Atlas I
USA Wikipedia 
Built & Operated By
General Dynamics
Commercial
Family
Atlas
variant I
Maiden Flight
25 JUL 1990
About
The Atlas I was a US expendable launch system manufactured by General Dynamics in the 1990s to launch a variety of satellites.
Vehicle Specifications
Height
43.9 m
Diameter
3.05 m
Launch Mass
164 T
Thrust
1,939 kN
Stages
2
Configuration
Expendable
Launch Record
Total Launches
11
Successful
9
Failed
2
Consecutive
7
Performance
To LEO
5,900 kg