Delta E

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This article is about the rocket. For the difference between colours, see color difference.
Delta E
Delta-E launching Pioneer-6.jpg
Launch of a Delta E with Pioneer 6
Function Expendable launch system
Country of origin  United States
Launch history
Status Retired
Launch sites Cape Canaveral LC-17
Vandenberg SLC-2E
Total launches 23
Successes 23
First flight 6 November 1965
Last flight 1 April 1971

The Delta E, or Thor-Delta E was an American expendable launch system used for twenty-three orbital launches between 1965 and 1971. It was a member of the Delta family of rockets.

The first stage was a Thor missile in the DSV-2C configuration, and the second stage was the Delta E, which was derived from the earlier Delta. Three Castor-1 solid rocket boosters were clustered around the first stage. Two different solid-fuel upper stages were available; an Altair-2 was used on the baseline version, however this could be replaced with an FW-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.

Delta E rockets were launched from Cape Canaveral Air Force Station Launch Complex 17 and Vandenberg Air Force Base Space Launch Complex 2E. All 23 flights were successful.

References[edit]

  • Wade, Mark. "Delta". Encyclopedia Astronautica. Retrieved 2009-02-09. 
  • Krebs, Gunter. "Thor family". Gunter's Space Page. Retrieved 2009-02-09.