| Magnum Core |
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Model: Magnum Core. Gross Mass: 830,000 kg (1,820,000 lb). Empty Mass: 70,000 kg (154,000 lb). Thrust (vac): 9,112.378 kN (2,048,544 lbf). Isp: 453 sec. Burn time: 500 sec. Propellants: Lox/LH2. Isp(sl): 363 sec. Diameter: 8.40 m (27.50 ft). Span: 8.40 m (27.50 ft). Length: 53.00 m (173.00 ft). Country: USA. No Engines: 4. Motor: SSME. Status: Study 1996. Alternative configurations used 2 to 3 RS-68 engines Used on Launch Vehicles: 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. | |