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astronautix.com Saturn V-25(S)B

Saturn V 156
Saturn V 156" SRB - Saturn V 156 inch strapons

Credit: © Mark Wade. 6,714 bytes. 154 x 1002 pixels.



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

Boeing study, 1967. 4 156 inch solid propellant boosters; Saturn IC stretched 498 inches with 6.64 million pounds propellant and 5 F-1 engines; S-II standard length with 5 J-2 engines; S-IVB stretched 198 inches with 350,000 lbs propellant, 1 J-2 engine.


Specifications

LEO Payload: 223,500 kg. to: 185 km Orbit. at: 28.0 degrees. Payload: 85,600 kg. to a: Translunar trajectory. Liftoff Thrust: 7,376,460 kgf. Total Mass: 6,342,540 kg. Core Diameter: 10.1 m. Total Length: 123.0 m. Flyaway Unit Cost $: 174.00 million. in 1985 unit dollars.



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