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Magnum Core
LOx/LH2 propellant rocket stage. Alternative configurations used 2 to 3 RS-68 engines.

Status: Study 1996. Thrust: 9,112.38 kN (2,048,544 lbf). Gross mass: 830,000 kg (1,820,000 lb). Unfuelled mass: 70,000 kg (154,000 lb). Specific impulse: 453 s. Specific impulse sea level: 363 s. Burn time: 500 s. Height: 53.00 m (173.00 ft). Diameter: 8.40 m (27.50 ft). Span: 8.40 m (27.50 ft).

No Engines: 4.



Country: USA. Engines: SSME. Launch Vehicles: Magnum HLLV. Propellants: Lox/LH2.

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