United Launch Alliance

Delta IV M

M

Delta IV M
Retired

Overview

/01

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.

Manufacturer

United Launch Alliance

Variant

M

Alias

N/A

Maiden Flight

March 11, 2003

Technical Specifications

/02
63 m

Length

5 m

Diameter

0 t

Launch Mass

2890 kN

Liftoff Thrust

8600 kg

LEO Capacity

3900 kg

GTO Capacity

Launch Record

/03
3

Total Launches

3

Successful

0

Failed

100.0%

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

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