Heavy-lift launch vehicle
Class overview | |
---|---|
Name | Heavy-lift launch vehicle |
Preceded by | Medium-lift launch vehicle |
Succeeded by | Super heavy-lift launch vehicle |
Built | Since 1966 |
General characteristics | |
Capacity | 20,000 to 50,000 kg (44,000 to 110,000 lb) |
A heavy-lift launch vehicle (HLV) is an orbital launch vehicle capable of lifting payloads between 20,000 to 50,000 kg (44,000 to 110,000 lb) (by NASA classification) or between 20,000 to 100,000 kilograms (44,000 to 220,000 lb) (by Russian classification)[1] into low Earth orbit (LEO).[2] Heavy-lift launch vehicles often carry payloads into higher-energy orbits, such as geosynchronous transfer orbit (GTO) or heliocentric orbit (HCO).[3] An HLV is between a medium-lift launch vehicle and a super heavy-lift launch vehicle.
History and design
[edit]Government
[edit]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).[4] Russia still operates variants of the Proton as of 2024[update], 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.[5] The USAF began the Evolved Expendable Launch Vehicle (EELV) program in 1994 to ensure access to space through contracted launch providers. This lead 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.[6]
Commercial
[edit]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.[a] 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.[7] 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.[8] 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
[edit]Operational
[edit]Vehicle | Origin | Manufacturer | Mass to LEO (kg) | Heaviest launch (kg) | Launches | First flight | ||
---|---|---|---|---|---|---|---|---|
...to LEO or MEO | ...to GTO or GSO | ...to HEO and beyond | ||||||
Long March 5/5B | China | CALT | 25,000[9] | 23,200[10] | 14,000[11] | 8,350 to Moon[12] | 12 | 2016 |
Proton-M | Russia | Khrunichev | 23,000[13] | 20,350[14] | 6,740[15] | 3,755 to Mars[16] | 115 | 2001 |
Angara A5 | Russia | Khrunichev KBKhA |
24,500[17][b] | — | 2,400[18] | — | 4 | 2014 |
Falcon 9[c] | United States | SpaceX | 22,800[19][d] | 17,400[20] | 7,076[21] | 1,108 to HCO | 18[e] | 2015 (Falcon 9 FT)[f] |
Falcon Heavy[g] | United States | SpaceX | 38,000+[22][h] | 3,700 | 6,465[23][i] | 5,900 to Jupiter[24][j] | 11[k] | 2018 |
Vulcan Centaur[l] | United States | ULA | 25,400[25][m] | — | — | 1,500 to HCO[26] | 2 | 2024 |
Under development
[edit]Vehicle | Origin | Manufacturer | Mass to LEO (kg) | Expected flight |
---|---|---|---|---|
New Glenn[27] | United States | Blue Origin | 45,000[28] | 2024[29] |
Ariane 6 (A64) | France Europe[n] |
ArianeGroup | 21,650[30] | 2025 |
HLV | India | ISRO | 20,000 | TBD |
SHLV | India | ISRO | 41,300[31] | TBD |
Zhuque-3 | China | LandSpace | 21,000[32] | 2025 |
Gravity-2 | China | Orienspace | 25,600[33] | 2025 |
Terran R | United States | Relativity Space | 33,500 | 2026[34] |
Angara-A5V | Russia | Khrunichev, Polyot | 38,000 | 2027 |
H3 Heavy | Japan | Mitsubishi | 28,300[35] | 2030 |
Retired
[edit]Vehicle | Origin | Manufacturer | Mass to LEO (kg) | Heaviest launch (kg) | Launches | First flight | Last Flight | ||
---|---|---|---|---|---|---|---|---|---|
...to LEO or MEO | ...to GTO or GSO | ...to HEO and beyond | |||||||
Saturn IB | United States | Chrysler & Douglas | 21,000 | 20,847 | — | — | 9 | 1966 | 1975 |
Proton-K | Soviet Union Russia |
Khrunichev | 19,760[36][o] | 22,776 | 4,723 | 6,220 | 310[38][p] | 1967 | 2012 |
Space Shuttle | United States | USA | 27,500[q][39] | 22,753 | Classified[r][s] | 3,445 to Venus[40][s] | 135 | 1981 | 2011 |
Titan IV | United States | Lockheed Martin | 21,680[41] | ≥ 19,600[r][t] | Classified[r] | 5,712 to Saturn[j] | 39 | 1989 | 2005 |
Ariane 5 ECA/ES | France Europe[u] |
Ariane Group | 21,000[43] | 20,293[44] | 11,210[45] | 6,161.4 to Sun-Earth L2[46] | 92 | 2002 | 2023 |
Delta IV Heavy | United States | ULA | 28,790[47] | < 21,000[48][v] | Classified[r] | 685 to heliocentric orbit | 16 | 2004 | 2024 |
Notes
[edit]- ^ The first successful landing of a Falcon 9 first stage occured in 2015
- ^ from Vostochny cosmodrome
- ^ Only when the first stage is expended. In reusable configuration, Falcon 9 is classified as a medium-lift launch vehicle
- ^ in expendable configuration
- ^ 18 expendable launches for Full Thrust and Block 5 versions, meeting the capacity requirement of a heavy-lift vehicle
- ^ The first Falcon 9 v1.0 launched in 2010; however, versions prior to Falcon 9 Full Thrust were not capable of lifting payloads over 20,000kg
- ^ When all cores are recovered. When the center core is expended, Falcon Heavy is classified as a super heavy-lift launch vehicle with a theoretical payload to LEO over 50,000 kg
- ^ Depending on booster recovery configuration
- ^ to 90,000-km supersynchronous GTO
- ^ a b With spacecraft gravity assists.
