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Shuttle HCR-1
Part of Shuttle-1 stage series Family
LOx/LH2 propellant rocket stage. Swept wing configuration.

Status: Study 1969. Thrust: 29,135.63 kN (6,549,949 lbf). Gross mass: 1,634,467 kg (3,603,382 lb). Unfuelled mass: 304,535 kg (671,384 lb). Specific impulse: 442 s. Specific impulse sea level: 392 s. Burn time: 195 s. Height: 70.79 m (232.25 ft). Diameter: 10.00 m (32.00 ft). Span: 46.04 m (151.04 ft).

No Engines: 14.



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

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