Function | Orbital 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) |
Stages | 2+ |
Capacity | |
Payload to LEO | |
Mass | 28,790 kg (63,470 lb) |
Payload to GEO | |
Mass | 6,750 kg (14,880 lb) |
Associated rockets | |
Family | Delta |
Comparable | |
Launch history | |
Status | Retired |
Launch sites | |
Total launches | 16 |
Success(es) | 15 |
Partial failure(s) | 1 |
First flight | 21 December 2004 (USA-181) |
Last flight | 9 April 2024 (NROL-70) |
Type of passengers/cargo | |
Boosters (CBC) | |
No. boosters | 2 |
Height | 40.8 m (134 ft) |
Diameter | 5.1 m (17 ft) |
Empty mass | 26,000 kg (57,000 lb) |
Gross mass | 226,400 kg (499,100 lb) |
Propellant mass | 200,400 kg (441,800 lb) [2] |
Powered by | 1 RS-68A |
Maximum thrust | 3,140 kN (710,000 lbf) |
Total thrust | 6,280 kN (1,410,000 lbf) |
Specific impulse | Sea level: 360 s (3.5 km/s) Vacuum: 412 s (4.04 km/s) |
Burn time | 242 seconds [3] |
Propellant | LH2 / LOX |
First stage (CBC) | |
Height | 40.8 m (134 ft) |
Diameter | 5.1 m (17 ft) |
Gross mass | 226,400 kg (499,100 lb) |
Propellant mass | 200,400 kg (441,800 lb) |
Powered by | 1 RS-68A |
Maximum thrust | 3,140 kN (710,000 lbf) |
Specific impulse | Sea level: 360 s (3.5 km/s) Vacuum: 412 s (4.04 km/s) |
Burn time | 328 seconds |
Propellant | LH2 / LOX |
Second stage (DCSS) | |
Height | 13.7 m (45 ft) |
Diameter | 5.1 m (17 ft) (LH2 tank) 3.2 m (10 ft) (LOX tank) [4] |
Gross mass | 30,700 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 | 1125 seconds |
Propellant | LH2 / LOX |
The Delta IV Heavy (Delta 9250H) was an expendable heavy-lift launch vehicle,the largest type of the Delta IV family. It had the highest capacity of any operational launch vehicle in the world after the retirement of the Space Shuttle in 2011 until the Falcon Heavy debuted in 2018,and it was the world's third highest-capacity launch vehicle in operation at the time of its retirement in 2024. [5] [6] [7] It was manufactured by United Launch Alliance (ULA) and was first launched in 2004. [8] Delta IV Heavy was the last operating member of the Delta IV family,and its final flight was on 9 April 2024. It is succeeded by the Vulcan Centaur rocket. [9] [10]
The Delta IV Heavy first stage consisted of a central Common Booster Core (CBC),with two additional CBCs as liquid rocket boosters instead of the GEM-60 solid rocket motors used by the Delta IV Medium+ versions. At lift-off,all three rocket engines would operate at full thrust,and 44 seconds later the central engine would throttle down to 55% to conserve fuel until the other two engines separate. The latter engines burn out at 242 seconds after launch and are separated as the central engine throttles back up to full thrust. The central engine burns out 86 seconds later,and the second stage completed the ascent to orbit. [3]
The launch vehicle used three RS-68 engines,one in the central core and one in each booster. [11] On the last seconds of countdown,the liquid hydrogen fuel would flow through the engines and upwards along the booster body,and after the ignition that hydrogen inflamed,creating the characteristic fireball and charred look of the booster. [12]
The Delta IV line of rockets were developed by Boeing. The program was later transferred to United Launch Alliance. The Delta IV Heavy was the most powerful member of the line,which also includes the smaller Delta IV Medium. [13] The Delta IV Heavy can lift 28,370 kg (62,550 lb) to low Earth orbit and 13,810 kg (30,450 lb) to geostationary transfer orbit (GTO). [13] It was an all liquid-fueled launch vehicle,consisting of an upper stage,one main booster and two strap-on boosters. [13]
