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Shuttle NAR A-2
Part of Shuttle-2 stage series Family
LOx/LH2 propellant rocket stage. Faget Straight Wing Configuration - Cross Range 2,000 km.

Status: Study 1969. Thrust: 5,256.89 kN (1,181,797 lbf). Gross mass: 395,011 kg (870,850 lb). Unfuelled mass: 121,542 kg (267,954 lb). Specific impulse: 459 s. Specific impulse sea level: 359 s. Burn time: 231 s. Height: 61.59 m (202.06 ft). Diameter: 6.71 m (22.01 ft). Span: 44.51 m (146.03 ft).

No Engines: 2.



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

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