Wikipedia

Medium-lift launch vehicle

(Redirected from Comparison of medium lift launch systems)

A medium-lift launch vehicle (MLV) is a rocket launch vehicle that is capable of lifting between 2,000 to 20,000 kg (4,400 to 44,100 lb) by NASA classification or between 5,000 to 20,000 kilograms (11,000 to 44,000 lb) by Russian classification[1] of payload into low Earth orbit (LEO).[2] An MLV is between small-lift launch vehicles and heavy-lift launch vehicles.

Clockwise from top left: Falcon 9, Soyuz-2, LVM3, Nuri, H-IIA, Long March 2D
Class overview
NameMedium-lift launch vehicle
Preceded bySmall-lift launch vehicle
Succeeded byHeavy-lift launch vehicle
BuiltSince 1958
General characteristics
Capacity
  • US definition: 2,000 to 20,000 kg (4,400 to 44,100 lb)
  • Russian definition: 5,000 to 20,000 kg (11,000 to 44,000 lb)

Rated launch vehicles

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Operational

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Vehicle Origin Manufacturer Mass to LEO (kg) Mass to other orbits (kg) Launches First Flight
Falcon 9 Block 5[a]   United States SpaceX 18,500 (reusable)
22,800 (expendable) 		7,350 to GTO (reusable)
8,300 to GTO (expendable)
4,020 to Mars 		348 2018
Soyuz-2   Russia Progress 8,200 3,250 to GTO
4,400 to SSO 		175 2006[b]
Long March 4B/4C   China SAST 4,200 1,500 to GTO
2,800 to SSO 		101 1999
Atlas V   United States ULA 18,850 8,900 to GTO 99 2002
Long March 2D   China SAST 3,500 1,300 to SSO 89 1992
Zenit-3   Ukraine Yuzhmash 7,000 6,160 to GTO 84 1999
Long March 3B/E   China CALT 11,500 5,500 to GTO
6,900 to SSO 		82 2007
Long March 2C   China CALT 3,850 1,900 to SSO 77 1982
PSLV   India ISRO 3,800 1,200 to GTO
1,750 to SSO 		60 1993
H-IIA   Japan Mitsubishi 15,000 6,000 to GTO 48 2001
Long March 3A   China CALT 6,000 2,600 to GTO
5,000 to SSO 		27 1994
Long March 2F   China CALT 8,400 3,500 to GTO 23 1999
Long March 3C   China CALT 9,100 3,800 to GTO
6,500 to SSO 		18 2008
GSLV   India ISRO 5,000 2,700 to GTO 16 2010
Long March 7/7A   China CALT 13,500 5,500 to SSO
7,000 to GTO 		14 2016
Soyuz-2.1v   Russia Progress 2,800 1,400 to SSO 9 2013
LVM3   India ISRO 10,000 4,000 to GTO 7 2017[c]
Long March 6A   China CALT 4,500 to SSO 5 2022
Nuri   South Korea KARI 3,300 1,900 to SSO (700 km) 3 2022[d]
Zhuque-2   China LandSpace 6,000 4,000 to SSO (500 km) 3 2022
Long March 8   China CALT 8,100 4,500 to SSO 3 2020
Angara 1.2   Russia Khrunichev 3,500[3] 2 2022[c]
Vega C   Italy
  Europe[e] 		Avio 2,300 to SSO 2 2022
H3   Japan Mitsubishi 7,900 to GTO
4,000 to SSO 		2 2023
Gravity-1   China Orienspace 6,500 4,000 to SSO 1 2024
Ariane 6 (A62)   France
  Europe[f] 		Ariane Group 10,350 5,000 to GTO 1 2024

