ABOUT ATLAS IIIA
American orbital launch vehicle used between 2000 and 2005.
PAYLOAD CAPACITY
8,640 kg
TO LEO
19,051 lbs
4,055 kg
TO GTO
8,941 lbs
LIFTOFF THRUST
4,149
KILONEWTONS
932,733
POUNDS-FORCE
~5,564
HORSEPOWER
FLIGHT HISTORY
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