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astronautix.com Saturn V-4X(U)


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

Boeing study, 1968. Four core vehicles from Saturn V-25(S) study lashed together to obtain million-pound payload using existing hardware. First stage consisted of 4 Saturn IC's stretched 498 inches with 6.64 million pounds propellant and 5 F-1 engines; second stage 4 Saturn II standard length stages with 5 J-2 engines


Specifications

LEO Payload: 527,600 kg. to: 486 km Orbit. at: 28.0 degrees. Liftoff Thrust: 16,329,230 kgf. Total Mass: 15,504,720 kg. Core Diameter: 10.1 m. Total Length: 95.0 m.



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Last update 12 March 2001.
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