Shuttle LS A-2

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Shuttle LS A-2

Part of Starlifter

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

Status: Study 1969. Thrust: 6,823.56 kN (1,533,997 lbf). Gross mass: 406,344 kg (895,835 lb). Unfuelled mass: 104,891 kg (231,245 lb). Specific impulse: 459 s. Specific impulse sea level: 359 s. Burn time: 196 s. Height: 49.70 m (163.00 ft). Diameter: 8.00 m (26.20 ft). Span: 28.05 m (92.02 ft).

No Engines: 3.

Country: USA. Engines: SSME Study. Launch Vehicles: Shuttle LS A. Propellants: Lox/LH2.

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