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![]() Delta IV Heavy launches from Vandenberg Space Force Base | |
Function | Heavy-lift launch vehicle |
---|---|
Manufacturer | United Launch Alliance |
Country of origin | United States |
Cost per launch | US$350 million [1] NRO: US$440 million |
Size | |
Height | 70.7 m (232 ft) |
Diameter | 5.1 m (17 ft) |
Width | 15.3 m (50 ft) |
Mass | 733,000 kg (1,616,000 lb) |
Associated rockets | |
Family | Delta |
Comparable | |
Launch history | |
Status | Retired |
Launch sites | |
Total launches | 16 |
Success(es) | 15 |
Partial failure(s) | 1 |
First flight | December 21, 2004 (USA-181) |
Last flight | April 9, 2024 (NROL-70) |
Carries passengers or cargo | |
Boosters – CBC | |
No. boosters | 2 |
Height | 40.8 m (134 ft) |
Empty mass | 26,760 kg (59,000 lb) |
Gross mass | 226,400 kg (499,100 lb) |
Propellant mass | 200,400 kg (441,800 lb) [2] |
Powered by | 1 × RS-68 |
Maximum thrust | 3,140 kN (710,000 lbf) |
Total thrust | 6,280 kN (1,410,000 lbf) |
Specific impulse | SL: 360 s (3.5 km/s) vac: 412 s (4.04 km/s) |
Burn time | 246 seconds |
Propellant | LH2 / LOX |
First stage –CBC | |
Height | 40.8 m (134 ft) |
Empty mass | 26,760 kg (59,000 lb) |
Gross mass | 226,400 kg (499,100 lb) |
Propellant mass | 200,400 kg (441,800 lb) [2] |
Powered by | 1 × RS-68 |
Maximum thrust | 3,140 kN (710,000 lbf) |
Specific impulse | SL:360 s (3.5 km/s) vac:412 s (4.04 km/s) |
Burn time | 334 seconds |
Propellant | LH2 / LOX |
Second stage –DCSS | |
Height | 13.7 m (45 ft) |
Empty mass | 3,490 kg (7,690 lb) |
Gross mass | 30,710 kg (67,700 lb) |
Propellant mass | 27,220 kg (60,010 lb) |
Powered by | 1 × RL10-B-2 |
Maximum thrust | 110 kN (25,000 lbf) |
Specific impulse | 465.5 s (4.565 km/s) |
Burn time | 1,125 seconds |
Propellant | LH2 / LOX |
The Delta IV Heavy (Delta 9250H) 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.. [3] [4] [5] 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. [6] [7]
The vehicle consisted of three Common Booster Cores (CBCs),each powered by an RS-68 engine. Two served as strap-on boosters attached to a central core. During ascent,all three engines ignited at liftoff,with the central engine throttling down partway through flight to conserve propellant before throttling up again after booster separation. [8] [9]
A distinctive feature of Delta IV Heavy launches was the hydrogen-fueled ignition sequence,which often produced a large fireball that scorched the booster’s exterior surface. [10]
The Delta IV program was initiated by Boeing under the U.S. Air Force's Evolved Expendable Launch Vehicle program and was transferred to ULA in 2006. The Delta IV Heavy was developed as the most powerful configuration of the family,complementing the smaller Delta IV Medium. [11]
Its maiden flight on December 21,2004 carried a boilerplate payload and ended in partial failure when cavitation in liquid-oxygen lines caused premature shutdown of the engines,leaving the test article in a lower-than-intended orbit. [12] The rocket achieved its first fully successful operational flight in 2007 with the launch of the DSP-23 satellite,and subsequently deployed several reconnaissance satellites for the National Reconnaissance Office (NRO).
