Atlas II
Lockheed Martin
Manufacturer
Lockheed Martin
Family
Atlas, Atlas II
Maiden flight
1991-12-07
Length
47.54 m
Diameter
3.04 m
Payload to LEO
6,580 kg
Payload to GTO
2,810 kg
Launches
10
Successful
10
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.
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Atlas IISuccess
UHF F/O F8 · Lockheed Martin
Monday, Mar 16, 1998, 21:32 UTC
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Atlas IISuccess
UHF F/O F7 · Lockheed Martin
Thursday, Jul 25, 1996, 12:41 UTC
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Atlas IISuccess
UHF F/O F6 · Lockheed Martin
Sunday, Oct 22, 1995, 08:00 UTC
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Atlas IISuccess
UHF F/O F5 · Lockheed Martin
Wednesday, May 31, 1995, 15:27 UTC
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Atlas IISuccess
UHF F/O F4 · United States Air Force
Sunday, Jan 29, 1995, 01:25 UTC
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Atlas IISuccess
DSCS-3 B10 · United States Air Force
Sunday, Nov 28, 1993, 23:40 UTC
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Atlas IISuccess
DSCS-3 B9 · United States Air Force
Monday, Jul 19, 1993, 22:04 UTC
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Atlas IISuccess
DSCS-3 B12 · United States Air Force
Thursday, Jul 2, 1992, 21:54 UTC
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Atlas IISuccess
DSCS-3 B14 · United States Air Force
Tuesday, Feb 11, 1992, 00:41 UTC
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Atlas IISuccess
Eutelsat II F-3 · United States Air Force
Saturday, Dec 7, 1991, 22:47 UTC
No media yet. Livestreams usually appear shortly before launch.