ABOUT ATLAS CENTAUR
The Atlas-Centaur was a US expendable launch vehicle derived from the SM-65 Atlas D missile. Launches were conducted from Launch Complex 36 at the Cape Canaveral Air Force Station in Florida.
PAYLOAD CAPACITY
1,800 kg
TO GTO
3,969 lbs
LIFTOFF THRUST
1,704
KILONEWTONS
383,075
POUNDS-FORCE
~2,285
HORSEPOWER