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Shuttle LCR-2
Part of Shuttle-2 stage series Family
LOx/LH2 propellant rocket stage. Faget Straight Wing Configuration.

Status: Study 1969. Thrust: 4,719.64 kN (1,061,016 lbf). Gross mass: 322,449 kg (710,878 lb). Unfuelled mass: 120,816 kg (266,353 lb). Specific impulse: 459 s. Specific impulse sea level: 359 s. Burn time: 189 s. Height: 45.00 m (147.00 ft). Diameter: 8.00 m (26.20 ft). Span: 34.70 m (113.80 ft).

No Engines: 2.



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

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