SM-65B Atlas (Convair)
The SM-65B Atlas is a non-reusable, inactive launch vehicle manufactured by Convair (established in 1943). It undertook its inaugural launch on 07/19/1958.
The Convair SM-65B Atlas, or Atlas B, also designated X-12 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 with an operational sustainer engine and jettisonable rocket booster section. Unlike later Atlas models, the Atlas B used explosive bolts to jettison the booster section.
SM-65B Atlas Specifications
| Variant | B |
|---|---|
| Length | 31.4 m |
| Diameter | 3.66 m |
| Stages | 1 |
| Launch Mass | 3 T |
| LEO Capacity | 68 kg |
SM-65B Atlas Launch Record
| Total Launches | 1 |
|---|---|
| Successful Launches | 1 |
| Consecutive Successful Launches | 1 |
Manufacturer
Convair, previously Consolidated Vultee, was an American aircraft manufacturing company that later expanded into rockets and spacecraft. The company was formed in 1943 by the merger of Consolidated Aircraft and Vultee Aircraft. In 1953 it was purchased by General Dynamics, and operated as their Convair Division for most of its corporate history.