Delta IV Heavy

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Delta IV Heavy
Delta logo.png
NROL-71 Wide (cropped alt).jpg
Delta IV Heavy launches from Vandenberg Space Force Base
FunctionOrbital heavy-lift launch vehicle
Manufacturer United Launch Alliance
Country of originUnited States
Cost per launchUS$350 million [1]
NRO: US$440 million
Size
Height70.7 m (232 ft)
Diameter5.1 m (17 ft)
Width15.3 m (50 ft)
Mass733,000 kg (1,616,000 lb)
Stages2+
Capacity
Payload to LEO
Mass28,790 kg (63,470 lb)
Launch history
StatusRetired
Launch sites
Total launches16
Success(es)15
Partial failure(s)1
First flight21 December 2004 (USA-181)
Last flight9 April 2024 (NROL-70)
Type of passengers/cargo
Boosters (CBC)
No. boosters2
Height40.8 m (134 ft)
Diameter5.1 m (17 ft)
Empty mass26,000 kg (57,000 lb)
Gross mass226,400 kg (499,100 lb)
Propellant mass200,400 kg (441,800 lb) [2]
Powered by1 RS-68A
Maximum thrust3,140 kN (710,000 lbf)
Total thrust6,280 kN (1,410,000 lbf)
Specific impulse Sea level: 360 s (3.5 km/s)
Vacuum: 412 s (4.04 km/s)
Burn time242 seconds [3]
Propellant LH2 / LOX
FlightDatePayload [27] MassLaunch siteOutcome [27]
121 December 2004 DemoSat, Sparkie / 3CS-1 and Ralphie / 3CS-2 6,000 kg (13,000 lb) Cape Canaveral, SLC-37B Partial failure [a]
211 November 2007 DSP-23 5,250 kg (11,570 lb) Cape Canaveral, SLC-37B Success
318 January 2009 Orion 6 / Mentor 4 (USA-202 / NROL-26)Classified Cape Canaveral, SLC-37B Success
421 November 2010Orion 7 / Mentor 5 (USA-223 / NROL-32)Classified Cape Canaveral, SLC-37B Success
520 January 2011 KH-11 Kennen 15 (USA-224 / NROL-49)<17,000 kg (37,000 lb) Vandenberg, SLC-6 Success
629 June 2012Orion 8 / Mentor 6 (USA-237 / NROL-15)Classified Cape Canaveral, SLC-37B Success
726 August 2013KH-11 Kennen 16 (USA-245 / NROL-65)<17,000 kg (37,000 lb) Vandenberg, SLC-6 Success
85 December 2014 Orion Exploration Flight Test-1 (EFT-1)21,000 kg (46,000 lb) [28] [b] Cape Canaveral, SLC-37B Success
911 June 2016Orion 9 / Mentor 7 (USA-268 / NROL-37)Classified Cape Canaveral, SLC-37B Success
1012 August 2018 Parker Solar Probe [c] 685 kg (1,510 lb) Cape Canaveral, SLC-37B Success
1119 January 2019 NROL-71 Classified Vandenberg, SLC-6 Success
1211 December 2020Orion 10 / Mentor 8 (USA-268/ NROL-44) [29] [30] Classified Cape Canaveral, SLC-37B Success
1326 April 2021 KH-11 Kennen 17 (NROL-82)Classified Vandenberg, SLC-6 Success
1424 September 2022 KH-11 Kennen 18 (NROL-91)Classified Vandenberg, SLC-6 Success
1522 June 2023 Orion 11 / Mentor 9 (NROL-68) [31] Classified Cape Canaveral, SLC-37B Success
169 April 2024 Orion 12 / Mentor 10 (NROL-70) [32] Classified CCSFS, SLC-37B Success
  1. Common Booster Cores underperformed, lower orbit than planned
  2. The officially reported mass of 21,000 kg includes the Launch Abort System (LAS) which did not reach orbit, but excludes the residual mass of the upper stage, which did reach orbit, likely offsetting the mass of the LAS.
  3. Star 48BV upper stage

Comparable vehicles

Current:

In development:

Retired or cancelled:

