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Spacemaster-2
Part of Starlifter Family
LOx/LH2 propellant rocket stage. Delta Winged, Cross Range 2,742 km.

Status: Study 1967. Thrust: 4,549.05 kN (1,022,667 lbf). Gross mass: 362,812 kg (799,863 lb). Unfuelled mass: 80,000 kg (176,000 lb). Specific impulse: 459 s. Specific impulse sea level: 359 s. Burn time: 276 s. Height: 48.78 m (160.03 ft). Diameter: 6.71 m (22.01 ft). Span: 32.62 m (107.02 ft).

No Engines: 2.



Country: USA. Engines: SSME Study. Launch Vehicles: Spacemaster. Propellants: Lox/LH2.

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