Space · launch vehicle
Delta IV M
ULA
RETIRED
At a glance
Launches
3
Success rate
100%
3 ok · 0 failed
Payload to LEO
8,600 kg
Payload to GTO
3,900 kg
Manufacturer
United Launch AllianceStatus
RetiredFirst flight
11 Mar 2003Reusable
NoHeight
63 mDiameter
5 mLaunch mass
250 tLiftoff thrust
2,890 kNStages
2Launch cost
$164,000,000Booster landings
—Links
WikipediaAbout
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.
Source The Space Devs — Launch Library 2
Last checked 29 Sept 2026
