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Centaur G Prime
Part of Centaur stage series Family
LOx/LH2 propellant rocket stage. Centaur for Shuttle payload bay. Cancelled after Challenger disaster on safety grounds.

Status: Out of production. Thrust: 146.80 kN (33,002 lbf). Gross mass: 19,501 kg (42,992 lb). Unfuelled mass: 3,000 kg (6,600 lb). Specific impulse: 444 s. Burn time: 550 s. Height: 8.87 m (29.10 ft). Diameter: 4.33 m (14.20 ft). Span: 4.33 m (14.20 ft).

Cost $ : 22.000 million. No Engines: 2.



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

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