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Centaur II
Part of Centaur stage series Family
LOx/LH2 propellant rocket stage. .

Status: Out of production. Thrust: 146.80 kN (33,002 lbf). Gross mass: 18,833 kg (41,519 lb). Unfuelled mass: 2,053 kg (4,526 lb). Specific impulse: 444 s. Burn time: 488 s. Height: 10.10 m (33.10 ft). Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft).

Cost $ : 25.000 million. No Engines: 2.



Family: Space Tugs. Country: USA. Engines: RL-10A-3A. Launch Vehicles: Atlas II. Propellants: Lox/LH2.

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