- ^ 8 of these launches were in at least partially expendable configurations, rating the vehicle as super heavy for those launches
- ^ Vulcan has heavy-lift capabilities when launching with certain SRB configurations.
- ^ when launching in VC6 configuration with six SRBs
- ^ The lead manufacturer is from France, but the rocket has significant contributions from companies based in Germany, Italy, Spain, Belgium, Austria, Switzerland and Sweden.
- ^ Proton-K is considered to be a heavy-lift launch vehicle[37]
- ^ 4 launches carried over 20,000 kg
- ^ excluding orbiter mass
- ^ a b c d Actual payloads flown are classified under the NRO launch program.
- ^ a b The Space Shuttle deployed payloads with an attached Inertial Upper Stage to reach orbits beyond LEO
- ^ KH-11 launches had 19,600 kg[42]
- ^ The lead manufacturer is from France, but the rocket has significant contributions from companies based across Europe.
- ^ The officially reported mass of 21,000 kg includes the Launch Abort System (LAS) which did not reach orbit.
See also
[edit]- Comparison of orbital launch systems
- Comparison of orbital rocket engines
- Comparison of space station cargo vehicles
- List of orbital launch systems
- Sounding rocket, suborbital launch vehicle
- Small-lift launch vehicle, capable of lifting up to 2,000 kg (4,400 lb) to low Earth orbit
- Medium-lift launch vehicle, capable of lifting between 2,000 and 20,000 kg (4,400 and 44,100 lb) to low Earth orbit
- Super heavy-lift launch vehicle, capable of lifting more than 50,000 kg (110,000 lb) to Low Earth orbit
References
[edit]- ^ Osipov, Yuri (2004–2017). Great Russian Encyclopedia. Moscow: Great Russian Encyclopedia. Archived from the original on 27 May 2021. Retrieved 9 June 2021.
- ^ NASA Space Technology Roadmaps – Launch Propulsion Systems, p.11 Archived 24 March 2016 at the Wayback Machine: "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. Archived from the original on 11 September 2020. Retrieved 11 June 2017.
- ^ Howell, Elizabeth (24 April 2018). "Proton Rocket: Russian Workhorse". Space.com. Retrieved 17 December 2024.
- ^ "Lockheed Martin Titan IV Rocket". National Museum of the United States Air Force. Retrieved 17 December 2024.
- ^ Marie, Olive (28 December 2019). "Launch of China Heavy Rocket a success; Continues its Roadmap to Moon & Beyond". Tech Times. Retrieved 17 December 2024.
- ^ Wattles, Jackie (24 January 2021). "SpaceX launches 143 satellites on one rocket in record-setting mission". CNN. Archived from the original on 24 January 2021. Retrieved 24 January 2021.
- ^ Wattles, Jackie (1 November 2022). "SpaceX's Falcon Heavy rocket, world's most powerful rocket, launches after three-year hiatus". CNN. Retrieved 17 December 2024.
- ^ "Long March 5B launch clears path for Chinese space station project". SpaceNews.com. 5 May 2020. Retrieved 5 June 2020.
- ^ "长五B火箭打赢空间站建造关键之战" (in Simplified Chinese). 新华网. 25 July 2022. Retrieved 26 July 2022.
- ^ Andrew Jones (15 December 2023). "China launches large classified optical satellite towards geostationary orbit". SpaceNews. Retrieved 13 March 2024.
- ^ "Historic journey from Chang'e 6 lifts off". China National Space Administration. 3 May 2024. Archived from the original on 3 May 2024. Retrieved 3 May 2024.
- ^ "Proton Launch System Mission Planner's Guide – Section 2. LV Performance" (PDF). International Launch Services. July 2009. Archived (PDF) from the original on 17 May 2013. Retrieved 11 June 2017.
- ^ "Nauka science module launches to ISS". nasaspaceflight.com. 21 July 2021. Archived from the original on 13 August 2021. Retrieved 13 August 2021.
- ^ Krebs, Gunter. "ViaSat 1". Gunter's Space Page. Archived from the original on 4 June 2017. Retrieved 11 June 2017.
- ^ "ExoMars Trace Gas Orbiter (TGO)". European Space Agency. 12 July 2012. Archived from the original on 27 April 2020. Retrieved 8 March 2014.
- ^ "Spaceflight101, Angara-a5". Archived from the original on 9 August 2018. Retrieved 22 December 2015.
- ^ "The cargo was delivered to orbit: the launch of the "Angara" was carried out in the normal mode. (In Russian)". Vesti.ru. 14 December 2020. Archived from the original on 14 December 2020. Retrieved 14 December 2020.
