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Atlas Centaur SLV-3C/D
Part of Atlas A stage Family
LOx/Kerosene propellant rocket stage.

Status: Out of production. Thrust: 386.30 kN (86,844 lbf). Gross mass: 128,500 kg (283,200 lb). Unfuelled mass: 4,000 kg (8,800 lb). Specific impulse: 316 s. Specific impulse sea level: 220 s. Burn time: 430 s. Height: 22.20 m (72.80 ft). Diameter: 3.05 m (10.00 ft). Span: 4.90 m (16.00 ft).

Cost $ : 14.210 million.



Country: USA. Engines: LR105-5. Launch Vehicles: Atlas SLV-3C Centaur, Atlas SLV-3D Centaur. Propellants: Lox/Kerosene.

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