The rocket was also used for two notable missions for NASA,Exploration Flight Test-1,the first uncrewed test of the Orion spacecraft in 2014, [13] and the Parker Solar Probe launch in 2018,which required an additional Star 48BV third stage to achieve its elliptical heliocentric orbit. [14]
Production of Delta IV Heavy hardware ended in May 2023, [15] with its last mission flying for the NRO on April 9,2024. [16]
At liftoff,the rocket had a mass of approximately 733,000 kilograms (1,616,000 lb) and generated about 9,420 kilonewtons (2,120,000 lbf) of thrust. [17]
The Delta IV Heavy had the following payload capacities: [18] [19]
Orbit | Payload capacity |
---|---|
LEO [a] | 28,370 kg (62,550 lb) |
LEO-ISS [b] | 25,980 kg (57,280 lb) |
Polar [c] | 23,560 kg (51,940 lb) |
MEO [d] | 8,450 kg (18,630 lb) |
GTO [e] | 14,210 kg (31,330 lb) |
GEO [f] | 6,580 kg (14,510 lb) |
TLI [g] | 11,290 kg (24,890 lb) |
TMI [h] | 8,000 kg (18,000 lb) |
A 20.5-meter-long (67.2 ft) carbon composite bisector payload faring was standard. The Delta IV with the extended fairing was over 62 meters (203 ft) tall.
An aluminum isogrid trisector fairing, derived from a Titan IV fairing, was also available as an option. [20] The trisector fairing was first used on the DSP-23 flight. [21]
Flight | Date | Payload [22] | Mass | Launch site | Outcome [22] |
---|---|---|---|---|---|
1 | December 21, 2004 | DemoSat, Sparkie / 3CS-1 and Ralphie / 3CS-2 | ≈6,000 kg (13,000 lb) | Cape Canaveral, SLC-37B | Partial failure [a] |
2 | November 11, 2007 | DSP-23 | 5,250 kg (11,570 lb) | Cape Canaveral, SLC-37B | Success |
3 | January 18, 2009 | Orion 6 / Mentor 4 (USA-202 / NROL-26) | Classified | Cape Canaveral, SLC-37B | Success |
4 | November 21, 2010 | Orion 7 / Mentor 5 (USA-223 / NROL-32) | Classified | Cape Canaveral, SLC-37B | Success |
5 | January 20, 2011 | KH-11 Kennen 15 (USA-224 / NROL-49) | <17,000 kg (37,000 lb) | Vandenberg, SLC-6 | Success |
6 | June 29, 2012 | Orion 8 / Mentor 6 (USA-237 / NROL-15) | Classified | Cape Canaveral, SLC-37B | Success |
7 | August 26, 2013 | KH-11 Kennen 16 (USA-245 / NROL-65) | <17,000 kg (37,000 lb) | Vandenberg, SLC-6 | Success |
8 | December 5, 2014 | Orion Exploration Flight Test-1 (EFT-1) | 21,000 kg (46,000 lb) [23] [b] | Cape Canaveral, SLC-37B | Success |
9 | June 11, 2016 | Orion 9 / Mentor 7 (USA-268 / NROL-37) | Classified | Cape Canaveral, SLC-37B | Success |
10 | August 12, 2018 | Parker Solar Probe [c] | 685 kg (1,510 lb) | Cape Canaveral, SLC-37B | Success |
11 | January 19, 2019 | NROL-71 | Classified | Vandenberg, SLC-6 | Success |
12 | December 11, 2020 | Orion 10 / Mentor 8 (USA-268/ NROL-44) [24] [25] | Classified | Cape Canaveral, SLC-37B | Success |
13 | April 26, 2021 | KH-11 Kennen 17 (NROL-82) | Classified | Vandenberg, SLC-6 | Success |
14 | September 24, 2022 | KH-11 Kennen 18 (NROL-91) | Classified | Vandenberg, SLC-6 | Success |
15 | June 22, 2023 | Orion 11 / Mentor 9 (NROL-68) [26] | Classified | Cape Canaveral, SLC-37B | Success |
16 | April 9, 2024 | Orion 12 / Mentor 10 (NROL-70) [27] | Classified | Cape Canaveral, SLC-37B | Success |
Current:
Retired or cancelled:
Delta IV Heavy goes for about US$350M. That's current and future, after the retirement of both Delta IV Medium and Delta II.
The Falcon Heavy is capable of lifting 140,000 pounds to low Earth orbit, more than any other rocket today.
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.