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This comparison of retired orbital launch systems lists the attributes of all retired individual rocket configurations designed to reach orbit. For a list of proposed rocket configurations or individual configurations currently being launched check out Comparison of Orbital Launch Systems.
Retired rockets
Vehicle | Origin | Manufacturer | Height | Mass to ... (kg) | Reuse | Launches (+ suborbital) |
Launch Sites | Date of flight | |||
---|---|---|---|---|---|---|---|---|---|---|---|
LEO | GTO | Other | First | Last | |||||||
Antares 110–130 | United States | Orbital | 40.5-41.9 m | 5,100 | 1,500 to SSO | No | 5 | MARS | 2013 | 2014 | |
Antares 230 / 230+ | United States | Northrop Grumman | 42.5 m | 8,200 | 3,000 to SSO | No | 13 | MARS | 2016 | 2023 | |
Ariane 1 | Europe | Aérospatiale | 49.1 m | 1,830 | No | 11 | CSG | 1979 | 1986 | ||
Ariane 2 | Europe | Aérospatiale | 49.1 m | 2,270 | No | 6 | CSG | 1986 | 1989 | ||
Ariane 3 | Europe | Aérospatiale | 49.1 m | 2,650 | No | 11 | CSG | 1984 | 1989 | ||
Ariane 4 40 | Europe | Aérospatiale | 58.7 m | 4,600 | 2,105 | 2,740 to SSO | No | 7 | CSG | 1990 | 1999 |
Ariane 4 42L | Europe | Aérospatiale | 58.7 m | 7,000 | 3,480 | 4,500 to SSO | No | 13 | CSG | 1993 | 2002 |
Ariane 4 42P | Europe | Aérospatiale | 58.7 m | 6,000 | 2,930 | 3,400 to SSO | No | 15 | CSG | 1990 | 2002 |
Ariane 4 44L | Europe | Aérospatiale | 58.7 m | 7,000 | 4,720 | 6,000 to SSO | No | 40 | CSG | 1989 | 2003 |
Ariane 4 44LP | Europe | Aérospatiale | 58.7 m | 7,000 | 4,220 | 5,000 to SSO | No | 26 | CSG | 1988 | 2001 |
Ariane 4 44P | Europe | Aérospatiale | 58.7 m | 6,500 | 3,465 | 4,100 to SSO | No | 15 | CSG | 1991 | 2001 |
Ariane 5 G | Europe | EADS Astrium | 47.5 m | 18,000 | 6,900 | No | 16 | CSG | 1996 | 2003 | |
Ariane 5 G+ | Europe | EADS Astrium | 47.8 m | 7,100 | No | 3 | CSG | 2004 | 2004 | ||
Ariane 5 GS | Europe | EADS Astrium | 47.8 m | 16,000 | 6,600 | No | 6 | CSG | 2005 | 2009 | |
Ariane 5 ES | Europe | EADS Astrium | 50.7 m | 21,000 | 8,000 | No | 8 | CSG | 2008 | 2018 | |
Ariane 5 ECA | Europe | EADS Astrium | 52.6 m | 21,000 | 11,210 | No | 84 | CSG | 2002 | 2023 | |
ASLV | India | ISRO | 23.5 m | 150 | No | 4 | SDSC | 1987 | 1994 | ||
Athena I LLV-1 | United States | Lockheed Martin | 18.4 m | 500 | No | 1 | VAFB | 1995 | 1995 | ||
Athena I | United States | Lockheed Martin | 18.9 m | 795 | 515 | No | 3 | VAFB, CCSFS, KLC |
1997 | 2001 | |
Athena II | United States | Lockheed Martin | 28.2 m | 1,800 | No | 3 | VAFB, CCSFS |
1998 | 1999 | ||
Black Arrow | United Kingdom | RAE | 13 m | 73 | No | 2 (+2) | WRC | 1969 | 1971 | ||
Blue Scout II | United States | Vought | 24 m | 30 | No | 3 | CCSFS | 1961 | 1961 | ||
Ceres-1 (1) | China | Galactic Energy | 18.5 m | 350 | No | 1 | JSLC | 2020 | 2020 | ||
Ceres-1 (2) | China | Galactic Energy | 19.5 m | 400 | No | 1 | JSLC | 2021 | 2021 | ||
