Delta·McDonnell Douglas
Delta IV M+(4,2)
retired
Loading…
Specifications
- Status
- retired
- Height
- 66.2 m
- Diameter
- 5 m
- Mass
- 292,000 kg
- Stages
- 2
- Thrust
- 4,200 kN
- Payload to LEO
- 11,920 kg
- Payload to GTO
- 6,270 kg
- First flight
- 2002-11-20
- Total launches
- 15
- Success / Fail
- 15 / 0
The Delta IV Heavy was an expendable heavy-lift launch vehicle, the largest member of the Delta IV family. Following the retirement of the Space Shuttle in 2011, it was the most capable operational launch vehicle until the Falcon Heavy's debut in 2018. At the time of its retirement in 2024, it ranked third among active rockets in payload capacity. Developed by Boeing and later manufactured by United Launch Alliance (ULA), it first flew in 2004. The Delta IV Heavy was retired after its 16th and final launch on 9 April 2024 and was succeeded by ULA's Vulcan Centaur rocket, which can offer similar heavy-lift capabilities at a lower cost with a single-core and six solid rocket boosters.
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
18 loaded
GPS BIII-2 (PRN 18)
GPS · MEO
USA 270
GEO
USA 271
GEO
GPS BIIF-9 (PRN 26)
GPS · MEO
USA 255
GEO
USA 253
GEO
USA 254
GEO
GPS BIIF-6 (PRN 06)
GPS · MEO
GPS BIIF-5 (PRN 30)
GPS · MEO
GPS BIIF-3 (PRN 24)
GPS · MEO
NAVSTAR 66 (USA 232)
MEO
USA 227
GEO
GPS BIIF-1 (PRN 25)
GPS · MEO
EWS-G2 (GOES 15)
GEO
EWS-G3 (GOES 14)
GEO
USA 184
HEO
EWS-G1 (GOES 13)
GEO
EUTELSAT 33B
GEO