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astronautix.com Saturn INT-20

S-1C details
S-1C details

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


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

Saturn variant consisting of S-IC first stage and S-IVB second stage. Consideration was given to deleting one or more of the F-1 engines in the first stage.

Liftoff Mass - kgS-IC - No. F-1 MotorsPayload - kg - 4.68 G limitPayload - kg - 6.0 G limit
1,107,000236,00027,000
1,655,000378,00047,000
2,209,0004132,00063,000
2,299,0005133,00072,000

Specifications

LEO Payload: 60,000 kg. to: 185 km Orbit. at: 28.0 degrees. Liftoff Thrust: 3,440,310 kgf. Total Mass: 2,478,120 kg. Core Diameter: 10.1 m. Total Length: 72.0 m. Flyaway Unit Cost $: 391.50 million. in 1985 unit dollars.



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