From Surf Wiki (app.surf) — the open knowledge base
Heavy-lift launch vehicle
Launch vehicle capable of lifting over 20,000 kg into low Earth orbit
Launch vehicle capable of lifting over 20,000 kg into low Earth orbit
| Field | Value |
|---|---|
| section1 | {{Infobox ship/image |
| image | {{multiple image |
| border | infobox |
| Perrow | 2 |
| total_width | 300 |
| image1 | Falcon Heavy Demo Mission (39337245145).jpg |
| image2 | 长征五号遥二火箭转场.jpg |
| image3 | On_the_launch_pad.jpg |
| image_caption | From left: Falcon Heavy, Long March 5, Proton-M |
| section2 | {{Infobox ship/class overview |
| name | Heavy-lift launch vehicle |
| class_before | Medium-lift launch vehicle |
| class_after | Super heavy-lift launch vehicle |
| built_range | Since 1966 |
| section3 | {{Infobox ship/characteristics |
| capacity | 20000 to |
A heavy-lift launch vehicle (HLV) is an orbital launch vehicle capable of lifting payloads between 20000 to (by NASA classification) or between 20,000 to 100,000 kg (by Russian classification) into low Earth orbit (LEO). Heavy-lift launch vehicles often carry payloads into higher-energy orbits, such as geosynchronous transfer orbit (GTO) or heliocentric orbit (HCO). An HLV is between a medium-lift launch vehicle and a super heavy-lift launch vehicle.
History and design
Government
The first heavy-lift launch vehicles in the 1960s included the US Saturn IB and the Soviet Proton. Saturn IB was designed to carry the Apollo spacecraft into orbit and had increased engine thrust and a redesigned second stage from its predecessor. Proton was originally designed to be a large intercontinental ballistic missile (ICBM). Russia still operates variants of the Proton , although it is expected to be phased out in favor of the Angara A5.
NASA introduced the Space Shuttle as the first partially reusable launch vehicle in 1981. The Space Shuttle carried up to eight crew members in addition to deploying heavy payloads to LEO, including space station modules and Department of Defense payloads. Higher-energy orbits for payloads were reached through the use of a kick stage such as the Inertial Upper Stage.
The United States Air Force (USAF) operated the Titan IV to supplement Space Shuttle launches. This was derived from the Titan family of ICBMs and launch vehicles, with upgrades including solid rocket boosters (SRBs), vehicle lengthening, and an optional third stage. The USAF began the Evolved Expendable Launch Vehicle (EELV) program in 1994 to ensure access to space through contracted launch providers. This led to the development of the Delta IV, with the heavy variant using three first stage cores. United Launch Alliance (ULA) introduced Vulcan Centaur in 2024 as the successor to its Delta IV and Atlas V rockets, with Vulcan featuring a single, wider core and optional SRBs.
China's Long March 5 was introduced in 2016 as the most powerful version of the Long March family. It is notable as a Chinese launch vehicle using non-hypergolic liquid propellants.
Commercial
The European Ariane 5 first flew in 1996 and launched many commercial payloads to GTO. It benefited in this role by launching from Guiana Space Center, a spaceport near the equator in French territory. Ariane 5 often carried multiple payloads per launch and set records for mass to GTO delivered for commercial payloads.
Falcon 9 was introduced by SpaceX in 2010, designed as a medium-lift launch vehicle with a reusable first stage. Falcon 9 grew more capable through iterative design, with upgrades including improved Merlin engines and the lengthening of both stages. Since the introduction of Falcon 9 Full Thrust in 2015, the vehicle meets the capacity requirements of a heavy-lift vehicle when the first stage is expended. In 2021, Falcon 9 carried a record of 143 satellites into orbit on a single launch. Falcon Heavy uses three first stage boosters similarly to Delta IV Heavy, but requires a strengthened center core. Falcon Heavy made its first flight in 2017 and was most capable operational launch vehicle until NASA's SLS launched in 2022. Falcon Heavy is categorized as a heavy-lift launch vehicle when flown in configuration to recover the center core and both side boosters. When expending the center core or all boosters, its payload to LEO exceeds 50,000 kg, qualifying Falcon Heavy as a super heavy-lift launch vehicle.
