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Delta A
American expendable launch vehicle
American expendable launch vehicle
| Field | Value | |
|---|---|---|
| image | [[File:Thor Delta A with Explorer 14 (Oct. 2, 1962).gif | 300px]] |
| caption | Delta A launching Explorer 14 | |
| function | Expendable launch system | |
| country-origin | United States | |
| sites | Cape Canaveral LC-17 | |
| launches | 2 | |
| success | 2 | |
| status | Retired | |
| first | 2 October 1962 | |
| last | 27 October 1962 |
| country-origin = United States
The Delta A, or Thor-Delta A was an American expendable launch system used to launch two Explorer spacecraft in October 1962. A derivative of the Thor-Delta, it was a member of the Delta family of launch vehicles. The Thor-Delta itself was a Thor booster with an Able second stage and Altair third stage.
The first stage was a Thor missile in the DM-21 configuration, and the second stage was the Delta-A, an uprated version of the original Delta. An Altair solid rocket motor was used as a third stage. Both launches occurred from Cape Canaveral Air Force Station (CCAFS) Launch Complex 17B, and were successful. The first launched Explorer 14, and the second Explorer 15.
References
References
- Wade, Mark. "Delta". Encyclopedia Astronautica.
- Krebs, Gunter. "Thor family". Gunter's Space Page.
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