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

AKA: Atlas IIAS. Status: Out of production. Thrust: 386.30 kN (86,844 lbf). Gross mass: 161,950 kg (357,030 lb). Unfuelled mass: 6,050 kg (13,330 lb). Specific impulse: 316 s. Specific impulse sea level: 220 s. Burn time: 283 s. Height: 24.90 m (81.60 ft). Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft).

Cost $ : 60.000 million.



Country: USA. Engines: RS-56-OSA. Launch Vehicles: Atlas IIAS. Propellants: Lox/Kerosene.

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