SM-65D Atlas Vehicle Overview
A complete overview of the SM-65D Atlas launch vehicle, including launch stats, vehicle info and launch locations.
Basic Info
Name
SM-65D Atlas
Family
Atlas
Manufacturer
First Launch
14 Apr 1959
Successful Launches
6
Failed Launches
3
Rocket Info
Status
Inactive
Stages
1
Length
25.15 m
Diameter
3 m
Launch Mass
119 tons
Thrust
1,880 kN
Reusability
Not Reusable
Payload Info
LEO Capacity
1,400 kg
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.
Launch Sites used by SM-65D Atlas
Cape Canaveral Space Force Station
Historic U.S. military rocket launch site, pivotal in space exploration and national security.
Vandenberg SFB
U.S. Space Force facility in California for spacecraft launches and missile testing.