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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