Under development

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Vehicle Origin Manufacturer Mass to LEO (kg) Mass to other orbits (kg) Expected Flight
Tianlong-3   China Space Pioneer 17,000 14,000 to SSO 2024
Long March 12   China CALT 10,000 6,000 to SSO 2024
Pallas-1   China Galactic Energy 5,000 3,000 to SSO 2024
Neutron   New Zealand
  United States 		Rocket Lab 13,000 2025[4]
MLV   United States Firefly 14,000[5] 2025
Zhuque-3   China LandSpace 11,000-20,000 2025
Irtysh   Russia Progress 18,000 5,000 to GTO 2025
Hyperbola-3   China i-Space 13,400 (expendable)
8,500 (reusable)[6] 		2025[6]
Unified Launch Vehicle   India ISRO 4,500-15,000 1,500-6,000 to GTO 2026
Long March 10A   China CALT 14,000 2026
Pallas-2   China Galactic Energy 14,000[7] 2026[8]

Retired

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Vehicle Origin Manufacturer[g] Mass to LEO (kg) Mass to other orbits (kg) Launches First Flight Last Flight
Vostok   Soviet Union RSC Energia 4,730 163 1958 1991
Saturn I   United States Chrysler & Douglas 9,000 10 1961 1965
Atlas-Centaur   United States Lockheed 5,100 61 1962 1983
Titan II GLV   United States Martin 3,580 12 1964 1966
Titan IIIC   United States Martin 13,100 3,000 to GTO
1,200 to TMI 		36 1965 1982
Molniya-M   Soviet Union
  Russia 		Progress 2,400 280 1965 2010
Proton-K   Soviet Union
  Russia 		Khrunichev 19,760 311 1965 2012
Soyuz original   Soviet Union OKB-1 6,450 32 1966 1975
R-36 Tsyklon   Soviet Union
  Ukraine 		Yuzhmash 2,820–5,250[9][10] 500–910 to GTO[11] 236 1967 2009
Soyuz-L   Soviet Union OKB-1 5,500 3 1970 1971
Titan IIID   United States Martin 12,300 22 1971 1982
Soyuz-M   Soviet Union OKB-1 6,600 8 1971 1976
Soyuz-U   Soviet Union
  Russia 		Progress 6,900 786 1973 2017
Feng Bao 1   China SAST 2,500 8 1973 1981
Long March 2A   China CALT 2,000 4 1974 1976
Titan IIIE   United States Martin Marietta 15,400 3,700 to TMI 7 1974 1977
Delta 3920–5920   United States McDonnell Douglas 3,452–3,848 30 1980 1990
N-II[12]   Japan Mitsubishi 2,000 8 1981 1987
Soyuz-U2   Soviet Union Progress 7,050 72 1982 1995
Atlas G   United States Lockheed 5,900 7 1984 1989
Long March 3   China CALT 5,000 1,340 to GTO 14 1984 2000
Zenit-2   Soviet Union
  Ukraine 		Yuzhnoye 13,740 36 1985 2004
H-I   Japan Mitsubishi 3,200 1,100 to GTO 9 1986 1992
Long March 4A   China SAST 4,000 2 1988 1990
Ariane 4   France
  Europe[h] 		Aérospatiale 7,600 4,800 to GTO 116 1988 2003
Delta II   United States ULA 6,100 2,170 to GTO
1,000 to HCO 		156 1989 2018
Atlas I, II, III   United States Lockheed 5,900–8,686 2,340–4,609 to GTO 80 1990 2005
Long March 2E   China CALT 9,200 7 1990 1995
H-II / IIS   Japan Mitsubishi 10,060 4,000 to GTO 7 1994 1999
Ariane 5   France
  Europe[i] 		Ariane Group 16,000 6,950 to GTO 117 1996 2023
Long March 3B   China CALT 11,200 5,100 to GTO
5,700 to SSO 		12 1996 2012
Delta III   United States Boeing 8,290 3,810 to GTO 3 1998 2000
Dnepr   Ukraine Yuzhmash 4,500 2,300 to GTO
550 to TLI 		22 1999 2015
Soyuz-FG   Russia Progress 6,900 70 2001 2019
GSLV Mk.I   India ISRO 4,000 2,150 to GTO 6 2001 2010
H-IIB   Japan Mitsubishi 19,000 8,000 to GTO 9 2009 2020
Falcon 9 v1.0   United States SpaceX 10,450 4,540 to GTO 5 2010 2013
Antares 110/120/130   United States Orbital 5,100[13] 1,500 to SSO 5 2013 2014
Falcon 9 v1.1   United States SpaceX 13,150 4,850 to GTO 15 2013 2016
Falcon 9 Full Thrust Blocks 3 and 4[j]   United States SpaceX 15,600+[14] 7,075+[15] to GTO 36 2015 2018
Antares 230/230+   United States Northrop Grumman 8,000[13] 3,000 to SSO 13 2016 2023