- ^ "Capabilities & Services (2016)". SpaceX. 28 November 2012. Archived from the original on 2 August 2013. Retrieved 3 May 2016.
- ^ @spacex (26 January 2023). "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" (Tweet). Retrieved 27 January 2023 – via Twitter.
- ^ Stephen Clark (21 July 2018). "Record-setting commercial satellite awaits blastoff from Cape Canaveral". Spaceflight Now.
- ^ "Capabilities & Services | SpaceX". Archived from the original on 4 April 2016. Retrieved 3 May 2016.
- ^ "Arabsat 6A". Gunter's Space Page. Archived from the original on 16 July 2019. Retrieved 13 April 2019.
- ^ "Liftoff! NASA's Europa Clipper Sails Toward Ocean Moon of Jupiter". NASA JPL. Retrieved 4 November 2024.
- ^ "United Launch Alliance Building Rocket of the Future with Industry-Leading Strategic Partnerships" (Press release). United Launch Alliance. 27 September 2018. Archived from the original on 28 September 2018. Retrieved 28 September 2018.
- ^ "Certification Flight 2". Next Spaceflight. Retrieved 16 December 2024.
- ^ "New Glenn". Blue Origin. Retrieved 19 April 2024.
- ^ Foust, Jeff (8 March 2017). "Eutelsat first customer for Blue Origin's New Glenn". SpaceNews. Archived from the original on 21 March 2017. Retrieved 8 March 2017.
- ^ Foust, Jeff [@jeff_foust] (24 April 2024). "For what it's worth: a NASA presentation at a COSPAR planetary protection meeting this morning listed a Sept. 29 launch date for ESCAPADE, the Mars orbiter smallsat mission flying on Blue Origin's New Glenn" (Tweet) – via Twitter.
- ^ Lagier, Roland (March 2018). "Ariane 6 User's Manual Issue 1 Revision 0" (PDF). Arianespace. p. 46. Archived (PDF) from the original on 11 November 2020. Retrieved 27 May 2018.
- ^ "ULV". www.b14643.de. Archived from the original on 31 October 2020. Retrieved 6 January 2021.
- ^ Jones, Andrew (19 January 2024). "China's Landspace conducts first VTVL test for reusable stainless steel rocket". SpaceNews. Retrieved 29 March 2024.
- ^ Jones, Andrew (11 January 2024). "Orienspace breaks Chinese commercial launch records with Gravity-1 solid rocket". SpaceNews. Retrieved 11 January 2024.
- ^ Berger, Eric (12 April 2023). "Relativity Space is moving on from the Terran 1 rocket to something much bigger". Ars Technica. Retrieved 12 April 2023.
- ^ Henry, Caleb (25 October 2019). "Mitsubishi Heavy Industries mulls upgraded H3 rocket variants for lunar missions". SpaceNews. Archived from the original on 11 April 2021. Retrieved 6 January 2021.
- ^ "ГКНПЦ имени М.В.Хруничева | Служебный модуль «Звезда»". www.khrunichev.ru. Archived from the original on 27 May 2011. Retrieved 6 January 2021.
- ^ "Proton". NASA. Retrieved 20 December 2024.
- ^ "Proton Data Sheet". www.spacelaunchreport.com. Archived from the original on 4 July 2018. Retrieved 6 January 2021.
{{cite web}}
: CS1 maint: unfit URL (link) - ^ Jones, Harry. "The Recent Large Reduction in Space Launch Cost" (PDF). NASA. p. 1. Retrieved 17 December 2024.
- ^ "Magellan". NASA. Retrieved 21 December 2024.
- ^ astronautix.com, Titan IV Archived 18 February 2016 at the Wayback Machine
- ^ Carmona, Camps; José, Adriano (12 November 2019). "Nanosatellites and applications to commercial and scientific missions". Satellites Missions and Technologies for Geosciences. doi:10.5772/intechopen.90039. ISBN 978-1-78985-995-9. S2CID 209187371. Archived from the original on 18 May 2021. Retrieved 18 May 2021.
- ^ "Ariane 5 Users Manual, Issue 4, P. 39 (ISS orbit)" (PDF). Arianespace. Archived from the original (PDF) on 27 September 2007. Retrieved 13 November 2007.
- ^ "Lanzamiento del ATV-5 Georges Lemaître (Ariane 5 ES)". 30 July 2014. Archived from the original on 3 August 2014. Retrieved 11 June 2017.
- ^ "Ariane Flight VA255". Arianespace. Retrieved 4 November 2021.
- ^ "Webb". www.esa.int. Retrieved 27 December 2021.
- ^ "Delta IV Launch Services User's Guide, June 2013" (PDF). United Launch Alliance. June 2013. pp. 2–10. Archived from the original (PDF) on 10 July 2014. Retrieved 9 October 2017.
- ^ "NASA Orion Exploration Flight Test-1 PRESS KIT" (PDF). NASA. December 2014. p. 12. Archived (PDF) from the original on 28 August 2018. Retrieved 11 February 2018.