Saturn MS-II-1

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Saturn MS-II-1

Part of Saturn II

LOx/LH2 propellant rocket stage. Basic Saturn II with 41 inch stretch of hydrogen tank.

Status: Study 1965. Thrust: 5,165.79 kN (1,161,316 lbf). Gross mass: 521,447 kg (1,149,593 lb). Unfuelled mass: 49,877 kg (109,959 lb). Specific impulse: 425 s. Specific impulse sea level: 306 s. Burn time: 361 s. Height: 25.88 m (84.90 ft). Diameter: 10.06 m (33.00 ft). Span: 10.06 m (33.00 ft).

No Engines: 5.

Country: USA. Engines: J-2. Launch Vehicles: Saturn MLV-V-1, Saturn MLV-V-2, Saturn MLV-V-4(S)-A. Propellants: Lox/LH2.

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