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Saturn S-IB-2
Part of S-I stage
LOx/Kerosene propellant rocket stage. .

Status: Study 1960. Thrust: 13,339.96 kN (2,998,941 lbf). Gross mass: 725,491 kg (1,599,433 lb). Unfuelled mass: 68,014 kg (149,945 lb). Specific impulse: 304 s. Specific impulse sea level: 265 s. Burn time: 139 s. Height: 34.50 m (113.10 ft). Diameter: 8.25 m (27.06 ft). Span: 10.00 m (32.00 ft).

No Engines: 2.



Country: USA. Engines: F-1. Launch Vehicles: Saturn C-3. Propellants: Lox/Kerosene.

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