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Centaur B-X
Part of Centaur stage series Family
LOx/LH2 propellant rocket stage. Conceptual design, 1998. Not put into production.

Status: Development 1998. Thrust: 186.80 kN (41,994 lbf). Gross mass: 19,138 kg (42,192 lb). Unfuelled mass: 2,358 kg (5,198 lb). Specific impulse: 470 s. Burn time: 408 s. Height: 10.10 m (33.10 ft). Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft).

Cost $ : 21.000 million. No Engines: 2.



Family: Space Tugs. Country: USA. Engines: RL-10B-X. Propellants: Lox/LH2.

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