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Shuttle H33-2
Part of Shuttle-2 stage series
LOx/LH2 propellant rocket stage. Delta wing configuration with drop tanks - Cross Range 1,774 km.

Status: Study 1971. Thrust: 7,079.45 kN (1,591,524 lbf). Gross mass: 474,199 kg (1,045,429 lb). Unfuelled mass: 100,153 kg (220,799 lb). Specific impulse: 459 s. Specific impulse sea level: 359 s. Burn time: 234 s. Height: 47.87 m (157.05 ft). Diameter: 8.07 m (26.47 ft). Span: 29.57 m (97.01 ft).

No Engines: 3.



Country: USA. Engines: SSME Study. Launch Vehicles: Shuttle H33. Propellants: Lox/LH2.

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