| Saturn MLV 5-23L-0 |
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Model: Saturn MLV 5-23L-0. Gross Mass: 1,180,000 kg (2,600,000 lb). Empty Mass: 80,000 kg (176,000 lb). Thrust (vac): 15,484.000 kN (3,480,941 lbf). Isp: 304 sec. Burn time: 200 sec. Propellants: Lox/Kerosene. Isp(sl): 265 sec. Diameter: 6.61 m (21.68 ft). Span: 6.61 m (21.68 ft). Length: 51.00 m (167.00 ft). Country: USA. No Engines: 2. Motor: F-1. Status: Study 1966. Liquid strap-on booster studied for improved Saturn V. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted. |