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CONVAIR

Atlas D

9FLIGHTS
66.7%SUCCESS
3FAILURES
Apr 1959FIRST FLIGHT
NOREUSABLE
HEIGHT25.15 m
DIAMETER3 m
LAUNCH MASS119 kg
LIFTOFF THRUST1,880 kN
STAGES1

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.

1,400 kg
TO LEO
3,087 lbs
1,880
KILONEWTONS
422,641
POUNDS-FORCE
~2,521
HORSEPOWER
Height25.15 m (83 ft)
Diameter3 m (9.8 ft)
Launch Mass119 kg (262 lbs)
Stages1