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

AKA: Atlas B. Status: Out of production. Thrust: 363.22 kN (81,655 lbf). Gross mass: 107,610 kg (237,230 lb). Unfuelled mass: 3,980 kg (8,770 lb). Specific impulse: 309 s. Specific impulse sea level: 215 s. Burn time: 240 s. Height: 21.90 m (71.80 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 B, Atlas C. Propellants: Lox/Kerosene.

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