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Centaur I
Part of Centaur stage series
LOx/LH2 propellant rocket stage. .

Status: Out of production. Thrust: 146.80 kN (33,002 lbf). Gross mass: 15,600 kg (34,300 lb). Unfuelled mass: 1,700 kg (3,700 lb). Specific impulse: 444 s. Burn time: 402 s. Height: 9.15 m (30.01 ft). Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft).

Cost $ : 20.300 million. No Engines: 2.



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

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