Commercial Titan III | United States | Martin Marietta | 47.3 m | 13,100 | No | 4 | CCSFS | 1990 | 1992 | ||
Conestoga 1620 | United States | Space Services | 15.2 m | 1179 | No | 1 | MARS | 1995 | 1995 | ||
Diamant A | France | SEREB | 18.9 m | 80 | No | 4 | CIEES | 1965 | 1967 | ||
Diamant B | France | SEREB | 23.5 m | 115 | No | 5 | CSG | 1970 | 1973 | ||
Diamant BP4 | France | SEREB | 21.6 m | 153 | No | 3 | CSG | 1975 | 1975 | ||
Dnepr | Ukraine | Yuzhmash | 34.3 m | 3,700 | No | 22 | Baikonur, Yasny |
1999 | 2015 | ||
Energia | Soviet Union | NPO Energia | 58.8 m | 105,000 | 20,000 to GEO
32,000 to TLI |
No | 1 (failed to orbit) | Baikonur | 1987 | 1987 | |
Energia-Buran | Soviet Union | NPO Energia | 58.8 m | 30,000 | Yes | 1 | Baikonur | 1988 | 1988 | ||
Epsilon | Japan | IHI | 24.4 m | 1,200 | N/A | 450 to SSO | No | 1 | KSC | 2013 | 2022 |
Epsilon (enhanced) | Japan | IHI | 26 m | 1,500 | N/A | 590 to SSO | No | 6 | KSC | ||
Europa I | Europe | ELDO | 31.7 m | 1,440 | 200 | No | 3 | WRC | 1968 | 1970 | |
Europa II | Europe | ELDO | 31.7 m | 360 | No | 1 | CSG | 1971 | 1971 | ||
Falcon 1 | United States | SpaceX | 21 m | 470 | No | 5 | Omelek | 2006 | 2009 | ||
Falcon 9 v1.0 | United States | SpaceX | 51.9 m | 9,000 | 3,400 | No | 5 | CCSFS | 2010 | 2013 | |
Falcon 9 v1.1 | United States | SpaceX | 68.3 m | 13,150 | 4,850 | No | 15 | VAFB, CCSFS |
2013 | 2016 | |
Falcon 9 Full Thrust | United States | SpaceX |
69.8m |
17,400 | 5,500 | 9,600 to polar | Yes | 36 | VAFB, CCSFS, KSC |
2015 | 2018 |
22,800 | 8,300 | No | |||||||||
Feng Bao 1 | China | Shanghai Bureau No.2 | 33 m | 2,500 | No | 8 (+3) | JSLC | 1972 | 1981 | ||
GSLV Mk.I(a) | India | ISRO | 49.1 m | 5,000 | 1,540 | No | 1 | SDSC | 2001 | 2001 | |
GSLV Mk.I(b) | India | ISRO | 49.1 m | 5,000 | 2,150 | No | 4 | SDSC | 2003 | 2007 | |
GSLV Mk.I(c) | India | ISRO | 49.1 m | 5,000 | No | 1 | SDSC | 2010 | 2010 | ||
H-I | Japan | Mitsubishi | 42 m | 1,400 | No | 9 | TNSC | 1986 | 1992 | ||
H-II / IIS | Japan | Mitsubishi | 49 m | 10,060 | 4,000 | No | 7 | TNSC | 1994 | 1999 | |
H-IIA 204 | Japan | Mitsubishi | 53 m | 15,000 | 5,950 | No | 5 | TNSC | 2006 | 2021 | |
H-IIA 2022 | Japan | Mitsubishi | 53 m | 4,500 | No | 3 | TNSC | 2005 | 2007 | ||
H-IIA 2024 | Japan | Mitsubishi | 57 m | 11,000 | 5,000 | No | 7 | TNSC | 2002 | 2008 | |
H-IIB | Japan | Mitsubishi | 56.6 m | 16,500 (ISS) | 8,000 | No | 8 | TNSC | 2009 | 2020 | |
Hyperbola-1 (1) | China | i-Space | 20.9 m | 260 | No | 1 | JSLC | 2019 | 2019 | ||
Juno I | United States | Chrysler | 21.2 m | 11 | No | 1 | CCSFS | 1958 | 1959 | ||
Juno II | United States | Chrysler | 24 m | 41 | 6 to TLI | No | 10 | CCSFS | 1958 | 1961 | |
Kaituozhe-1 | China | CALT | 13.6 m | 40 | No | 2 | JSLC | 2002 | 2003 | ||
Kaituozhe-2 | China | CASC | 16.8 m | 800 | No | 1 | JSLC | 2017 | 2017 | ||
