SM-65B Atlas Vehicle Overview
A complete overview of the SM-65B Atlas launch vehicle, including launch stats, vehicle info and launch locations.
Basic Info
Name
SM-65B Atlas
Family
Atlas
Manufacturer
First Launch
19 Jul 1958
Successful Launches
1
Failed Launches
0
Rocket Info
Status
Inactive
Stages
1
Length
31.4 m
Diameter
3.66 m
Launch Mass
3 tons
Reusability
Not Reusable
Payload Info
LEO Capacity
68 kg
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.
Launch Sites used by SM-65B Atlas
Cape Canaveral Space Force Station
Historic U.S. military rocket launch site, pivotal in space exploration and national security.