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Delta E

From Wikipedia, the free encyclopedia
American expendable launch vehicle
This article is about the rocket. For the difference between colours, seecolor difference.

Launch of a Delta E withPioneer 6
FunctionExpendable launch system
Country of originUnited States
Launch history
StatusRetired
Launch sitesCape CanaveralLC-17
VandenbergSLC-2E
Total launches23
Success(es)23
First flight6 November 1965
Last flight1 April 1971

TheDelta E, orThor-Delta E was an Americanexpendable launch system used for twenty-threeorbital launches between 1965 and 1971. It was a member of theDelta family of rockets.[1]

The first stage was aThor missile in theDSV-2C configuration, and the second stage was the Delta-E, which was derived from the earlierDelta-A.[2][3][4] ThreeCastor-1solid rocket boosters were clustered around the first stage. Two differentsolid-fuel upper stages were available; anAltair-2 was used on the baseline version, however this could be replaced with anFW-4D to increase performance. A Delta E with the FW-4D upper stage was designated Delta E1. Six flights used the Delta E configuration and seventeen used the Delta E1.[5][6]

Delta E rockets were launched fromCape Canaveral Air Force StationLaunch Complex 17 andVandenberg Air Force BaseSpace Launch Complex 2E. All 23 flights were successful. On December 16 1965, a Delta E launched thePioneer 6space probe.[1][4]

References

[edit]
  1. ^abWade, Mark."Delta". Archived fromthe original on 2008-07-24.
  2. ^Wade, Mark (2016-12-28)."Delta E". Archived fromthe original on 2016-12-28. Retrieved2024-01-30.
  3. ^Wade, Mark (2016-12-28)."Delta A". Archived fromthe original on 2016-12-28. Retrieved2024-01-30.
  4. ^abKrebs, Gunter."Thor Family".Gunter's Space Page.Archived from the original on 2007-08-06. Retrieved2021-12-21.
  5. ^Krebs, Gunter."Delta-E".Gunter's Space Page. Retrieved2024-01-30.
  6. ^Krebs, Gunter."Delta-E1".Gunter's Space Page. Retrieved2024-01-30.
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