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Shuttle LS A-1
Part of Starlifter Family
LOx/LH2 propellant rocket stage. Delta winged configuration.

Status: Study 1969. Thrust: 26,076.59 kN (5,862,250 lbf). Gross mass: 1,225,668 kg (2,702,135 lb). Unfuelled mass: 162,494 kg (358,237 lb). Specific impulse: 442 s. Specific impulse sea level: 392 s. Burn time: 754 s. Height: 67.07 m (220.04 ft). Diameter: 10.00 m (32.00 ft). Span: 31.40 m (103.00 ft).

No Engines: 13.



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

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