Delta IV M
United Launch Alliance
Details
Height
63 m
Diameter
5 m
GTO
3,900 kg
LEO
8,600 kg
Thrust at Liftoff
2,890 kN
Apogee
Unknown
Launch Cost
$164M
Maiden Flight
March 11, 2003
Description
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.