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Atlas · Convair

SM-65D Atlas

retired
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Specifications

Status
retired
Height
25.15 m
Diameter
3 m
Mass
119,000 kg
Stages
1
Payload to LEO
1,400 kg
First flight
1959-04-14
Total launches
9
Success / Fail
6 / 3

The SM-65D Atlas, or Atlas D, was the first operational version of the U.S. Atlas missile. Atlas D was first used as an intercontinental ballistic missile (ICBM) to deliver a nuclear weapon payload on a suborbital trajectory. It was later developed as a launch vehicle to carry a payload to low Earth orbit on its own, and later to geosynchronous orbit, to the Moon, Venus, or Mars with the Agena or Centaur upper stage.

Payloads it launched · 8

OV1-12
LEO
OV1-86
LEO
OV1-10
LEO
OV1-9
MEO
OV1-8
LEO
OV1-5
LEO
OV1-4
LEO
OV1-2
MEO