Saturn MS-LRB-23(L)

Saturn MS-LRB-23(L)

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Model: Saturn MS-LRB-23(L). Gross Mass: 874,100 kg (1,927,000 lb). Empty Mass: 18,100 kg (39,900 lb). Thrust (vac): 15,486.600 kN (3,481,526 lbf). Isp: 304 sec. Burn time: 162 sec. Propellants: Lox/Kerosene. Isp(sl): 265 sec. Diameter: 6.61 m (21.68 ft). Span: 6.61 m (21.68 ft). Length: 47.85 m (156.98 ft). Country: USA. No Engines: 2. Motor: F-1. Status: Study 1967.

Liquid rocket booster strap-ons using 2 F-1's.

Used on Launch Vehicles:

Saturn V.

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© Mark Wade, 1997 - 2008 except where otherwise noted.