Kosmos | Soviet Union | NPO Polyot | 29.6 m | 350 | No | 38 | Kapustin Yar | 1961 | 1967 | ||
Kosmos-1 | Soviet Union | NPO Polyot | 26.3 m | 1,400 | No | 8 | Baikonur | 1964 | 1965 | ||
Kosmos-2 | Soviet Union | NPO Polyot | 31 m | 300 | No | 127 | Kapustin Yar, Plesetsk |
1965 | 1977 | ||
Kosmos-3 | Soviet Union | NPO Polyot | 32.4 m | 1,400 | No | 6 | Baikonur | 1966 | 1968 | ||
Kosmos-3M | Soviet Union | NPO Polyot | 32.4 m | 1,500 | No | 445 | Kapustin Yar, Plesetsk |
1967 | 2010 | ||
Kosmos-3MRB | Soviet Union | NPO Polyot | 32.4 m | 1,500 | No | 10 | Kapustin Yar | 1980 | 1988 | ||
Lambda 4S | Japan | Nissan Motors | 16.5 m | 26 | No | 5 | KSC | 1966 | 1970 | ||
LauncherOne | United States | Virgin Orbit | 21.3 m | 500 | 300 to SSO | No | 6 | Mojave, Cornwall |
2020 | 2023 | |
Long March 1 | China | CALT | 29.9 m | 300 | No | 2 | JSLC | 1970 | 1971 | ||
Long March 1D | China | CALT | 28.2 m | 740 | No | 0 (+3) | TSLC | 1995 | 2002 | ||
Long March 2A | China | CALT | 32 m | 2,000 | No | 4 | JSLC | 1974 | 1978 | ||
Long March 2E | China | CALT | 49.7 m | 9,200 | No | 7 | XSLC | 1990 | 1995 | ||
Long March 3 | China | CALT | 43.3 m | 5,000 | No | 13 | XSLC | 1984 | 2000 | ||
Long March 3B | China | CALT | 54.8 m | 11,200 | 5,100 | 5,700 to SSO | No | 12 | XSLC | 1996 | 2012 |
Long March 4A | China | CALT | 41.9 m | 4,000 | No | 2 | TSLC | 1988 | 1990 | ||
M-V | Japan | Nissan Motors (1997–2000)
IHI Aerospace (2000–2006) |
30.8 m | 1,850 | No | 7 | KSC | 1997 | 2006 | ||
Molniya | Soviet Union | RSC Energia | 43.4 m | 1,800 | No | 40 | Baikonur, Plesetsk |
1960 | 1967 | ||
Molniya-M | Soviet Union | RSC Energia | 43.4 m | 2,400 | No | 280 | Baikonur, Plesetsk |
1965 | 2010 | ||
Mu-4S | Japan | Nissan Motors | 23.6 m | 180 | No | 4 | KSC | 1971 | 1972 | ||
Mu-3C | Japan | Nissan Motors | 20.3 m | 195 | No | 4 | KSC | 1974 | 1979 | ||
Mu-3H | Japan | Nissan Motors | 23.8 m | 300 | No | 3 | KSC | 1977 | 1978 | ||
Mu-3S | Japan | Nissan Motors | 23.8 m | 300 | No | 4 | KSC | 1980 | 1984 | ||
Mu-3SII | Japan | Nissan Motors | 27.8 m | 770 | No | 8 | KSC | 1985 | 1995 | ||
N1 | Soviet Union | NPO Energia | 105.3 m | 95,000 | No | 4 | Baikonur | 1969 | 1972 | ||
N-I | Japan | Mitsubishi | 34 m | 1,200 | No | 7 | TNSC | 1975 | 1982 | ||
N-II | Japan | Mitsubishi | 35 m | 2,000 | No | 8 | TNSC | 1981 | 1987 | ||
Naro-1 | South Korea | KARI Khrunichev | 33 m | 100 | No | 3 | Naro | 2009 | 2013 | ||
OS-M1 | China | OneSpace | 19 m | 205 | 143 to SSO | No | 1 | JSLC | 2019 | 2019 | |
Paektusan-1 | North Korea | KCST | 25.8 m | 20 | No | 1 | Tonghae | 1998 | 1998 | ||
Pegasus | United States | Northrop Grumman | 15.4 m | 455 | No | 6 | Edwards, CCSFS |
1990 | 1994 | ||
Pegasus H | United States | Northrop Grumman | 15.4 m | 544 | No | 4 | VAFB, CCSFS, Kwajalein Atoll |
1995 | 2000 | ||
Pilot II | United States | United States Navy | 4.4 m | N/A | 1.05 to MEO | No | 10 | Point Mugu | 1958 | 1958 | |
