Saturn MS-LRB-23(L)

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Saturn MS-LRB-23(L)

Part of Saturn LRB stage series

LOx/Kerosene propellant rocket stage. Liquid rocket booster strap-ons using 2 F-1's.

Status: Study 1967. Thrust: 15,486.60 kN (3,481,526 lbf). Gross mass: 874,100 kg (1,927,000 lb). Unfuelled mass: 18,100 kg (39,900 lb). Specific impulse: 304 s. Specific impulse sea level: 265 s. Burn time: 162 s. Height: 47.85 m (156.98 ft). Diameter: 6.61 m (21.68 ft). Span: 6.61 m (21.68 ft).

No Engines: 2.

Country: USA. Engines: F-1. Launch Vehicles: Saturn V-23(L), Saturn V-24(L). Propellants: Lox/Kerosene.

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