The first launch of the Delta IV Heavy on 21 December 2004 carried a boilerplate payload and was a partial failure. Cavitation in the liquid-oxygen propellant lines caused shutdown of both boosters eight seconds early,and the core engine nine seconds early;this resulted in a lower staging velocity for which the second stage was unable to compensate. The payload was left in a lower than intended orbit. [14]
Its first operational payload was the DSP-23 satellite,successfully launched in 2007;it was then used to launch a further five visual and electronic reconnaissance satellites for the National Reconnaissance Office (NRO) through 2013. In December 2014,the Delta IV Heavy was used to launch an uncrewed test flight of the Orion spacecraft,designated Exploration Flight Test-1 (EFT-1). After several delays,the mission was successfully launched at 12:05 UTC on 5 December 2014. [15]
On 12 August 2018,the Delta IV Heavy with an additional Star 48BV third stage was used to launch the Parker Solar Probe into an elliptical heliocentric orbit. [16] In May 2023,the final Delta IV Heavy core and boosters finished construction,officially ending Delta IV production and making way for the Vulcan launch vehicle. [17] The final Delta IV heavy would launch on April 9,2024. [18]
Delta IV's final flight was initially scheduled for March 29,2024 for the National Reconnaissance Office; [19] [20] its actual launch date was April 9,2024 after a postponement. [21] [18] [22]
Capacity of the Delta IV Heavy:
The Delta IV Heavy's total mass at launch was approximately 733,000 kg (1,616,000 lb) and produce around 952,000 kg (2,099,000 lb) of thrust to power the rocket skyward at liftoff. [26]
Flight | Date | Payload [27] | Mass | Launch site | Outcome [27] |
---|---|---|---|---|---|
1 | 21 December 2004 | DemoSat, Sparkie / 3CS-1 and Ralphie / 3CS-2 | ≈6,000 kg (13,000 lb) | Cape Canaveral, SLC-37B | Partial failure [a] |
2 | 11 November 2007 | DSP-23 | 5,250 kg (11,570 lb) | Cape Canaveral, SLC-37B | Success |
3 | 18 January 2009 | Orion 6 / Mentor 4 (USA-202 / NROL-26) | Classified | Cape Canaveral, SLC-37B | Success |
4 | 21 November 2010 | Orion 7 / Mentor 5 (USA-223 / NROL-32) | Classified | Cape Canaveral, SLC-37B | Success |
5 | 20 January 2011 | KH-11 Kennen 15 (USA-224 / NROL-49) | <17,000 kg (37,000 lb) | Vandenberg, SLC-6 | Success |
6 | 29 June 2012 | Orion 8 / Mentor 6 (USA-237 / NROL-15) | Classified | Cape Canaveral, SLC-37B | Success |
7 | 26 August 2013 | KH-11 Kennen 16 (USA-245 / NROL-65) | <17,000 kg (37,000 lb) | Vandenberg, SLC-6 | Success |
8 | 5 December 2014 | Orion Exploration Flight Test-1 (EFT-1) | 21,000 kg (46,000 lb) [28] [b] | Cape Canaveral, SLC-37B | Success |
9 | 11 June 2016 | Orion 9 / Mentor 7 (USA-268 / NROL-37) | Classified | Cape Canaveral, SLC-37B | Success |
10 | 12 August 2018 | Parker Solar Probe [c] | 685 kg (1,510 lb) | Cape Canaveral, SLC-37B | Success |
11 | 19 January 2019 | NROL-71 | Classified | Vandenberg, SLC-6 | Success |
12 | 11 December 2020 | Orion 10 / Mentor 8 (USA-268/ NROL-44) [29] [30] | Classified | Cape Canaveral, SLC-37B | Success |
13 | 26 April 2021 | KH-11 Kennen 17 (NROL-82) | Classified | Vandenberg, SLC-6 | Success |
14 | 24 September 2022 | KH-11 Kennen 18 (NROL-91) | Classified | Vandenberg, SLC-6 | Success |
15 | 22 June 2023 | Orion 11 / Mentor 9 (NROL-68) [31] | Classified | Cape Canaveral, SLC-37B | Success |
16 | 9 April 2024 | Orion 12 / Mentor 10 (NROL-70) [32] | Classified | CCSFS, SLC-37B | Success |
Current:
In development:
Retired or cancelled:
Ariane 5 is a retired European heavy-lift space launch vehicle operated by Arianespace for the European Space Agency (ESA). It was launched from the Guiana Space Centre (CSG) in French Guiana. It was used to deliver payloads into geostationary transfer orbit (GTO), low Earth orbit (LEO) or further into space. The launch vehicle had a streak of 82 consecutive successful launches between 9 April 2003 and 12 December 2017. Since 2014, Ariane 6, a direct successor system, first launched in 2024.
