Lockheed Martin
Atlas IIA
IIA

Retired
Overview
/01Atlas 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.
Manufacturer
Lockheed Martin
Variant
IIA
Alias
N/A
Maiden Flight
June 10, 1992
Technical Specifications
/0247.54 m
Length
3.04 m
Diameter
0 t
Launch Mass
2479 kN
Liftoff Thrust
6580 kg
LEO Capacity
2810 kg
GTO Capacity
Launch Record
/0323
Total Launches
23
Successful
0
Failed
100.0%
Success Rate
0
Attempted Landings
0
Successful Landings
0
Failed Landings
0
Consecutive Successes