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 (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] As of 2024[update], operational heavy-lift launch vehicles include the Long March 5 and the Proton-M.[3]
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) |
In addition, the Angara A5, the Falcon 9 Block 5, the Falcon Heavy, the Vulcan Centaur, Ariane 6, and New Glenn are designed to provide heavy-lift capabilities in at least some configurations but have not yet been proven to carry a 20-tonne payload into LEO. Several other heavy-lift rockets are in development. An HLV is between medium-lift launch vehicles and super heavy-lift launch vehicles.
Rated launch vehicles
editOperational
editVehicle | 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[4] | 23,200[5] | 14,000[6] | 8,350 to Moon[7] | 12 | 2016 |
Proton-M | Russia | Khrunichev | 23,000[8] | 23,200[9] | 6,740[10] | 3,755 to Mars[11] | 115 | 2001 |
Angara A5 | Russia | Khrunichev KBKhA |
24,500[12][a] | — | 2,400[13] | — | 4 | 2014 |
Falcon 9[b] | United States | SpaceX | 22,800[14][c] | 17,400[15] | 7,076[16] | 1,108 to HCO | 18[d] | 2015 (Falcon 9 FT)[e] |
Falcon Heavy[f] | United States | SpaceX | 38,000+[17][g] | 3,700 | 6,465[18][h] | 5,900 to Jupiter[19][i] | 11[j] | 2018 |
Vulcan Centaur | United States | ULA | 25,000[20] | — | — | 1,283 to Moon[21] | 2 | 2024 |
Under development
editVehicle | Origin | Manufacturer | Mass to LEO (kg) | Expected flight |
---|---|---|---|---|
New Glenn[22] | United States | Blue Origin | 45,000[23] | 2024[24] |
Ariane 6 (A64) | France Europe[k] |
ArianeGroup | 21,650[25] | 2025 |
HLV | India | ISRO | 20,000 | TBD |
SHLV | India | ISRO | 41,300[26] | TBD |
Zhuque-3 | China | LandSpace | 21,000[27] | 2025 |
Gravity-2 | China | Orienspace | 25,600[28] | 2025 |
Terran R | United States | Relativity Space | 33,500 | 2026[29] |
Angara-A5V | Russia | Khrunichev, Polyot | 38,000 | 2027 |
H3 Heavy | Japan | Mitsubishi | 28,300[30] | 2030 |
Retired
editVehicle | 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[31] | 22,776 | 4,723 | 6,220 | 4[32][l] | 1967 | 2012 |
Space Shuttle | United States | USA | 24,400[m][33] | 22,753 | — | — | 135 | 1981 | 2011 |
Titan IV | United States | Lockheed Martin | 21,680[34] | Classified[n][o] | Classified[n] | 5,712 to Saturn[p] | 39 | 1989 | 2005 |
Ariane 5 ECA/ES | France Europe[q] |
Ariane Group | 21,000[36] | 20,293[37] | 11,210[38] | 6,161.4 to Sun-Earth L2[39] | 92 | 2002 | 2023 |
Delta IV Heavy | United States | ULA | 28,790[40] | 21,000[41][r] | Classified[n] | 685 to heliocentric orbit | 16 | 2004 | 2024 |
Notes
edit- ^ 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
- ^ Falcon Heavy launched Europa Clipper to heliocentric orbit in expendable configuration. Europa Clipper will utilize gravity assists to reach Jovian orbit.
- ^ 8 of these launches were in at least partially expendable configurations, rating the vehicle as super heavy for those launches
- ^ 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 launched 310 times, with 4 launches over 20,000 kg
- ^ excluding orbiter weight
- ^ a b c Actual payloads flown are classified under the NRO launch program.
- ^ KH-11 launches had 19,600 kg[35]
- ^ Cassini-Huygens was launched to heliocentric orbit and used gravity assists to reach Saturn.
- ^ 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, but excludes the residual mass of the upper stage, which did reach orbit, likely offsetting the mass of the LAS.
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
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