The Centaur is a family of rocket propelled upper stages that has been in use since 1962. It is currently produced by U.S. launch service provider United Launch Alliance, with one main active version and one version under development. The 3.05 m (10.0 ft) diameter Common Centaur/Centaur III flies as the upper stage of the Atlas V launch vehicle, and the 5.4 m (18 ft) diameter Centaur V has been developed as the upper stage of ULA's new Vulcan rocket. Centaur was the first rocket stage to use liquid hydrogen (LH2) and liquid oxygen (LOX) propellants, a high-energy combination that is ideal for upper stages but has significant handling difficulties.
Delta II was an expendable launch system, originally designed and built by McDonnell Douglas, and sometimes known as the Thorad Delta 1. Delta II was part of the Delta rocket family, derived directly from the Delta 3000, and entered service in 1989. There were two main variants, the Delta 6000 and Delta 7000, with the latter also having "Light" and "Heavy" subvariants. During its career, Delta II flew several notable payloads, including 24 Global Positioning System (GPS) Block II satellites, several dozen NASA payloads, and 60 Iridium communication satellites. The rocket flew its final mission, ICESat-2, on 15 September 2018, earning the launch vehicle a streak of 100 successful missions in a row, with the last failure being GPS IIR-1 in 1997. In the late 1990s, Delta II was developed further into the unsuccessful Delta III, which was in turn developed into the more capable and successful Delta IV, though the latter shares little heritage with the original Thor and Delta rockets.
The Delta rocket family was a versatile range of American rocket-powered expendable launch systems that provided space launch capability in the United States from 1960 to 2024. Japan also launched license-built derivatives from 1975 to 1992. More than 300 Delta rockets were launched with a 95% success rate. The series was phased out in favor of the Vulcan Centaur, with the Delta IV Heavy rocket's last launch occurring on April 9, 2024.
Delta IV was a group of five expendable launch systems in the Delta rocket family. It flew 45 missions from 2002 to 2024. Originally designed by Boeing's Defense, Space and Security division for the Evolved Expendable Launch Vehicle (EELV) program, the Delta IV became a United Launch Alliance (ULA) product in 2006. The Delta IV was primarily a launch vehicle for United States Air Force (USAF) military payloads, but was also used to launch a number of United States government non-military payloads and a single commercial satellite.
Atlas II was a member of the Atlas family of launch vehicles, which evolved from the successful Atlas missile program of the 1950s. The Atlas II was a direct evolution of the Atlas I, featuring longer first-stage tanks, higher-performing engines, and the option for strap-on solid rocket boosters. It was designed to launch payloads into low Earth orbit, geosynchronous transfer orbit or geosynchronous orbit. Sixty-three launches of the Atlas II, IIA and IIAS models were carried out between 1991 and 2004; all sixty-three launches were successes, making the Atlas II a highly reliable space launch system. The Atlas line was continued by the Atlas III, used between 2000 and 2005, and the Atlas V, which is still in use as of 2024.
The Angara rocket family is a family of launch vehicles being developed by the Moscow-based Khrunichev State Research and Production Space Center. The launch vehicles are to put between 3,800 kg (8,400 lb) and 24,500 kg (54,000 lb) into low Earth orbit and are intended, along with Soyuz-2 variants, to replace several existing launch vehicles.
A launch vehicle is typically a rocket-powered vehicle designed to carry a payload from Earth's surface or lower atmosphere to outer space. The most common form is the ballistic missile-shaped multistage rocket, but the term is more general and also encompasses vehicles like the Space Shuttle. Most launch vehicles operate from a launch pad, supported by a launch control center and systems such as vehicle assembly and fueling. Launch vehicles are engineered with advanced aerodynamics and technologies, which contribute to high operating costs.
