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

Status: Study 1969. Thrust: 4,719.64 kN (1,061,016 lbf). Gross mass: 342,948 kg (756,070 lb). Unfuelled mass: 129,329 kg (285,121 lb). Specific impulse: 459 s. Specific impulse sea level: 359 s. Burn time: 201 s. Height: 48.26 m (158.33 ft). Diameter: 7.50 m (24.60 ft). Span: 29.73 m (97.53 ft).

No Engines: 2.



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

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