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SM-65E Atlas

Atlas familyConvairRetired

The SM-65E Atlas, or Atlas-E, was an operational variant of the Atlas missile. It first flew on 11 October 1960, and was deployed as an operational ICBM from September 1961 until April 1966. Following retirement as an ICBM, the Atlas-E, along with the Atlas-F, was refurbished for orbital launches as the Atlas E/F.

SM-65E Atlas vehicle

Specifications

Diameter
3.05 m
Launch mass
121 t
Stages
1
LEO capacity
820 kg

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

Flight record

15flightswith a definitive outcome
100%success rate15 of 15
15success streakcurrent

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

Flights

5 of 15

All 15 flights