Notes

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  1. ^ When launched with an expendable first stage, Falcon 9 has the capacity of a heavy-lift launch vehicle
  2. ^ A suborbital test flight was conducted in 2004, without the upper stage.
  3. ^ a b A suborbital test flight was conducted in 2014, without the upper stage.
  4. ^ A flight in 2021 failed to reach orbit.
  5. ^ The lead manufacturer is from Italy, but the rocket has significant contributions from companies based in Belgium, France, Netherlands, Spain, Switzerland and Ukraine.
  6. ^ The lead manufacturer is from France, but the rocket has significant contributions from companies based in Germany, Italy, Spain, Belgium, Austria, Switzerland and Sweden.
  7. ^ Some vehicles were made by multiple manufacturers during their lifespan due to mergers and acquisitions. For brevity, only the final manufacturer is shown.
  8. ^ The lead manufacturer is from France, but the rocket has significant contributions from companies based across Europe.
  9. ^ The lead manufacturer is from France, but the rocket has significant contributions from companies based across Europe.
  10. ^ When launched with an expendable first stage, Falcon 9 Full Thrust has the capacity of a heavy-lift launch vehicle

See also

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References

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  1. ^ Osipov, Yuri (2004–2017). Great Russian Encyclopedia. Moscow: Great Russian Encyclopedia. Archived from the original on 27 May 2021. Retrieved 9 June 2021.
  2. ^ 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"
  3. ^ "Angara Launch Vehicle Family". Khrunichev State Research and Production Space Center. Retrieved 2 September 2018.
  4. ^ "Rocket Lab Completes Archimedes Engine Build, Begins Engine Test Campaign". www.businesswire.com. 6 May 2024. Retrieved 7 May 2024.
  5. ^ "Medium Launch Vehicle". Firefly Aerospace. Retrieved 11 March 2023.
  6. ^ a b Jones, Andrew (11 December 2023). "China's (reusable) rocket race heats up with new hop test". SpaceNews. Retrieved 1 April 2024.
  7. ^ "三年回望：我们为什么坚定投资星河动力" [Three-year review: Why we firmly invest in Galactic Energy]. 3sNews (in Chinese). Taibo. 20 February 2021. Retrieved 4 March 2021.
  8. ^ Jones, Andrew (22 July 2023). "Galactic Energy registers sixth consecutive successful launch". SpaceNews. Retrieved 17 September 2023.
  9. ^ "Tsiklon-2". Archived from the original on 27 December 2016.
  10. ^ "Tsiklon-4". Encyclopedia Astronautica. Archived from the original on 22 August 2016. Retrieved 8 August 2016.
  11. ^ "Tsyklon-4M (Cyclone-4M) prepares a move to Canada".
  12. ^ "N-2". Encyclopedia Astronautica. Archived from the original on 8 November 2013. Retrieved 12 June 2013.
  13. ^ a b Krebs, Gunter. "Antares (Taurus-2)". Gunter's Space Page. Retrieved 22 September 2018.
  14. ^ "SpaceX and Cape Canaveral Return to Action with First Operational Starlink Mission". NASASpaceFlight.com. 11 November 2019. Retrieved 11 November 2019.
  15. ^ Krebs, Gunter. "Telstar 19V (Telstar 19 Vantage)". Gunter's Space Page. Gunter. Retrieved 7 August 2018.
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