Polyot | Soviet Union | RSC Energia | 30 m | 1,400 | No | 2 | Baikonur | 1963 | 1964 | ||
Proton (UR-500) | Soviet Union | Khrunichev | 39.8 m | 12,200 | No | 4 | Baikonur | 1965 | 1966 | ||
Proton-K | Soviet Union | Khrunichev | 50 m | 19,760 | 4,930 | No | 311 | Baikonur | 1965 | 2012 | |
PSLV-G | India | ISRO | 44 m | 3,200 | 1,050 | 1,600 to SSO | No | 12 | SDSC | 1993 | 2016 |
Rocket 3.0 | United States | Astra | 11.6 m | 100 | No | 1 | KLC | 2020 | 2020 | ||
Rocket 3.1 | United States | Astra | 11.6 m | 100 | No | 1 | KLC | 2020 | 2020 | ||
Rocket 3.2 | United States | Astra | 11.6 m | 100 | No | 1 | KLC | 2020 | 2020 | ||
Rocket 3.3 | United States | Astra | 13.1 m | 100 | 150 to SSO | No | 5 | CCSFS, KLC |
2021 | 2022 | |
Rokot-K | Russia | Khrunichev | 25.5 m | No | 4 | Baikonur, Plesetsk |
1990 | 1999 | |||
Rokot-KM | Russia | Khrunichev | 29.1 m | 1,950 | 1,200 to SSO | No | 31 | Plesetsk | 2000 | 2019 | |
RS1 B1 | United States | ABL Space Systems | 27 m | 1,350 | 400 | 975 to SSO
750 to MEO |
No | 1 | KLC | 2023 | 2023 |
Safir-1 | Iran | Iranian Space Agency | 22.6 m | 27 | No | 2 | Semnan | 2008 | 2009 | ||
Safir-1A | Iran | Iranian Space Agency | 22.6 m | 15 | No | 1 | Semnan | 2011 | 2011 | ||
Safir-1B | Iran | Iranian Space Agency | 22.6 m | 50 | No | 1 | Semnan | 2012 | 2012 | ||
Safir-1B+ | Iran | Iranian Space Agency | 22.6 m | 52 | No | 5 | Semnan | 2012 | 2019 | ||
Saturn I | United States | Chrysler (S-I) | 50-57.4 m | 9,000 | No | 10 | CCSFS | 1961 | 1965 | ||
Saturn IB | United States | Chrysler (S-IB) | 56.1-68.1 m | 18,600 | No | 9 | CCSFS, KSC |
1966 | 1975 | ||
Saturn V | United States | Boeing (S-IC) | 110.6 m | 140,000 | 47,000 to TLI | No | 13 | KSC | 1967 | 1973 | |
Scout X-1 | United States | Vought | 21.8 m | 59 | No | 4 | WFF | 1960 | 1961 | ||
Scout X-2 | United States | Vought | 21.8 m | 76 | No | 1 | VAFB, WFF |
1962 | 1962 | ||
Scout X-2M | United States | Vought | 21.8 m | 76 | No | 3 | VAFB | 1962 | 1963 | ||
Scout X-2B | United States | Vought | 21.8 m | 76 | No | 1 | VAFB | 1963 | 1963 | ||
Scout X-3 | United States | Vought | 21.8 m | 87 | No | 5 | VAFB, WFF |
1962 | 1964 | ||
Scout X-3M | United States | Vought | 21.8 m | 87 | No | 1 | VAFB | 1963 | 1963 | ||
Scout X-4 | United States | Vought | 22.8 m | 103 | No | 11 | VAFB, WFF |
1963 | 1965 | ||
Scout A | United States | NASA | 22.8 m | 110 | No | 11 | VAFB | 1965 | 1970 | ||
Scout A-1 | United States | NASA | 22.8 m | 122 | No | 1 | VAFB | 1973 | 1973 | ||
Scout B | United States | NASA | 22.8 m | 110 | No | 20 | BSC, VAFB, WFF |
1965 | 1971 | ||
Scout B-1 | United States | NASA | 22.8 m | 143 | No | 5 | BSC, VAFB, WFF |
1971 | 1976 | ||
Scout D-1 | United States | NASA | 22.9 m | 182 | No | 14 | BSC, VAFB, WFF |
1972 | 1979 | ||
Scout E-1 | United States | NASA | 22.8 m | 193 | No | 1 | VAFB | 1974 | 1974 | ||
