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SM-65F Atlas

Atlas familyConvairRetired

The SM-65F Atlas, or Atlas-F, was the final operational variant of the Atlas missile, only differing from the Atlas E in the launch facility and guidance package used. It first flew on 8 August 1961, and was deployed as an operational ICBM between 1961 and 1966. Following retirement as an ICBM, the Atlas-F, along with the Atlas-E, was refurbished for orbital launches as the Atlas E/F.

SM-65F Atlas vehicle

Specifications

Thrust
1,714 kN
Height
24 m
Diameter
3.05 m
Launch mass
122 t
Stages
1
LEO capacity
820 kg

Specifications from Launch Library. Figures the operator has not published are omitted.

Flight record

9flightswith a definitive outcome
88.9%success rate8 of 9
4success streakcurrent

Counted from padside's own launch record, the same basis as the stats page.

Flights

5 of 9

All 9 flights