Ares Stage 2

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Ares Stage 2

LOx/LH2 propellant rocket stage. Second stage proposed later in design stage by NASA for launch of CEV into low earth orbit. All masses estimated.

Status: In development. Thrust: 1,113.00 kN (250,212 lbf). Gross mass: 172,000 kg (379,000 lb). Unfuelled mass: 13,200 kg (29,100 lb). Specific impulse: 465 s. Burn time: 640 s. Height: 16.00 m (52.00 ft). Diameter: 10.00 m (32.00 ft). Span: 10.00 m (32.00 ft).

Country: USA. Launch Vehicles: Ares I-X, Ares V. Propellants: Lox/LH2.

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