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Retired

Delta IV M

Delta IV M

🏭 United Launch Alliance🌐 American📖 Wikipedia
Delta IV M

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.

8.6 t
LEO Capacity
63 m
Height
3
Total Launches
100.0%
Success Rate

📷 Photo Gallery

Delta IV M photo 1

📊 Specifications

📏Height
63 m
⭕Diameter
5 m
⚖️Launch Mass
250 kg
🛰️LEO Capacity
8,600 kg
🌍GTO Capacity
3,900 kg
🗓️Maiden Flight
Mar 11, 2003
🚀Total Launches
3
✅Success Rate
100%
♻️Reusable
Expendable
🏭Manufacturer
United Launch Alliance
🌐Country
American
📋Status
Retired