ABOUT ATLAS IIA
Atlas II was a member of the Atlas family of launch vehicles, which evolved from the successful Atlas missile program of the 1950s. It was designed to launch payloads into low earth orbit, geosynchronous transfer orbit or geosynchronous orbit. Sixty-three launches of the Atlas II, IIA and IIAS models were carried out between 1991 and 2004; all sixty-three launches were successes, making the Atlas II the most reliable launch system in history.
PAYLOAD CAPACITY
6,580 kg
TO LEO
14,509 lbs
2,810 kg
TO GTO
6,196 lbs
LIFTOFF THRUST
2,479
KILONEWTONS
557,302
POUNDS-FORCE
~3,324
HORSEPOWER
FLIGHT HISTORY
Atlas IIA | TDRS 10
Atlas IIA | TDRS 9
Atlas IIA | GOES 12
Atlas IIA | DSCS-3 B11
Atlas IIA | TDRS 8
Atlas IIA | GOES 11
Atlas IIA | DSCS-3 B8
Atlas IIA | UHF F/O F10
Atlas IIA | UHF F/O F9
Atlas IIA | Hot Bird 5
Atlas IIA | NROL-5
Atlas IIA | DSCS-3 B13
Atlas IIA | Tempo 2
Atlas IIA | INMARSAT III F-3
Atlas IIA | Hot Bird 2
⚙ RELATED ENGINES
🚀 OTHER LOCKHEED MARTIN VEHICLES