← ALL VEHICLES
LOCKHEED MARTIN

Atlas IIA

23FLIGHTS
100%SUCCESS
23STREAK
Jun 1992FIRST FLIGHT
NOREUSABLE
HEIGHT47.54 m
DIAMETER3.04 m
LAUNCH MASS204 kg
LIFTOFF THRUST2,479 kN
STAGES3

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.

6,580 kg
TO LEO
14,509 lbs
2,810 kg
TO GTO
6,196 lbs
2,479
KILONEWTONS
557,302
POUNDS-FORCE
~3,324
HORSEPOWER
Height47.54 m (156 ft)
Diameter3.04 m (10 ft)
Launch Mass204 kg (450 lbs)
Stages3