Delta IV
Riwayat Peluncuran Roket Delta IV

| No>  | Date/Time (UTC) | Type | Serial-no>  | Startplace | Payload | Type of payload | Orbit | Outcome | Remarks |
| --- | --- | --- | --- | --- | --- | --- | --- | --- | --- |
| 1 | 2002-11-20 22:39 | Medium+(4,2) | 293 | CCAFS SLC-37B | Eutelsat W5 | Commercial communications satellite | GTO | Success | First Delta IV launch |
| 2 | 2003-03-11 00:59 | Medium | 296 | CCAFS SLC-37B | USA-167 (DSCS-3 A3) | Military communications satellite | GTO | Success | First Delta IV Medium launch First USAF EELV mission |
| 3 | 2003-08-29 23:13 | Medium | 301 | CCAFS SLC-37B | USA-170 (DSCS-3 B6) | Military communications satellite | GTO | Success |  |
| 4 | 2004-12-21 21:50 | Heavy | 310 | CCAFS SLC-37B | DemoSat / 3CS-1 / 3CS-2 | Demonstration payload | GSO (planned) | Partial failure |  First Delta IV Heavy launch  Premature cutoff of CBCs  DemoSat reached incorrect orbit, 3CS failed to reach orbit |
| 5 | 2006-05-24 22:11 | Medium+(4,2) | 315 | CCAFS SLC-37B | GOES 13 (GOES-N) | Weather satellite | GTO | Success |  |
| 6 | 2006-06-28 03:33 | Medium+(4,2) | 317 | VAFB SLC-6 | USA-184 (NROL-22) | Reconnaissance satellite | Molniya | Success | First Delta IV launch from Vandenberg |
| 7 | 2006-11-04 13:53 | Medium | 320 | VAFB SLC-6 | USA-192 (DMSP F17) | Military weather satellite | SSO | Success | First Delta IV launch into a LEO/SSO |
| 8 | 2007-11-11 01:50 | Heavy | 329 | CCAFS SLC-37B | USA-197 (DSP-23) | Missile Warning satellite | GSO | Success | First Delta IV launch contracted by United Launch Alliance Launch delayed due to damage to launch pad caused by a liquid oxygen leak |
| 9 | 2009-01-18 02:47 | Heavy | 337 | CCAFS SLC-37B | USA-202 (NROL-26) | Reconnaissance satellite | GSO | Success |  |
| 10 | 2009-06-27 22:51 | Medium+(4,2) | 342 | CCAFS SLC-37B | GOES 14 (GOES-O) | Weather satellite | GTO | Success |  |
| 11 | 2009-12-06 01:47 | Medium+(5,4) | 346 | CCAFS SLC-37B | USA-211 (WGS-3) | Military communications satellite | GTO | Success | First Delta IV Medium+ (5,4) launch |
| 12 | 2010-03-04 23:57 | Medium+(4,2) | 348 | CCAFS SLC-37B | GOES 15 (GOES-P) | Weather satellite | GTO | Success |  |
| 13 | 2010-05-28 03:00 | Medium+(4,2) | 349 | CCAFS SLC-37B | USA-213 (GPS IIF SV-1) | Navigation Satellite | MEO | Success |  |
| 14 | 2010-11-21 22:58 | Heavy | 351 | CCAFS SLC-37B | USA-223 (NROL-32) | Reconnaissance satellite | GSO | Success |  |
| 15 | 2011-01-20 21:10 | Heavy | 352 | VAFB SLC-6 | USA-224 (NROL-49) | Reconnaissance satellite | LEO | Success | First Delta IV Heavy launch from Vandenberg |
| 16 | 2011-03-11 23:38 | Medium+(4,2) | 353 | CCAFS SLC-37B | USA-227 (NROL-27) | Reconnaissance satellite | GTO | Success |  |
| 17 | 2011-07-16 06:41 | Medium+(4,2) | 355 | CCAFS SLC-37B | USA-231 (GPS IIF SV-2) | Navigation Satellite | MEO | Success |  |
| 18 | 2012-01-20 00:38 | Medium+(5,4) | 358 | CCAFS SLC-37B | USA-233 (WGS-4) | Military communications satellite | GTO | Success |  |
| 19 | 2012-04-03 23:12 | Medium+(5,2) | 359 | VAFB SLC-6 | USA-234 (NROL-25) | Reconnaissance satellite | LEO | Success | First flight in the Medium+(5,2) version |
| 20 | 2012-06-29 13:15 | Heavy | 360 | CCAFS SLC-37B | USA-237 (NROL-15) | Reconnaissance satellite | GSO | Success | First flight of the RS-68A engine |
| 21 | 2012-10-04 12:10 | Medium+(4,2) | 361 | CCAFS SLC-37B | USA-239 (GPS IIF SV-3) | Navigation Satellite | MEO | Success | Minor upper stage anomaly |
| 22 | 2013-05-25 00:27 | Medium+(5,4) | 362 | CCAFS SLC-37B | USA-243 (WGS-5) | Military communications satellite | GTO | Success |  |
| 23 | 2013-08-08 00:29 | Medium+(5,4) | 363 | CCAFS SLC-37B | USA-244 (WGS-6) | Military communications satellite | GTO | Success |  |
| 24 | 2013-08-28 18:03 | Heavy | 364 | VAFB SLC-6 | USA-245 (NROL-65) | Reconnaissance satellite | LEO | Success |  |
List Date: August 28, 2013
Evolusi Delta IV
Delta IV 4-meter Kriogenik Tahap Kedua
Roket Delta IV yang terbang dalam konfigurasi Medium dan Medium+ masing-masing menggunakan satu Common Booster Core sebagai tahap pertama, sedangkan konfigurasi Heavy menggunakan tiga; satu sebagai tahap pertama dan dua sebagai pendorong