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Centaur G STS
Part of Centaur stage series
LOx/LH2 propellant rocket stage. .

Status: Out of production. Thrust: 146.80 kN (33,002 lbf). Gross mass: 16,327 kg (35,994 lb). Unfuelled mass: 2,600 kg (5,700 lb). Specific impulse: 444 s. Burn time: 420 s. Height: 5.95 m (19.52 ft). Diameter: 4.33 m (14.20 ft). Span: 4.33 m (14.20 ft).

Cost $ : 21.000 million. No Engines: 2.



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

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