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Atlas D (SM-65D)

Atlas D (SM-65D) was the first operational model of the United States Atlas intercontinental ballistic missile and the direct basis for several early American space boosters. Its pressure-stabilized stainless-steel airframe used a stage-and-a-half propulsion arrangement; retired missiles and D-series hardware supported Mercury, reentry-vehicle research, and Orbiting Vehicle 1 missions after the weapon left alert service.

Identity

Aliases
SM-65D AtlasConvair Atlas DAtlas SM-65D
Family Name
Atlas
Full Name
Atlas D (SM-65D)
Reusability
expendable
Slug
atlas-d-sm-65d
Status
retired
Type
rocket
Variant Name
D / SM-65D

Details

Description
Atlas D (SM-65D) was the first operational model of the United States Atlas intercontinental ballistic missile and the direct basis for several early American space boosters. Its pressure-stabilized stainless-steel airframe used a stage-and-a-half propulsion arrangement; retired missiles and D-series hardware supported Mercury, reentry-vehicle research, and Orbiting Vehicle 1 missions after the weapon left alert service.
Diameter M
3.05
First Flight Year
1,959
Last Flight Year
1,967
Liftoff Mass Kg
117,934
Manufacturer
Operator
Parent Vehicle Family

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Creation Time
July 18, 2026 at 19:48:37 UTC
Updated Time
July 18, 2026 at 19:48:37 UTC