Delta IV M
USA Wikipedia 
Built & Operated By
United Launch Alliance
Commercial · founded 2006
Family
Delta
variant M
Maiden Flight
11 MAR 2003
About
Delta IV is a group of five expendable launch systems in the Delta rocket family introduced in the early 2000s. Originally designed by Boeing's Defense, Space & Security division for the Evolved Expendable Launch Vehicle (EELV) program, the Delta IV became a United Launch Alliance (ULA) product in 2006. The Delta IV was and is primarily a launch vehicle for United States Air Force military payloads, but has also been used to launch a number of U.S. government non-military payloads and a single commercial satellite.
Vehicle Specifications
Height
63 m
Diameter
5 m
Launch Mass
250 T
Thrust
2,890 kN
Stages
2
Configuration
Expendable
Launch Record
Total Launches
3
Successful
3
Failed
0
Consecutive
3
Performance
To LEO
8,600 kg
To GTO
3,900 kg
Launch Cost
$164.0M