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Atlas · Convair

Atlas IIAS

retired
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Specifications

Status
retired
Height
47.54 m
Diameter
3.04 m
Mass
204,000 kg
Stages
3
Payload to LEO
6,580 kg
Payload to GTO
2,810 kg
First flight
1993-12-16
Total launches
30
Success / Fail
30 / 0

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.

Payloads it launched · 30

USA 179
HEO
AMC-11
GEO
SUPERBIRD-A2
GEO
AMC-10 (GE-10)
GEO
USA 173
LEO
HISPASAT 30W-4
GEO
USA 162
GEO
USA 160
LEO
OMNI-M1
MEO
USA 155
GEO
ECHOSTAR 6
GEO
HISPASAT 1C
GEO
TERRA
LEO
ECHOSTAR 5
GEO
EUTELSAT 48C
GEO
JCSAT-4A
GEO
INTELSAT 805 (IS-805)
GEO
NSS-806
GEO
GALAXY 8 (G-8)
GEO
ECHOSTAR 3
GEO
AMC-3
GEO
SUPERBIRD-A3
GEO
INTELSAT 26 (IS-26)
GEO
PAKSAT 1 (ANATOLIA 1)
GEO