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Atlas E/F
Part of Atlas A stage
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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