Scout F-1 | United States | NASA | 22.9 m | 192 | No | 2 | BSC, VAFB |
1975 | 1975 | ||
Scout G-1 | United States | NASA | 22.9 m | 208 | No | 18 | BSC, VAFB, WFF |
1979 | 1994 | ||
Shavit | Israel | IAI | 17.7 m | 160 | No | 2 | Palmachim | 1988 | 1990 | ||
Shavit-1 | Israel | IAI | 19.7 m | 225 | No | 4 | Palmachim | 1995 | 2004 | ||
Shtil-1 | Russia | Makeyev | 14.8 m | 280–420 | No | 2 | Novomoskovsk, Ekaterinburg |
1998 | 2006 | ||
SLV-3 | India | ISRO | 22 m | 40 | No | 4 | SDSC | 1979 | 1983 | ||
Soyuz | Soviet Union | RSC Energia | 45.6 m | 6,450 | No | 31 | Baikonur | 1966 | 1976 | ||
Soyuz-FG | Russia | TsSKB-Progress | 49.5 m | 6,900 | No | 70 | Baikonur | 2001 | 2019 | ||
Soyuz-L | Soviet Union | RSC Energia | 50 m | 5,500 | No | 3 | Baikonur | 1970 | 1971 | ||
Soyuz-M | Soviet Union | RSC Energia | 50 m | 6,600 | No | 8 | Baikonur | 1971 | 1976 | ||
Soyuz ST-A | Russia | TsSKB-Progress | 46.3 m | 7,800 from Kourou | 2,810 with Fregat | No | 9 | CSG | 2011 | 2021 | |
Soyuz ST-B | Russia | TsSKB-Progress | 46.3 m | 9,000 from Kourou | 3,250 with Fregat | 4,400 to SSO | No | 18 | CSG | 2011 | 2022 |
Soyuz-U | Soviet Union | TsSKB-Progress | 51.1 m | 6,650 from Baikonour
6,150 from Plesetsk |
No | 786 | Baikonur, Plesetsk |
1973 | 2017 | ||
Soyuz-U2 | Soviet Union | TsSKB-Progress | 34.5 m | 7,050 | No | 72 | Baikonur | 1982 | 1995 | ||
Space Shuttle | United States | ATK (SRBs) | 56.1 m | 24,400 | 3,550 to escape with IUS | Yes | 135 | KSC | 1981 | 2011 | |
SPARK | United States | UHAerojet RocketdyneSandia | 17 m | 300 | No | 1 | Barking Sands | 2015 | 2015 | ||
Sparta | United States | ABMA/Chrysler | 21.8 m | 45 | No | 10 | WRC | 1966 | 1967 | ||
Sputnik 8K71PS | Soviet Union | RSC Energia | 30 m | 500 | No | 2 | Baikonur | 1957 | 1957 | ||
Sputnik 8A91 | Soviet Union | RSC Energia | 31.1 m | 1,327 | No | 2 | Baikonur | 1958 | 1958 | ||
SS-520 | Japan | IHI Aerospace | 9.5 m | 4 | No | 2 | KSC | 2017 | 2018 | ||
Start-1 | Russia | MITT | 22.7 m | 532 | 250 to SSO | No | 5 | Svobodny, Plesetsk |
1993 | 2006 | |
Start-1.2 | Russia | MITT | 22.7 m | 250-300 to SSO | No | 1 | Svobodny | 1997 | 1997 | ||
Start | Russia | MITT | 28.9 m | 300 to SSO | No | 1 | Plesetsk | 1995 | 1995 | ||
Strela | Russia | Khrunichev | 24-
27.4 m |
1,400 | No | 3 | Baikonur | 2003 | 2014 | ||
Taurus-1110 | United States | Orbital | 28.2 m | 1180 | 370 | 750 to SSO | No | 3 | VAFB | 1994 | 2000 |
Taurus-2110 | United States | Orbital | 29.1 m | 1250 | 375 | 900 to SSO | No | 2 | VAFB | 1999 | 2001 |
Taurus-2210 | United States | Orbital | 30.9 m | 1050 | 700 to SSO | No | 1 | VAFB | 1998 | 1998 | |
Taurus-3110 | United States | Orbital | 30.1 m | 1450 | 445 | 1,050 to SSO | No | 2 | VAFB | 2009 | 2011 |
Taurus-3210 | United States | Northrop Grumman | 27.9 m | 1,458 | N/A | 1,054 to SSO | No | 1 | VAFB | 2004 | 2004 |
Terran 1 | United States | Relativity Space | 35.2 m | 1,250 | 900 to SSO | No | 1 | CCSFS | 2023 | 2023 | |
