SM-65C Atlas: Difference between revisions
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|name = Atlas C (SM-65C) |
|name = Atlas C (SM-65C) |
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|image = Atlas C.jpg |
|image = Atlas C.jpg |
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|imsize = |
|imsize = 150 |
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|caption = Atlas C awaiting launch (USAF) |
|caption = Atlas C awaiting launch (USAF) |
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|manufacturer = [[Convair]] |
|manufacturer = [[Convair]] |
Revision as of 05:52, 20 February 2013
Function | Prototype ICBM |
---|---|
Manufacturer | Convair |
Country of origin | United States |
Launch history | |
Status | Retired |
Launch sites | LC-12, CCAFS |
Total launches | 6 |
Success(es) | 3 |
Failure(s) | 3 |
First flight | 24 December 1958 |
Last flight | 24 August 1959 |
The SM-65C Atlas, or Atlas C was a prototype of the Atlas missile. First flown on 24 December 1958, the Atlas C was the final development version of the Atlas rocket, prior to the operational Atlas D. It was originally planned to be used as the first stage of the Atlas-Able rocket, but following an explosion during a static test on 24 September 1959, this was abandoned in favour of the Atlas D.
Six flights were made. These were all sub-orbital test flights of the Atlas as an Intercontinental Ballistic Missile, with three tests succeeding, and three failing.[citation needed]
All Atlas C launches were conducted from Cape Canaveral Air Force Station, at Launch Complex 12.[citation needed]
Launch history
Date | Time (GMT) | Serial | Apogee | Outcome |
---|---|---|---|---|
1958-12-24 | 04:45 | 3C | 900 kilometres (560 mi) | Success |
1959-01-27 | 23:34 | 4C | 900 kilometres (560 mi) | Failure |
1959-02-20 | 05:38 | 5C | 100 kilometres (62 mi) | Failure |
1959-03-19 | 00:59 | 7C | 200 kilometres (120 mi) | Failure |
1959-07-21 | 05:22 | 8C | 900 kilometres (560 mi) | Success |
1959-08-24 | 15:53 | 11C | 900 kilometres (560 mi) | Success |