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Atlas MA-5AS
Part of Atlas MA engine series Family
LOx/Kerosene propellant rocket stage. .

Status: Out of production. Thrust: 2,093.70 kN (470,682 lbf). Gross mass: 5,632 kg (12,416 lb). Unfuelled mass: 5,632 kg (12,416 lb). Specific impulse: 299 s. Specific impulse sea level: 263 s. Burn time: 172 s. Diameter: 4.90 m (16.00 ft). Span: 4.90 m (16.00 ft).

No Engines: 2.



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

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