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astronautix.com Saturn MLV-V-4(S)-A

Saturn V 120
Saturn V 120" SRB - Saturn V 120 inch strapons

Credit: © Mark Wade. 5,874 bytes. 161 x 996 pixels.



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

MSFC study, 1965. 4 Titan UA1205 solid rocket boosters; Saturn IC stretched 337 inches with 6.0 million pounds propellant and 5 F-1 engines; S-II with 970,000 pounds propellant and 5 J-2 engines; S-IVB strengthened but with standard 230,000 lbs propellant, 1 J-2 engine.


Specifications

LEO Payload: 160,880 kg. to: 185 km Orbit. at: 28.0 degrees. Payload: 57,500 kg. to a: Translunar trajectory. Liftoff Thrust: 5,600,700 kgf. Total Mass: 4,615,440 kg. Core Diameter: 10.1 m. Total Length: 113.0 m. Flyaway Unit Cost $: 71.92 million. in 1985 unit dollars.



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