Rated launch vehicles
| Rocket | Configuration | Organization | Nationality | Liftoff thrust | Mass to LEO | Maiden successful flight | Heaviest known launch | Status | Reusable | Launches | |||||||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| (success/total) | Cost per launch | ||||||||||||||||||||||||
| (adjusted for inflation) | ...to LEO or MEO | ...to GTO or GSO | ...to HEO and beyond | ||||||||||||||||||||||
| Saturn IB | NASA | 1,600,000 lbf | 21000 kg | 1966 | 20847 kg | 9 / 9 | title=SP-4221 The Space Shuttle Decision- Chapter 6: Economics and the Shuttle | url=https://history.nasa.gov/SP-4221/ch6.htm | access-date=2011-01-15 | publisher=NASA}} | |||||||||||||||
| Proton | K | Khrunichev | |||||||||||||||||||||||
| 10470 kN | 19760 kg | 1967 | 22776 kg | 4723 kg | 6220 kg | 275 / 310 | url=https://www.gao.gov/assets/690/686613.pdf | title=Surplus Missile Motors | date=August 2017 | publisher=United States Government Accountability Office | id=GAO-17-609 | access-date=27 November 2018}} | |||||||||||||
| M | 10532 kN | 23000 kg | 2001 | 20350 kg | 6740 kg | 3755 kg | 104 / 115 | US$65 million | |||||||||||||||||
| Space Shuttle | USA | 28750 kN | 27500 kg | 1981 | 22753 kg | Classified | 3455 kg | 133 / 135 | US$601 million | ||||||||||||||||
| Titan IV | Lockheed Martin | 15120 kN | 21380 kg | 1989 | ≥ 19600 kg | Classified | 5712 kg | 35 / 39 | US$432 million | ||||||||||||||||
| Ariane 5 | ECA/ES | Ariane Group | 15175 kN | 21000 kg | 1998 | 20293 kg | 11210 kg | 6161.4 kg | 90 / 92 | title=Arianespace aims high in Asia-Pacific | url=https://www.flightglobal.com/news/articles/arianespace-aims-high-in-asia-pacific-425928/ | url-status=live | archive-url=https://web.archive.org/web/20160602105116/https://www.flightglobal.com/news/articles/arianespace-aims-high-in-asia-pacific-425928/ | archive-date=2 June 2016 | access-date=1 June 2016 | publisher=Flightglobal}} | |||||||||
| Delta IV Heavy | ULA | 9420 kN | 28790 kg | 2007 | 21000 kg | Classified | 685 kg | 15 / 16 | US$350 million | ||||||||||||||||
| Angara A5 | Angara-A5 | Khrunichev, KBKhA | 9600 kN | 24500 kg | 2014 | 2400 kg | 4 / 5 | date=24 December 2021 | title=MGM n°3 | url=https://nextspaceflight.com/launches/details/4924 | access-date=24 December 2021}} | ||||||||||||||
| Angara-A5V | Khrunichev, Polyot | 38000 kg | — | ||||||||||||||||||||||
| Falcon 9 FT | Expended | SpaceX | 7600 kN | 22800 kg | 2017 | 17400 kg | 7076 kg | 1108 kg | 30 / 30 | US$69.7 million | |||||||||||||||
| Long March 5/5B | CALT | 10636 kN | 25000 kg | 2016 | 23200 kg | 14000 kg | 8350 kg | 14 / 15 | US$160 million | ||||||||||||||||
| Falcon Heavy | Recoverable boosters and first stage | SpaceX | 22800 kN | 38000 | kg}}" | 38000 kg | 2018 | 3700 kg | 6465 kg | 1250 | kg}}" | ~1250 kg | 3 / 3 | year=2022 | title=Capabilities & Services | url=https://www.spacex.com/media/Capabilities%26Services.pdf | url-status=dead | archive-url=https://web.archive.org/web/20220322170331/https://www.spacex.com/media/Capabilities%26Services.pdf | archive-date=22 March 2022 | access-date=March 22, 2022 | publisher=SpaceX }} | ||||
| Starship | Block 1 | SpaceX | 69627 kN | 15000 kg | 2024 | / | |||||||||||||||||||
| Block 2 | 69627 kN | 35000 kg | 2025 | / | |||||||||||||||||||||
| Vulcan Centaur | VC4 | ULA | 13137 kN | 21400 kg | 2025 | 1250 kg | 1 / 1 | US$110 million | |||||||||||||||||
| VC6 | 17259 kN | 27200 kg | — | ||||||||||||||||||||||
| New Glenn | Blue Origin | 17100 kN | 45000 kg | 2025 | 2 / 2 | US$68-110 million | |||||||||||||||||||
| Ariane 6 | A64 | Ariane Group | 15370 kN | 21650 kg | 2024 | 4040 kg | 4 / 4 | US$133 million | |||||||||||||||||
| Zhuque-3E | LandSpace | 7200 kN | 25600 kg | 2025 | 1 / 1 | ||||||||||||||||||||
| Gravity-2 | Orienspace | 21000 kg | — | ||||||||||||||||||||||
| Terran R | Relativity Space | 15480 kN | 33500 kg | — | |||||||||||||||||||||
| NGLV | NGLV | ISRO | 23000 kg | — | |||||||||||||||||||||
| NGLV-H | 31700 kg | — | |||||||||||||||||||||||
| Miura Next Heavy | Expended | PLD Space | 16600 kN | 36000 kg | — |
Notes
References
References
- Osipov, Yuri. (2004–2017). "Great Russian Encyclopedia". Great Russian Encyclopedia.
- [http://www.nasa.gov/pdf/500393main_TA01-LaunchPropulsion-DRAFT-Nov2010-A.pdf NASA Space Technology Roadmaps – Launch Propulsion Systems, p.11] {{Webarchive. link. (24 March 2016 : "Small: 0-2t payloads, Medium: 2-20t payloads, Heavy: 20-50t payloads, Super Heavy: >50t payloads")
- May, Sandra. (27 August 2014). "What Is a Heavy Lift Launch Vehicle?". [[NASA]].
