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Starlifter
LOx/LH2 propellant rocket stage. .

Status: Study 1966. Thrust: 5,217.00 kN (1,172,828 lbf). Gross mass: 42,630 kg (93,980 lb). Unfuelled mass: 19,955 kg (43,993 lb). Specific impulse: 455 s. Specific impulse sea level: 355 s. Burn time: 228 s. Height: 25.00 m (82.00 ft). Diameter: 15.85 m (52.00 ft). Span: 15.85 m (52.00 ft).

Cost $ : 18.000 million. No Engines: 3.



Subtopics

Spacemaster-1 LOx/LH2 propellant rocket stage. Unique Catamaran configuration.

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

Shuttle LS A-1 LOx/LH2 propellant rocket stage. Delta winged configuration.

Shuttle LS A-2 LOx/LH2 propellant rocket stage. High-fineness lifting-body configuration. Cross Range 2,419 km.

Shuttle LS200-1 LOx/LH2 propellant rocket stage. High-fineness lifting-body configuration. Cross Range 2,419 km.

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

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