SM-65D Atlas
Convair
Details
Height
25.15 m
Diameter
3 m
GTO
Unknown
LEO
1,400 kg
Thrust at Liftoff
1,880 kN
Apogee
Unknown
Launch Cost
Unknown
Maiden Flight
April 14, 1959
Description
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.
Agency
Convair