Saturn MS-II-1A

Gross Mass: 600,800 kg (1,324,500 lb). Empty Mass: 60,000 kg (132,000 lb). Thrust (vac): 6,380.941 kN (1,434,493 lbf). Isp: 421 sec. Burn time: 345 sec. Propellants: Lox/LH2. Isp(sl): 200 sec. Diameter: 10.06 m (33.00 ft). Span: 10.06 m (33.00 ft). Length: 29.59 m (97.08 ft). Country: USA. No Engines: 7. Engine: J-2. Status: Study 1966.

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

Used on Launch Vehicles:

Saturn MLV-V-1A.

Saturn V-ELV.

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