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astronautix.com Saturn V-D

Saturn V 260
Saturn V 260" SRB - Saturn V 260 inch strapons

Credit: © Mark Wade. 5,217 bytes. 155 x 914 pixels.



Family: Saturn V. Country: USA. Status: Study 1968.

MSFC study, 1968. Rehashed the Boeing 1967 studies, covering a variety of stage stretches and 120, 156, or 260 inch solid rocket boosters, but with S-ID stage-and-a-half first stage.


Specifications

LEO Payload: 326,500 kg. to: 185 km Orbit. at: 28.0 degrees. Payload: 112,000 kg. to a: Translunar trajectory. Liftoff Thrust: 16,503,750 kgf. Total Mass: 9,882,100 kg. Core Diameter: 10.1 m. Total Length: 102.0 m. Flyaway Unit Cost $: 736.60 million. in 1985 unit dollars.



Bibliography:



Saturn II stageSaturn II stage

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