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| | Fact Sheet - ATLAS II (Site not responding. Last check: 2007-10-31) |
 | | The total thrust capability of the Atlas II of 490,000 pounds enables the booster to lift payloads of 6,100 pounds in geosynchronous orbit (22,000 miles-plus). |
 | | Atlas II also has lower-cost electronics, an improved flight computer and longer propellant tanks than its predecessor, Atlas I. Atlas IIs are launched from Cape Canaveral Air Force Station, Fla., by the 45th Space Wing and, in the future, will be launched by the 30th Space Wing at Vandenberg Air Force Base, Calif. |
 | | Atlas space launch vehicles were used in all three unmanned lunar exploration programs. |
| www.au.af.mil /au/awc/space/factsheets/atlas_ii.htm (421 words) |
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