See also

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References

  1. "ULA CEO Tory Bruno". twitter.com. Retrieved 12 February 2018. Delta IV Heavy goes for about US$350M. That's current and future, after the retirement of both Delta IV Medium and Delta II.
  2. "Delta IV Heavy". Spaceflight 101. Retrieved 26 July 2014.
  3. 1 2 "Delta IV Payload Planner's Guide, June 2013" (PDF). United Launch Alliance. Archived from the original (PDF) on 10 July 2014. Retrieved 26 July 2014.
  4. "Delta IV Launch Services User's Guide" (PDF). United Launch Alliance. Retrieved 13 April 2024.
  5. Clark, Stephen. "The Delta IV Heavy, a rocket whose time has come and gone, will fly once more". ars Technica. Retrieved 9 November 2024.
  6. Chang, Kenneth (6 February 2018). "Falcon Heavy, SpaceX's Big New Rocket, Succeeds in Its First Test Launch". The New York Times. Retrieved 6 February 2018. The Falcon Heavy is capable of lifting 140,000 pounds to low Earth orbit, more than any other rocket today.
  7. "Mission Status Center". Spaceflight Now. Retrieved 26 July 2014. The ULA Delta 4-Heavy is currently the world's largest rocket, providing the nation with reliable, proven, heavy lift capability for our country's national security payloads from both the east and west coasts.
  8. "Boeing Delta IV Heavy Achieves Major Test Objectives in First Flight" (Press release). Boeing. 21 December 2004. Archived from the original on 19 April 2012. Retrieved 22 March 2012.
  9. Erwin, Sandra (24 August 2020). "ULA to launch Delta 4 Heavy for its 12th mission, four more to go before rocket is retired". SpaceNews. Retrieved 29 August 2020.
  10. "Delta IV Heavy - NROL-70". Next Spaceflight. 9 February 2024. Retrieved 10 February 2024.
  11. "Delta 4-Heavy likely heading for geosynchronous orbit with top secret payload". Spaceflight Now. 26 August 2020. Retrieved 27 August 2020.
  12. Berger, Eric (21 January 2019). "This massive rocket creates a fireball as it launches, and that's by design". Ars Technica. Retrieved 13 April 2023.
  13. 1 2 3 Howell, Elizabeth (20 April 2018). "Delta IV Heavy: Powerful Launch Vehicle". Space.com. Retrieved 21 July 2018.
  14. "Delta 4-Heavy investigation identifies rocket's problem". Spaceflight Now. 16 March 2005. Retrieved 26 July 2014.
  15. "Second Stage Ignites as First Stage Falls Away". 5 December 2014.PD-icon.svg This article incorporates text from this source, which is in the public domain .
  16. "Delta IV Parker Solar Probe". ulalaunch.com. Retrieved 11 December 2020.
  17. "ULA's Delta rocket assembly line falls silent". Spaceflight Now.
  18. 1 2 "Delta IV Heavy NROL-70". www.ulalaunch.com. Retrieved 8 April 2024.
  19. Chang, Kenneth (28 March 2024). "A Fiery Finale for a Rocket That Brings the Heat - The Delta IV Heavy, a rocket that briefly bursts into flame just before it lifts off, is set to launch for the last time soon". The New York Times . Archived from the original on 28 March 2024. Retrieved 29 March 2024.
  20. Angle, Richard (15 March 2024). "United Launch Alliance's Delta IV Heavy readies for final flight". TESLARATI. Retrieved 21 March 2024.
  21. Pare, Sascha (28 March 2024). "Secretive Delta IV Heavy rocket launch postponed indefinitely". livescience.com. Retrieved 30 March 2024.
  22. Robert Z. Pearlman (9 April 2024). "'Heavy' history: ULA launches final Delta rocket after 64 years (video, photos)". Space.com. Retrieved 11 April 2024.
  23. 1 2 3 "Delta IV Launch Services User's Guide – June 2013" (PDF). United Launch Alliance. 4 June 2013. pp. 2–10, 5–3. Archived from the original (PDF) on 14 October 2013. Retrieved 31 October 2020.
  24. "Delta IV Data Sheet". Space Launch Report. Archived from the original on 6 December 2012. Retrieved 26 July 2014.{{cite web}}: CS1 maint: unfit URL (link)
  25. Ray, Justin (7 December 2004). "The Heavy: Triple-sized Delta 4 rocket to debut". Spaceflight Now. Archived from the original on 11 December 2004. Retrieved 13 May 2014.
  26. "Live coverage: Launch of Delta 4-Heavy rocket set for early Saturday". Spaceflight Now. 29 August 2020. Retrieved 29 August 2020.
  27. 1 2 Krebs, Gunter. "Delta-4". Gunter's Space Page. Retrieved 15 March 2018.
  28. "NASA Orion Exploration Flight Test-1 PRESS KIT" (PDF). NASA. December 2014. p. 12.PD-icon.svg This article incorporates text from this source, which is in the public domain.
  29. "Launch Schedule". Spaceflight Now. 27 October 2020. Retrieved 31 October 2020.
  30. "Launch Mission Execution Forecast". 45th Weather Squadron - Patrick Air Force Base. 30 October 2020. Retrieved 31 October 2020.PD-icon.svg This article incorporates text from this source, which is in the public domain.
  31. Clark, Stephen (22 June 2023). "Delta 4-Heavy rocket lifts off with NRO spy satellite". Spaceflight Now. Retrieved 27 June 2023.
  32. Graham, William (9 April 2024). "Delta IV Heavy launches on final mission". NASASpaceFlight.com. Retrieved 28 September 2024.