Atlas V 521
USA Wikipedia 
Built & Operated By
United Launch Alliance
Commercial · founded 2006
Family
Atlas
variant 521
Maiden Flight
17 JUL 2003
About
Atlas V is the fifth major version in the Atlas rocket family. It is an expendable launch system originally designed by Lockheed Martin, now being operated by United Launch Alliance (ULA), a joint venture between Lockheed and Boeing.
Vehicle Specifications
Height
58.3 m
Diameter
3.81 m
Launch Mass
590 T
Thrust
7,203 kN
Stages
2
Configuration
Expendable
Launch Record
Total Launches
2
Successful
2
Failed
0
Consecutive
2
Performance
To LEO
13,490 kg
To GTO
6,475 kg
Launch Cost
$135.0M