Saturn MS-II-1A

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Saturn MS-II-1A

Part of Saturn II

LOx/LH2 propellant rocket stage. Basic Saturn II with 187 inch stretch of propellant tanks, 1.2 million pound propellant capacity, and 7 J-2 engines.

Status: Study 1966. Thrust: 6,380.94 kN (1,434,493 lbf). Gross mass: 600,800 kg (1,324,500 lb). Unfuelled mass: 60,000 kg (132,000 lb). Specific impulse: 421 s. Specific impulse sea level: 200 s. Burn time: 345 s. Height: 29.59 m (97.08 ft). Diameter: 10.06 m (33.00 ft). Span: 10.06 m (33.00 ft).

No Engines: 7.

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

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