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Atlas MA-2
Status: Out of production. Thrust: 1,517.42 kN (341,130 lbf). Gross mass: 3,050 kg (6,720 lb). Unfuelled mass: 3,050 kg (6,720 lb). Specific impulse: 282 s. Specific impulse sea level: 248 s. Burn time: 135 s. Diameter: 4.90 m (16.00 ft). Span: 4.90 m (16.00 ft).
No Engines: 2.
Country: USA. Engines: XLR89-5. Launch Vehicles: Atlas Able, Atlas B, Atlas C, Atlas D, Atlas C Able, Atlas D Able, Atlas Agena A, Atlas LV-3B / Mercury, Atlas Centaur, Atlas Centaur D. Propellants: Lox/Kerosene.
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