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

AKA: Atlas Centaur LV-3C. Status: Retired 1961. Thrust: 363.22 kN (81,655 lbf). Gross mass: 117,350 kg (258,710 lb). Unfuelled mass: 3,700 kg (8,100 lb). Specific impulse: 309 s. Specific impulse sea level: 215 s. Burn time: 335 s. Height: 18.30 m (60.00 ft). Diameter: 3.05 m (10.00 ft). Span: 4.90 m (16.00 ft).

Cost $ : 14.210 million.



Country: USA. Engines: XLR105-5. Launch Vehicles: Atlas Centaur LV-3C. Propellants: Lox/Kerosene.

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