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X-34A-2
LOx/Kerosene propellant rocket stage. Original design for the second stage of the X-34A.

Status: Development ended 1996. Thrust: 44.10 kN (9,914 lbf). Gross mass: 4,500 kg (9,900 lb). Unfuelled mass: 300 kg (660 lb). Specific impulse: 348 s. Burn time: 325 s. Height: 4.00 m (13.10 ft). Diameter: 2.00 m (6.50 ft). Span: 2.00 m (6.50 ft).

Cost $ : 2.000 million.



Country: USA. Engines: FastTrack. Launch Vehicles: X-34A. Propellants: Lox/Kerosene.

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