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Centaur D/E
Part of Centaur stage series Family
LOx/LH2 propellant rocket stage. .

Status: Study 1968. Thrust: 131.22 kN (29,500 lbf). Gross mass: 16,258 kg (35,842 lb). Unfuelled mass: 2,631 kg (5,800 lb). Specific impulse: 444 s. Burn time: 470 s. Height: 9.60 m (31.40 ft). Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft).

Cost $ : 20.300 million. No Engines: 2.



Family: Space Tugs. Country: USA. Engines: RL-10A-3, MR-106. Launch Vehicles: Titan 3BAS2, Atlas Centaur D, Saturn IB-A, Saturn IB-CE, Titan 3L2, Titan 3L4, Atlas SLV-3C Centaur, Saturn V-Centaur, Atlas SLV-3D Centaur, Titan IIIE. Propellants: Lox/LH2.

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