Saturn MS-IC-1

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Saturn MS-IC-1

Part of Saturn IC

LOx/Kerosene propellant rocket stage. Basic Saturn IC stretched 240 inches with F-1A engines uprated 20% in thrust and 6 second improvement in specific impulse.

Status: Study 1967. Thrust: 45,948.75 kN (10,329,691 lbf). Gross mass: 2,694,703 kg (5,940,803 lb). Unfuelled mass: 169,719 kg (374,166 lb). Specific impulse: 310 s. Specific impulse sea level: 270 s. Burn time: 158 s. Height: 48.15 m (157.97 ft). Diameter: 10.06 m (33.00 ft). Span: 19.00 m (62.00 ft).

No Engines: 5.

Country: USA. Engines: F-1A. Launch Vehicles: Saturn MLV-V-1, Saturn MLV-V-2, Saturn MLV-V-3, Saturn MLV-V-1/J-2T/200K, Saturn MLV-V-1/J-2T/250K, Saturn V-24(L), Saturn MLV-V-4(S)-B. Propellants: Lox/Kerosene.

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