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Shuttle DC-3-1
Part of Shuttle-1 stage series Family
LOx/LH2 propellant rocket stage. Faget Configuration.

Status: Study 1970. Thrust: 10,290.00 kN (2,313,280 lbf). Gross mass: 799,537 kg (1,762,677 lb). Unfuelled mass: 131,519 kg (289,949 lb). Specific impulse: 442 s. Specific impulse sea level: 392 s. Burn time: 277 s. Height: 61.89 m (203.05 ft). Diameter: 5.08 m (16.66 ft). Span: 42.99 m (141.04 ft).

Cost $ : 20.000 million. No Engines: 4.



Country: USA. Engines: SSME Study. Launch Vehicles: Shuttle DC-3. Propellants: Lox/LH2.

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