Saturn MS-IC-1A

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Saturn MS-IC-1A

Part of Saturn IC

LOx/Kerosene propellant rocket stage. Basic Saturn IC stretched 240 inches with 6 F-1 engines.

Status: Study 1965. Thrust: 46,443.30 kN (10,440,869 lbf). Gross mass: 2,694,700 kg (5,940,700 lb). Unfuelled mass: 160,600 kg (354,000 lb). Specific impulse: 304 s. Specific impulse sea level: 265 s. Burn time: 160 s. Height: 48.16 m (158.00 ft). Diameter: 10.06 m (33.00 ft). Span: 19.01 m (62.36 ft).

No Engines: 6.

Country: USA. Engines: F-1. Launch Vehicles: Saturn MLV-V-1A. Propellants: Lox/Kerosene.

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