Saturn MS-II-2

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Saturn MS-II-2

Part of Saturn II

LOx/LH2 propellant rocket stage. Basic Saturn II with 187 inch stretch of propellant tanks and high chamber pressure SSME-type engines with 65% increase in thrust and 26 second improvement in specific impulse.

Status: Study 1966. Thrust: 7,003.48 kN (1,574,444 lbf). Gross mass: 600,788 kg (1,324,510 lb). Unfuelled mass: 59,844 kg (131,933 lb). Specific impulse: 451 s. Specific impulse sea level: 280 s. Burn time: 324 s. Height: 29.59 m (97.08 ft). Diameter: 10.06 m (33.00 ft). Span: 10.06 m (33.00 ft).

No Engines: 5.

Country: USA. Engines: HG-3. Launch Vehicles: Saturn MLV-V-3, Saturn V/4-260. Propellants: Lox/LH2.

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