SM-65D Atlas
Convair
Manufacturer
Convair
Family
Atlas, Atlas D
Maiden flight
1959-04-14
Length
25.15 m
Diameter
3 m
Payload to LEO
1,400 kg
Launches
9
Successful
6
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.


Atlas DFailure
OV1-11,12,86 · United States Air Force
Thursday, Jul 27, 1967, 19:00 UTC

Atlas DSuccess
OV1-9 & 10 · United States Air Force
Sunday, Dec 11, 1966, 21:09 UTC

Atlas DSuccess
OV1-7 · United States Air Force
Thursday, Jul 14, 1966, 02:10 UTC

Atlas DSuccess
OV1-4 & 5 · United States Air Force
Wednesday, Mar 30, 1966, 09:20 UTC

Atlas DSuccess
OV1-2 · United States Air Force
Tuesday, Oct 5, 1965, 09:07 UTC

Atlas DFailure
OV1-3 · United States Air Force
Friday, May 28, 1965, 02:54 UTC

Atlas DSuccess
FIRE 2 · United States Air Force
Saturday, May 22, 1965, 21:55 UTC

Atlas DFailure
OV1-1 · United States Air Force
Thursday, Jan 21, 1965, 21:34 UTC

Atlas DSuccess
FIRE 1 · United States Air Force
Tuesday, Apr 14, 1964, 21:42 UTC
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