Atlas V is an expendable launch system and the fifth major version in the Atlas launch vehicle family. It was designed by Lockheed Martin and has been operated by United Launch Alliance (ULA) since 2006. It is used for DoD, NASA, and commercial payloads. It is America's longest-serving active rocket. After 87 launches, in August 2021 ULA announced that Atlas V would be retired, and all 29 remaining launches had been sold. As of July 2024, 15 launches remain. Production ceased in 2024. Other future ULA launches will use the Vulcan Centaur rocket.
United Launch Alliance, LLC (ULA) is an American launch service provider formed in December 2006 as a joint venture between Lockheed Martin Space and Boeing Defense, Space & Security. The company designs, assembles, sells and launches rockets, but the company subcontracts out the production of rocket engines and solid rocket boosters.
The Atlas III was an American orbital launch vehicle, used in the years between 2000 and 2005. It was developed from the highly successful Atlas II rocket and shared many components. It was the first member of the Atlas family since the Atlas A to feature a "normal" staging method, compared to the previous Atlas family members, which were equipped with two jettisonable outboard engines on the first (booster) stage. The Atlas III was developed further to create the Atlas V.
The Long March 3B, also known as the CZ-3B and LM-3B, is a Chinese orbital launch vehicle. Introduced in 1996, it is launched from Launch Area 2 and 3 at the Xichang Satellite Launch Center in Sichuan. A three-stage rocket with four strap-on liquid rocket boosters, it is the heaviest variant of the Long March 3 rocket family, and is mainly used to place communications satellites and navigation satellites into geosynchronous orbits.
A heavy-lift launch vehicle (HLV) is an orbital launch vehicle capable of generating a large amount of lift to reach its intended orbit. Heavy-lift launch vehicles generally are capable of lifting payloads between 20,000 to 50,000 kg or between 20,000 to 100,000 kilograms into low Earth orbit (LEO). As of 2024, operational heavy-lift launch vehicles include the Long March 5 and the Proton-M.
Falcon Heavy is a super heavy-lift launch vehicle with partial reusability that can carry cargo into Earth orbit and beyond. It is designed, manufactured and launched by American aerospace company SpaceX.
SpaceX manufactures launch vehicles to operate its launch provider services and to execute its various exploration goals. SpaceX currently manufactures and operates the Falcon 9 Block 5 family of medium-lift launch vehicles and the Falcon Heavy family of heavy-lift launch vehicles – both of which are powered by SpaceX Merlin engines and employ VTVL technologies to reuse the first stage. As of 2024, the company is also developing the fully reusable Starship launch system, which will replace Falcon 9, Falcon Heavy, and Dragon.
The H3 Launch Vehicle is a Japanese expendable launch system. H3 launch vehicles are liquid-propellant rockets with strap-on solid rocket boosters and are launched from Tanegashima Space Center in Japan. Mitsubishi Heavy Industries (MHI) and JAXA are responsible for the design, manufacture, and operation of the H3. The H3 is the world's first rocket to use an expander bleed cycle for the first stage engine.
Space launch market competition is the manifestation of market forces in the launch service provider business. In particular it is the trend of competitive dynamics among payload transport capabilities at diverse prices having a greater influence on launch purchasing than the traditional political considerations of country of manufacture or the national entity using, regulating or licensing the launch service.
Vulcan Centaur is a heavy-lift launch vehicle created and operated by United Launch Alliance (ULA). It is a two-stage-to-orbit launch vehicle consisting of the Vulcan first stage and the Centaur second stage. It replaces ULA's Atlas V and Delta IV rockets. It is principally designed for the National Security Space Launch (NSSL) program, which launches satellites for U.S. intelligence agencies and the Defense Department, but ULA believes it will also be able to price missions low enough to attract commercial launches.
OmegA was a medium-lift to heavy-lift launch vehicle concept that spent several years in development by Northrop Grumman during 2016–2020, with that development substantially funded by the U.S. government. OmegA was intended for launching U.S. national security satellites, as part of the U.S. Department of the Air Force National Security Space Launch (NSSL) replacement program.
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.
{{cite web}}
: CS1 maint: unfit URL (link)