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Atlas MA-5A
Status: Out of production. Thrust: 2,093.70 kN (470,682 lbf). Gross mass: 4,187 kg (9,230 lb). Unfuelled mass: 4,187 kg (9,230 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 Burner 2, Atlas II, Atlas IIA. Propellants: Lox/Kerosene.
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