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UNITED LAUNCH ALLIANCE

Delta IV M

3FLIGHTS
100%SUCCESS
3STREAK
Mar 2003FIRST FLIGHT
NOREUSABLE
HEIGHT63 m
DIAMETER5 m
LAUNCH MASS250 kg
LIFTOFF THRUST2,890 kN
STAGES2

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.

8,600 kg
TO LEO
18,963 lbs
3,900 kg
TO GTO
8,600 lbs
2,890
KILONEWTONS
649,698
POUNDS-FORCE
~3,876
HORSEPOWER
Height63 m (207 ft)
Diameter5 m (16.4 ft)
Launch Mass250 kg (551 lbs)
Stages2
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