Delta·McDonnell Douglas
Delta IV M
retired
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Specifications
- Status
- retired
- Height
- 63 m
- Diameter
- 5 m
- Mass
- 250,000 kg
- Stages
- 2
- Thrust
- 2,890 kN
- Payload to LEO
- 8,600 kg
- Payload to GTO
- 3,900 kg
- First flight
- 2003-03-11
- Total launches
- 3
- Success / Fail
- 3 / 0
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.
Propulsion
First stage
RS-68A3,137 kN
LH2 / LOX · gas-generator
Aerojet RocketdyneIsp 412s (vac)since 2002
Second stage
RL10110 kN
LH2 / LOX · expander
Aerojet RocketdyneIsp 451s (vac)since 1963
Payloads it launched
3 loaded