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Spacemaster-1
Part of Starlifter Family
LOx/LH2 propellant rocket stage. Unique Catamaran configuration.

Status: Study 1967. Thrust: 28,082.54 kN (6,313,206 lbf). Gross mass: 1,224,490 kg (2,699,530 lb). Unfuelled mass: 203,342 kg (448,292 lb). Specific impulse: 442 s. Specific impulse sea level: 392 s. Burn time: 155 s. Height: 57.93 m (190.05 ft). Diameter: 8.00 m (26.20 ft). Span: 45.12 m (148.03 ft).

No Engines: 14.



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

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