated from 31 October 2001. Latest version can be found at Saturn MLV-V-4(S)

S-1C details
S-1C details

Credit: © Mark Wade. 40,371 bytes. 510 x 391 pixels.

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

MSFC study, 1965. Saturn V core, strengthened but not stretched, with 4 Titan UA1205 strap-on solid rocket boosters.


LEO Payload: 118,000 kg. to: 185 km Orbit. at: 28.0 degrees. Payload: 52,900 kg. to a: Translunar trajectory. Liftoff Thrust: 5,599,410 kgf. Total Mass: 3,947,350 kg. Core Diameter: 10.1 m. Total Length: 102.0 m. Flyaway Unit Cost $: 463.42 million. in 1985 unit dollars.


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