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Atlas Able stage
Part of Atlas A stage Family
LOx/Kerosene propellant rocket stage. .

AKA: Atlas Able. Status: Retired 1960. Thrust: 363.22 kN (81,655 lbf). Gross mass: 114,495 kg (252,418 lb). Unfuelled mass: 4,200 kg (9,200 lb). Specific impulse: 309 s. Specific impulse sea level: 215 s. Burn time: 275 s. Height: 20.64 m (67.71 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 D Able. Propellants: Lox/Kerosene.

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