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Shuttle R134C-2
Part of Shuttle-2 stage series Family
LOx/LH2 propellant rocket stage. Delta winged configuration.

Status: Study 1970. Thrust: 4,804.13 kN (1,080,011 lbf). Gross mass: 424,449 kg (935,749 lb). Unfuelled mass: 138,910 kg (306,240 lb). Specific impulse: 459 s. Specific impulse sea level: 359 s. Burn time: 264 s. Height: 64.02 m (210.03 ft). Diameter: 4.57 m (14.99 ft). Span: 37.80 m (124.00 ft).

No Engines: 2.



Country: USA. Engines: SSME Study. Launch Vehicles: Shuttle R134C. Propellants: Lox/LH2.

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