SM-65B Atlas
From Wikipedia, the free encyclopedia
| Atlas B (SM-65B) | |
Atlas B before the launch of SCORE (USAF) |
|
| Fact sheet | |
|---|---|
| Function | Prototype ICBM Expendable launch system |
| Manufacturer | Convair |
| Country of origin | |
| Launch History | |
| Status | Retired |
| Launch sites | LC-11, LC-13 & LC-14, CCAFS |
| Total launches | 10 |
| Successes | 6 |
| Failures | 4 |
| Maiden flight | 19 July 1958 |
| Last flight | 4 February 1959 |
The SM-65B Atlas, or Atlas B was a prototype of the Atlas missile. First flown on 19 July 1958, the Atlas B was the first version of the Atlas rocket to use the stage and a half design.
Ten flights were made. Nine of these were sub-orbital test flights of the Atlas as an Intercontinental Ballistic Missile, with five successful missions and four failures. The seventh flight, launched on 18 December 1958, was used to place the SCORE satellite into low Earth orbit, the first orbital launch conducted by an Atlas rocket.
All Atlas-B launches were conducted from Cape Canaveral Air Force Station, at Launch Complexes 11, 13 and 14.
[edit] Launch history
| Date | Time (GMT) | Pad | Serial | Apogee | Outcome | Remarks |
|---|---|---|---|---|---|---|
| 1958-07-19 | 17:36 | LC-11 | 3B | 10 kilometres (6.2 mi) | Failure | |
| 1958-08-02 | 22:16 | LC-13 | 4B | 900 kilometres (560 mi) | Success | |
| 1958-08-29 | 04:30 | LC-11 | 5B | 900 kilometres (560 mi) | Success | |
| 1958-09-14 | 05:24 | LC-14 | 8B | 900 kilometres (560 mi) | Success | |
| 1958-09-18 | 21:27 | LC-13 | 6B | 100 kilometres (62 mi) | Failure | |
| 1958-11-18 | 04:00 | LC-11 | 9B | 800 kilometres (500 mi) | Failure | |
| 1958-11-29 | 02:27 | LC-14 | 12B | 900 kilometres (560 mi) | Success | First full-range test flight |
| 1958-12-18 | 22:02 | LC-11 | 10B | N/A | Success | Placed SCORE satellite into 185km x 1,484km x 32.3° orbit |
| 1959-01-16 | 04:00 | LC-14 | 13B | 100 kilometres (62 mi) | Failure | |
| 1959-02-04 | 08:01 | LC-11 | 11B | 900 kilometres (560 mi) | Success |

