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

AKA: Atlas D. Status: Out of production. Thrust: 363.22 kN (81,655 lbf). Gross mass: 113,050 kg (249,230 lb). Unfuelled mass: 2,347 kg (5,174 lb). Specific impulse: 309 s. Specific impulse sea level: 215 s. Burn time: 303 s. Height: 21.20 m (69.50 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 Able, Atlas D, Atlas C Able, Atlas LV-3B / Mercury, Atlas Centaur, Atlas Centaur D. Propellants: Lox/Kerosene.

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