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X-34A-1
Part of X-34 Family
LOx/Kerosene propellant rocket stage. Original design for the winged first stage of the X-34A.

Status: Development ended 1996. Thrust: 386.30 kN (86,844 lbf). Gross mass: 29,500 kg (65,000 lb). Unfuelled mass: 6,700 kg (14,700 lb). Specific impulse: 316 s. Specific impulse sea level: 220 s. Burn time: 180 s. Height: 21.95 m (72.01 ft). Diameter: 3.05 m (10.00 ft). Span: 10.37 m (34.02 ft).

Cost $ : 1.000 million.



Country: USA. Engines: RS-56-OSA. Launch Vehicles: X-34A. Propellants: Lox/Kerosene.

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