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Saturn IB-INT-16
Saturn IB-INT-16 -

Credit: © Mark Wade. 1,309 bytes. 55 x 396 pixels.

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

UA Studies, 1966: S-IVB upper stage with from 2 to 5 Titan UA1205, 1206, or 1207 motors as first stage, clustered around from 1 to 3 of the same motors as a second stage. S-IVB upper stage.


LEO Payload: 28,000 kg. to: 185 km Orbit. at: 28.0 degrees. Liftoff Thrust: 2,698,870 kgf. Total Mass: 1,283,570 kg. Core Diameter: 6.6 m. Total Length: 52.0 m. Flyaway Unit Cost $: 89.90 million. in 1985 unit dollars.


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