Saturn MS-IC-23(L)

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Saturn MS-IC-23(L)

Part of Saturn IC

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

Status: Study 1967. Thrust: 38,703.16 kN (8,700,816 lbf). Gross mass: 2,694,000 kg (5,939,000 lb). Unfuelled mass: 169,000 kg (372,000 lb). Specific impulse: 304 s. Specific impulse sea level: 265 s. Burn time: 192 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-1. Launch Vehicles: Saturn V-23(L). Propellants: Lox/Kerosene.

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