Delta E

This article is about the rocket. For the difference between colours, see color difference.

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
Success(es)	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

• Wade, Mark. "Delta". Encyclopedia Astronautica. Archived from the original on 2008-07-24. Retrieved 2009-02-09. {{cite web}}: Unknown parameter |deadurl= ignored (|url-status= suggested) (help)
• Krebs, Gunter. "Thor family". Gunter's Space Page. Retrieved 2009-02-09.