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Saturn MLV 5-23L-0
Part of Saturn LRB stage series Family
LOx/Kerosene propellant rocket stage. Liquid strap-on booster studied for improved Saturn V.

Status: Study 1966. Thrust: 15,484.00 kN (3,480,941 lbf). Gross mass: 1,180,000 kg (2,600,000 lb). Unfuelled mass: 80,000 kg (176,000 lb). Specific impulse: 304 s. Specific impulse sea level: 265 s. Burn time: 200 s. Height: 51.00 m (167.00 ft). Diameter: 6.61 m (21.68 ft). Span: 6.61 m (21.68 ft).

No Engines: 2.



Country: USA. Engines: F-1. Propellants: Lox/Kerosene.

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