This page no longer updated from 31 October 2001. Latest version can be found at Saturn INT-13

Family: Saturn I. Country: USA. Status: Study 1966.

Chrysler Studies, 1966: S-IB with 2 Titan UA1205 with standard length S-IB stage, S-IVB stage, or 2 Titan UA1207 strap-ons with 20-foot stretche S-IB stage, S-IVB stage. S-IB ignition at sea level at same time as strap-ons.


LEO Payload: 36,590 kg. to: 169 km Orbit. at: 28.0 degrees. Liftoff Thrust: 2,051,270 kgf. Total Mass: 1,307,320 kg. Core Diameter: 6.6 m. Total Length: 58.0 m. Flyaway Unit Cost $: 48.72 million. in 1985 unit dollars.


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