ABOUT ATLAS IIAS
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
4,391
KILONEWTONS
987,136
POUNDS-FORCE
~5,888
HORSEPOWER
FLIGHT HISTORY
Atlas IIAS | NROL-1
Atlas IIAS | AMC 11
Atlas IIAS | Superbird A2
Atlas IIAS | AMC 10
Atlas IIAS | NROL-18
Atlas IIAS | Hispasat 1D
Atlas IIAS | NROL-12
Atlas IIAS | NROL-13
Atlas IIAS | ICO F2
Atlas IIAS | GOES-L
Atlas IIAS | NROL-10
Atlas IIAS | Echostar VI
Atlas IIAS | Hispasat 1C
Atlas IIAS | Terra
Atlas IIAS | Echostar V
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