This page no longer updated from 31 October 2001. Latest version can be found at Saturn INT-05

Saturn 1B/260
Saturn 1B/260" SRB - Saturn 1B with 260 in solid replacing S-1B

Credit: © Mark Wade. 2,899 bytes. 78 x 667 pixels.

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

NASA Study, 1965: Half length 260 inch solid motor with S-IVB upper stage.


LEO Payload: 27,200 kg. to: 185 km Orbit. at: 28.0 degrees. Liftoff Thrust: 1,632,930 kgf. Total Mass: 982,790 kg. Core Diameter: 6.6 m. Total Length: 43.0 m. Flyaway Unit Cost $: 58.00 million. in 1985 unit dollars.


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