Delta·McDonnell Douglas
Delta IV Heavy
retired
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Specifications
- Status
- retired
- Height
- 72 m
- Diameter
- 5 m
- Mass
- 733,000 kg
- Stages
- 2
- Thrust
- 8,674 kN
- Payload to LEO
- 28,370 kg
- Payload to GTO
- 14,210 kg
- First flight
- 2004-12-21
- Total launches
- 16
- Success / Fail
- 15 / 1
The Delta IV Heavy (Delta 9250H) is an expendable heavy-lift launch vehicle, the largest type of the Delta IV family, and is the world's second highest-capacity rocket in operation. It is manufactured by United Launch Alliance and was first launched in 2004.
Propulsion
First stage
3×RS-68A3,137 kN
LH2 / LOX · gas-generator
Aerojet RocketdyneIsp 412s (vac)since 2002three CBC cores
Second stage
RL10110 kN
LH2 / LOX · expander
Aerojet RocketdyneIsp 451s (vac)since 1963
Payloads it launched
16 loaded