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Centaur G
Part of Centaur stage series
LOx/LH2 propellant rocket stage. Centaur for Titan 4.

Status: Retired 2005. Thrust: 146.80 kN (33,002 lbf). Gross mass: 23,880 kg (52,640 lb). Unfuelled mass: 2,775 kg (6,117 lb). Specific impulse: 444 s. Burn time: 625 s. Height: 9.00 m (29.50 ft). Diameter: 4.33 m (14.20 ft). Span: 4.33 m (14.20 ft).

Cost $ : 23.000 million. No Engines: 2.



Family: Space Tugs. Country: USA. Engines: RL-10A-3A. Launch Vehicles: Titan 401A/Centaur, Titan 401B/Centaur, Titan 404B. Propellants: Lox/LH2.

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