Heavy-lift launch vehicle

Launch vehicle capable of lifting over 20,000 kg into low Earth orbit From Wikipedia, the free encyclopedia

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.

NameHeavy-lift launch vehicle
BuiltSince 1966
Quick facts Class overview, Name ...
Class overview
NameHeavy-lift launch vehicle
Preceded byMedium-lift launch vehicle
Succeeded bySuper heavy-lift launch vehicle
BuiltSince 1966
General characteristics
Capacity20,000 to 50,000 kg (44,000 to 110,000 lb)
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History and design

Launch of AS-203, an uncrewed Saturn IB

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).[4] Russia still operates variants of the Proton as of 2024, 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 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.[6]

Commercial

Ariane 5ES carrying ATV-004

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

More information Rocket, Configuration ...
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  United States 7,100 kN (1,600,000 lbf) 21,000 kg (46,000 lb) 1966 20,847 kg (45,960 lb) N/a N/a Retired (1975) No 9 / 9 US$413 million[9]
Proton K Khrunichev  Soviet Union
 Russia
10,470 kN (2,350,000 lbf) 19,760 kg (43,560 lb)[10][b] 1967 22,776 kg (50,212 lb) 4,723 kg (10,412 lb) 6,220 kg (13,710 lb) Retired (2017) No 275 / 310 US$65 million[12]
M  Russia 10,532 kN (2,368,000 lbf) 23,000 kg (51,000 lb)[13] 2001 20,350 kg (44,860 lb) 6,740 kg (14,860 lb) 3,755 kg (8,278 lb) Operational No 104 / 115 US$65 million[12]
Space Shuttle USA  United States 28,750 kN (6,460,000 lbf) 27,500 kg (60,600 lb)[c][14] 1981 22,753 kg (50,162 lb) Classified[d][e] 3,455 kg (7,617 lb) Retired (2011) Partially 133 / 135 US$601 million[15]
Titan IV Lockheed Martin 15,120 kN (3,400,000 lbf) 21,380 kg (47,130 lb)[16] 1989 19,600 kg (43,200 lb)[d][f] Classified[d] 5,712 kg (12,593 lb) Retired (2005) No 35 / 39 US$432 million
Ariane 5 ECA/ES Ariane Group  Europe 15,175 kN (3,411,000 lbf) 21,000 kg (46,000 lb)[18] 1998 20,293 kg (44,738 lb)[19] 11,210 kg (24,710 lb)[20] 6,161.4 kg (13,584 lb)[21] Retired (2023) No 90 / 92 US$200 million[22]
Delta IV Heavy ULA  United States 9,420 kN (2,120,000 lbf) 28,790 kg (63,470 lb)[23] 2007 21,000 kg (46,000 lb)[24] Classified[d] 685 kg (1,510 lb) Retired (2024) No 15 / 16 US$350 million[25]
Angara A5 Angara-A5 Khrunichev, KBKhA  Russia 9,600 kN (2,200,000 lbf) 24,500 kg (54,000 lb)[26] 2014 N/a 2,400 kg (5,300 lb)[27] N/a Operational No 4 / 5 US$100 million (2021) [28]
Angara-A5V Khrunichev, Polyot 38,000 kg (84,000 lb) N/a N/a N/a N/a Under development No ?
Falcon 9 FT Expended SpaceX  United States 7,600 kN (1,700,000 lbf) 22,800 kg (50,300 lb) 2017 17,400 kg (38,400 lb)[29] 7,076 kg (15,600 lb)[30] 1,108 kg (2,443 lb) Operational No 30 / 30 US$69.7 million
Long March 5/5B CALT  China 10,636 kN (2,391,000 lbf) 25,000 kg (55,000 lb)[31] 2016 23,200 kg (51,100 lb)[32] 14,000 kg (31,000 lb)[33] 8,350 kg (18,410 lb)[34] Operational No 14 / 15 US$160 million[35][36]
Falcon Heavy Recoverable boosters and first stage SpaceX  United States 22,800 kN (5,100,000 lbf) >38,000 kg (84,000 lb)[37] 2018 3,700 kg (8,200 lb) 6,465 kg (14,253 lb)[38] ~1,250 kg (2,760 lb) Operational Partially 3 / 3 US$95 million[39]
Starship Block 1 SpaceX 69,627 kN (15,653,000 lbf) 15,000 kg (33,000 lb)[40] 2024 N/a N/a N/a Retired (2024) No 4 / 6 ?
Block 2 69,627 kN (15,653,000 lbf) 35,000 kg (77,000 lb)[40] 2025 N/a N/a N/a Retired (2025) Partially 2 / 5 ?
Vulcan Centaur VC4 ULA 13,137 kN (2,953,000 lbf) 21,400 kg (47,200 lb) 2025 N/a 1,250 kg (2,760 lb) N/a Operational Planned (partial) 1 / 1 US$110 million[41]
VC6 17,259 kN (3,880,000 lbf) 27,200 kg (60,000 lb)[42] N/a N/a N/a N/a Under development Planned (partial)
New Glenn Blue Origin 17,100 kN (3,800,000 lbf) 45,000 kg (99,000 lb)[43] 2025 Unknown N/a N/a Operational Partial 2 / 2 US$68-110 million[44][45]
Ariane 6 A64 Ariane Group  Europe 15,370 kN (3,460,000 lbf) 21,650 kg (47,730 lb)[46] 2024 4,040 kg (8,910 lb)[47] N/a N/a Operational Planned (partially) 4 / 4 US$133 million[48]
Zhuque-3E LandSpace  China 7,200 kN (1,600,000 lbf) 25,600 kg (56,400 lb) 2025 N/a N/a N/a Operational Planned (partially) 1 / 1 ?
Gravity-2 Orienspace ? 21,000 kg (46,000 lb) N/a N/a N/a N/a Under development Planned (partially) ?
Terran R Relativity Space  United States 15,480 kN (3,480,000 lbf) 33,500 kg (73,900 lb) N/a N/a N/a N/a Under development Planned (partially) ?
NGLV NGLV ISRO  India ? 23,000 kg (51,000 lb) N/a N/a N/a N/a Under development Planned (partially) ?
NGLV-H ? 31,700 kg (69,900 lb) N/a N/a N/a N/a Under development Planned (partially) ?
Miura Next Heavy Expended PLD Space  Spain 16,600 kN (3,700,000 lbf) 36,000 kg (79,000 lb)[49] N/a N/a N/a N/a Under development Planned (partially) ?
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Notes

  1. The first successful landing of a Falcon 9 first stage occurred in 2015
  2. Proton-K is considered to be a heavy-lift launch vehicle[11]
  3. excluding orbiter mass
  4. Actual payloads flown are classified under the NRO launch program.
  5. The Space Shuttle deployed payloads with an attached Inertial Upper Stage to reach orbits beyond LEO
  6. KH-11 launches had 19,600 kg[17]

See also

References

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