Atlas IIAS
Lockheed Martin
Details
Height
47.54 m
Diameter
3.04 m
GTO
2,810 kg
LEO
6,580 kg
Thrust at Liftoff
4,391 kN
Apogee
Unknown
Launch Cost
Unknown
Maiden Flight
December 16, 1993
Description
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.