- (24 April 2018). "Proton Rocket: Russian Workhorse".
- "Lockheed Martin Titan IV Rocket".
- (28 December 2019). "Launch of China Heavy Rocket a success; Continues its Roadmap to Moon & Beyond".
- (24 January 2021). "SpaceX launches 143 satellites on one rocket in record-setting mission".
- (1 November 2022). "SpaceX’s Falcon Heavy rocket, world’s most powerful rocket, launches after three-year hiatus".
- "SP-4221 The Space Shuttle Decision- Chapter 6: Economics and the Shuttle". NASA.
- "ГКНПЦ имени М.В.Хруничева {{!}} Служебный модуль «Звезда»".
- "Proton".
- (August 2017). "Surplus Missile Motors". United States Government Accountability Office.
- (July 2009). "Proton Launch System Mission Planner's Guide – Section 2. LV Performance". [[International Launch Services]].
- "The Recent Large Reduction in Space Launch Cost".
- Bray, Nancy. (August 3, 2017). "Kennedy Space Center FAQ". NASA.
- [http://www.astronautix.com/lvs/titan4b.htm astronautix.com, Titan IV] {{webarchive. link. (18 February 2016)
- (12 November 2019). "Satellites Missions and Technologies for Geosciences".
- "Ariane 5 Users Manual, Issue 4, P. 39 (ISS orbit)". [[Arianespace]].
- (30 July 2014). "Lanzamiento del ATV-5 Georges Lemaître (Ariane 5 ES)".
- "Ariane Flight VA255".
- "Webb".
- "Arianespace aims high in Asia-Pacific". Flightglobal.
- (June 2013). "Delta IV Launch Services User's Guide, June 2013". [[United Launch Alliance]].
- (December 2014). "NASA Orion Exploration Flight Test-1 PRESS KIT". [[NASA]].
- "ULA CEO Tory Bruno".
- "Spaceflight101, Angara-a5".
- (14 December 2020). "The cargo was delivered to orbit: the launch of the "Angara" was carried out in the normal mode. (In Russian)".
- (24 December 2021). "MGM n°3".
- "Falcon 9 launches to orbit 56 Starlink satellites—weighing in total more than 17.4 metric tons—marking the heaviest payload ever flown on Falcon".
- Stephen Clark. (21 July 2018). "Record-setting commercial satellite awaits blastoff from Cape Canaveral". Spaceflight Now.
- (5 May 2020). "Long March 5B launch clears path for Chinese space station project".
- (2022-07-25). "长五B火箭打赢空间站建造关键之战". 新华网.
- Andrew Jones. (15 December 2023). "China launches large classified optical satellite towards geostationary orbit". SpaceNews.
- (3 May 2024). "Historic journey from Chang'e 6 lifts off".
- (16 December 2023). "A top-secret Chinese spy satellite just launched on a supersized rocket".
- "weibo".
- "Capabilities & Services | SpaceX".
- "Arabsat 6A".
- (2022). "Capabilities & Services". SpaceX.
- Musk, Elon. "Elon Musk on X: "This slide needs an update, but gives a rough idea o…".
- Roulette, Joey. (January 26, 2024). "Vulcan rocket's debut brings long-awaited challenge to SpaceX dominance". Reuters.
- "Vulcan".
- Foust, Jeff. (8 March 2017). "Eutelsat first customer for Blue Origin's New Glenn". [[SpaceNews]].
- Sheetz, Michael. (5 April 2022). "Amazon signs massive rocket deal with 3 firms, including Bezos' Blue Origin, to launch internet satellites".
- Bogaisky, Jeremy. "With New Glenn Launch, Bezos Looks To Break Musk's Stranglehold On Space".
- Lagier, Roland. (March 2018). "Ariane 6 User's Manual Issue 1 Revision 0". [[Arianespace]].
- "METOP-SG-A 1, 2, 3 (Sentinel 5A, 5B, 5C)".
- Enthusiast, Space. (2024-10-18). "ESA Ariane 6 vs SpaceX Starship: Will There Be a Leadership Race?".
- (7 October 2024). "The Miura Next heavy-lift rocket and the manned capsule Lince: PLD Space's ambitious space program for the next twenty years".
This article was imported from Wikipedia and is available under the Creative Commons Attribution-ShareAlike 4.0 License. Content has been adapted to SurfDoc format. Original contributors can be found on the article history page.
Ask Mako anything about Heavy-lift launch vehicle — get instant answers, deeper analysis, and related topics.
Research with MakoFree with your Surf account
Create a free account to save articles, ask Mako questions, and organize your research.
Sign up freeThis content may have been generated or modified by AI. CloudSurf Software LLC is not responsible for the accuracy, completeness, or reliability of AI-generated content. Always verify important information from primary sources.
Report