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Centaur V2
Part of Centaur stage series
LOx/LH2 propellant rocket stage. Dual-engine Centaur for Atlas V. For heavy payload, low earth orbit missions, Centaur will use two RL10 engines to maximize boost phase mission performance.

Status: Active. Thrust: 198.40 kN (44,602 lbf). Gross mass: 23,050 kg (50,810 lb). Unfuelled mass: 2,250 kg (4,960 lb). Specific impulse: 451 s. Burn time: 435 s. Height: 12.68 m (41.60 ft). Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft).

No Engines: 2.

Family: Space Tugs. Country: USA. Engines: RL-10A-4-2. Launch Vehicles: Atlas 3B DEC. Propellants: Lox/LH2.
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