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Shuttle R134G-1
Part of Shuttle-1 stage series
LOx/LH2 propellant rocket stage. Delta winged configuration.

Status: Study 1970 November. Thrust: 28,824.77 kN (6,480,067 lbf). Gross mass: 1,600,000 kg (3,500,000 lb). Specific impulse: 442 s. Specific impulse sea level: 392 s. Height: 78.35 m (257.05 ft). Diameter: 10.37 m (34.02 ft). Span: 43.30 m (142.00 ft).

No Engines: 12.



Country: USA. Engines: SSME Study. Propellants: Lox/LH2.

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