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

Status: Retired 1995. Thrust: 386.30 kN (86,844 lbf). Gross mass: 117,826 kg (259,761 lb). Unfuelled mass: 4,926 kg (10,859 lb). Specific impulse: 316 s. Specific impulse sea level: 214 s. Burn time: 309 s. Height: 20.12 m (66.01 ft). Diameter: 3.05 m (10.00 ft). Span: 4.90 m (16.00 ft).

Cost $ : 11.000 million.



Country: USA. Engines: LR105-5. Launch Vehicles: Atlas E, Atlas E CGM-16E, Atlas F HGM-16F, Atlas F, Atlas F/Trident, Atlas E/Trident, Atlas F/PTS, Atlas F/MSD, Atlas F/SVS, Atlas F/Agena D, Atlas F/OIS, Atlas E/MSD, Atlas E/SVS, Atlas E/SGS-2, Atlas E/OIS, Atlas E Altair. Propellants: Lox/Kerosene.

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