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Ares I-2
LOx/LH2 propellant rocket stage. Second stage figures as of summer 2008. Dry mass includes 2500 kg for avionics bay.

Status: In development. Thrust: 1,304.00 kN (293,150 lbf). Gross mass: 158,500 kg (349,400 lb). Unfuelled mass: 20,500 kg (45,100 lb). Specific impulse: 448 s. Burn time: 450 s. Height: 25.60 m (83.90 ft). Diameter: 5.50 m (18.00 ft). Span: 5.50 m (18.00 ft).



Country: USA. Engines: J-2X. Propellants: Lox/LH2.

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