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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

FieldValue
section1{{Infobox ship/image
image{{multiple image
borderinfobox
Perrow2
total_width300
image1Falcon Heavy Demo Mission (39337245145).jpg
image2长征五号遥二火箭转场.jpg
image3On_the_launch_pad.jpg
image_captionFrom left: Falcon Heavy, Long March 5, Proton-M
section2{{Infobox ship/class overview
nameHeavy-lift launch vehicle
class_beforeMedium-lift launch vehicle
class_afterSuper heavy-lift launch vehicle
built_rangeSince 1966
section3{{Infobox ship/characteristics
capacity20000 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

RocketConfigurationOrganizationNationalityLiftoff thrustMass to LEOMaiden successful flightHeaviest known launchStatusReusableLaunches
(success/total)Cost per launch
(adjusted for inflation)...to LEO or MEO...to GTO or GSO...to HEO and beyond
Saturn IBNASA1,600,000 lbf21000 kg196620847 kg9 / 9title=SP-4221 The Space Shuttle Decision- Chapter 6: Economics and the Shuttleurl=https://history.nasa.gov/SP-4221/ch6.htmaccess-date=2011-01-15publisher=NASA}}
ProtonKKhrunichev
10470 kN19760 kg196722776 kg4723 kg6220 kg275 / 310url=https://www.gao.gov/assets/690/686613.pdftitle=Surplus Missile Motorsdate=August 2017publisher=United States Government Accountability Officeid=GAO-17-609access-date=27 November 2018}}
M10532 kN23000 kg200120350 kg6740 kg3755 kg104 / 115US$65 million
Space ShuttleUSA28750 kN27500 kg198122753 kgClassified3455 kg133 / 135US$601 million
Titan IVLockheed Martin15120 kN21380 kg1989≥ 19600 kgClassified5712 kg35 / 39US$432 million
Ariane 5ECA/ESAriane Group15175 kN21000 kg199820293 kg11210 kg6161.4 kg90 / 92title=Arianespace aims high in Asia-Pacificurl=https://www.flightglobal.com/news/articles/arianespace-aims-high-in-asia-pacific-425928/url-status=livearchive-url=https://web.archive.org/web/20160602105116/https://www.flightglobal.com/news/articles/arianespace-aims-high-in-asia-pacific-425928/archive-date=2 June 2016access-date=1 June 2016publisher=Flightglobal}}
Delta IV HeavyULA9420 kN28790 kg200721000 kgClassified685 kg15 / 16US$350 million
Angara A5Angara-A5Khrunichev, KBKhA9600 kN24500 kg20142400 kg4 / 5date=24 December 2021title=MGM n°3url=https://nextspaceflight.com/launches/details/4924access-date=24 December 2021}}
Angara-A5VKhrunichev, Polyot38000 kg
Falcon 9 FTExpendedSpaceX7600 kN22800 kg201717400 kg7076 kg1108 kg30 / 30US$69.7 million
Long March 5/5BCALT10636 kN25000 kg201623200 kg14000 kg8350 kg14 / 15US$160 million
Falcon HeavyRecoverable boosters and first stageSpaceX22800 kN38000kg}}"38000 kg20183700 kg6465 kg1250kg}}"~1250 kg3 / 3year=2022title=Capabilities & Servicesurl=https://www.spacex.com/media/Capabilities%26Services.pdfurl-status=deadarchive-url=https://web.archive.org/web/20220322170331/https://www.spacex.com/media/Capabilities%26Services.pdfarchive-date=22 March 2022access-date=March 22, 2022publisher=SpaceX }}
StarshipBlock 1SpaceX69627 kN15000 kg2024/
Block 269627 kN35000 kg2025/
Vulcan CentaurVC4ULA13137 kN21400 kg20251250 kg1 / 1US$110 million
VC617259 kN27200 kg
New GlennBlue Origin17100 kN45000 kg20252 / 2US$68-110 million
Ariane 6A64Ariane Group15370 kN21650 kg20244040 kg4 / 4US$133 million
Zhuque-3ELandSpace7200 kN25600 kg20251 / 1
Gravity-2Orienspace21000 kg
Terran RRelativity Space15480 kN33500 kg
NGLVNGLVISRO23000 kg
NGLV-H31700 kg
Miura Next HeavyExpendedPLD Space16600 kN36000 kg

Notes

References

References

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