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Delta M

From Wikipedia, the free encyclopedia
American expendable launch system

Launch of first Delta M, withIntelsat III F-1
FunctionExpendable launch system
Country of originUnited States
Launch history
StatusRetired
Launch sitesCape Canaveral,LC-17A
Total launches13
Success(es)11
Failure2
First flight18 September 1968
Last flight17 March 1971

TheDelta M orThor-Delta M was an Americanexpendable launch system used for thirteenorbital launches between 1968 and 1971. It was a member of theDelta family of rockets.

The Delta M had a three-stage configuration. The first stage was theLong Tank Thor, a stretched version of theThor missile, previously flown on theDelta L. ThreeCastor-2solid rocket boosters were attached to the first stage to increase thrust at lift-off. ADelta E was used as the second stage, and the third stage was aStar-37Dsolid rocket motor. On the final flight, six boosters were flown instead of three, in a configuration known as the Delta M6, or "Super Six."

All thirteen launches were made fromLaunch Complex 17A at theCape Canaveral Air Force Station (CCAFS). The first launch carryingIntelsat III F-1 on 18 September 1968, was a complete failure when the first stage began suffering abnormal pitch gyrations starting at T+20 seconds. The booster maintained a stable attitude until around T+100 seconds when it pitched over and began to break up from structural loads. As the Delta was also headed back towards land,Range Safety Officer sent the destruct signal at T+108 seconds. It was bound for aGeostationary transfer orbit above theAtlantic Ocean and be in operation in time to relay broadcasts of the next month's1968 Summer Olympics inMexico City.[1][2][3]

The fifth launch on 25 July 1969,Intelsat III F-5 suffered a rupture of either the third stage casing or nozzle and ended up in an unusable orbit. Of the thirteen launches, twelve carriedgeosynchronouscommunications satellites. The thirteenth, which was the final flight and the only one in the Delta-M6 configuration, placedExplorer 43 into ahighly elliptical orbit.[4][5]

References

[edit]
  1. ^"Rocket explodes after launch; new satellite lost". The St. Petersburg Times (Florida). UPI. 19 September 1968. p. 11A.
  2. ^"Blast ends orbit try for satellite". Spokane, Washington: The Spokesman-Review. Associated Press. 19 September 1968. p. 1.
  3. ^"Olympic Games Relay Satellite Misfires, Explodes Over Atlantic". Journal and Courier. 19 September 1968. p. 2. Retrieved4 August 2025 – via newspapers.com.
  4. ^Wade, Mark."Delta". Archived fromthe original on 24 July 2008.
  5. ^Krebs, Gunter."Thor Family".Gunter's Space Page.Archived from the original on 6 August 2007. Retrieved21 December 2021.
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  • * - Japanese projects using US rockets or stages
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  • ††† - used Ukrainian first stage
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