Titan II GLV | United States | Martin Marietta | 33 m | 3,600 | No | 11 (+1) | CCSFS | 1964 | 1966 | ||
Titan II(23)G | United States | Martin Marietta | 31.4 m | 3,600 | No | 13 | VAFB | 1988 | 2003 | ||
Titan IIIA | United States | Martin Marietta | 38.5 m | 3,500 | No | 4 | CCSFS | 1964 | 1965 | ||
Titan IIIB | United States | Martin Marietta | 42 m | 3,300 | No | 22 | VAFB | 1966 | 1969 | ||
Titan III(23)B | United States | Martin Marietta | 42 m | 3,350 | No | 9 | VAFB | 1969 | 1971 | ||
Titan III(33)B | United States | Martin Marietta | 42 m | N/A | 4,500 | No | 3 | VAFB | 1971 | 1973 | |
Titan III(24)B | United States | Martin Marietta | 44 m | 4,500 | No | 23 | VAFB | 1971 | 1984 | ||
Titan III(34)B | United States | Martin Marietta | 45.3 m | N/A | No | 11 | VAFB | 1975 | 1987 | ||
Titan IIIC | United States | Martin Marietta | 41 m | 11,500 | 3,000 | No | 14 | CCSFS | 1965 | 1970 | |
Titan III(23)C | United States | Martin Marietta | 42.5 m | 13,100 | 3,000 | No | 22 | CCSFS | 1970 | 1982 | |
Titan IIID | United States | Martin Marietta | 36 m | 12,300 | No | 22 | VAFB | 1971 | 1982 | ||
Titan IIIE | United States | Martin Marietta | 48.8 m | 15,400 | No | 7 | CCSFS | 1974 | 1977 | ||
Titan 34D | United States | Martin Marietta | 44.5 m | 14,350 | 3,600 | No | 15 | VAFB, CCSFS |
1982 | 1989 | |
Titan IVA | United States | Martin Marietta | 51.36 m(standard) | 17,110 | 4,944 with IUS | 14,090 to SSO
4,536 to GSO with Centaur 3,550 to escape with IUS |
No | 22 | VAFB, CCSFS |
1989 | 1998 |
Titan IVB | United States | Lockheed Martin | 51.36 m(standard) | 21,682 | 5,761
(9,000 with upper stage) |
No | 17 | VAFB, CCSFS |
1997 | 2005 | |
Tysklon-2 | Soviet Union | Yuzhmash | 32 m | 3,350 | No | 18 | Baikonur | 1965 | 1971 | ||
Tsyklon-2A | Soviet Union | Yuzhmash | 39.7 m | 3,350 | No | 8 | Baikonur | 1967 | 1969 | ||
Tsyklon-2M | Soviet Union | Yuzhmash | 39.7 m | 2,820 | No | 106 | Baikonur | 1969 | 2006 | ||
Tsyklon-3 | Soviet Union | Yuzhmash | 39.3 m | 1,920 | No | 122 | Plesetsk | 1977 | 2009 | ||
Unha-2 | North Korea | KCST | 29.5 m | 80 | No | 1 | Tonghae | 2009 | 2009 | ||
Unha-3 | North Korea | KCST | 30 m | 110 | No | 4 | Sohae | 2009 | 2016 | ||
Vanguard | United States | Martin | 22.1 m | 9 | No | 10 (+1) | CCSFS | 1957 | 1959 | ||
Vanguard SLV-7 | United States | Martin | 21.6 m | 20 | No | 1 | CCSFS | 1959 | 1959 | ||
Vega | Europe Italy |
ArianeGroupAvio | 31 m | 2,300 | N/A | 1,450 to SSO 1,500 to polar | No | 22 | CSG | 2012 | 2024 |
VLS-1 | Brazil | AEB, IAE | 19.5 m | 380 | No | 2 | CEA | 1997 | 2003 | ||
Volna-O | Russia | Makeyev | 14.2 m | 100 | No | 1 (+5) | Borisoglebsk | 1995 | 2005 | ||
Voskhod | Soviet Union | RSC Energia | 44.1 m | 5,680 | No | 299 | Baikonur, Plesetsk |
1963 | 1976 | ||
Vostok-L (Luna) | Soviet Union | RSC Energia | 30.8 m | 4,000 | 400 to TLI | No | 9 | Baikonur | 1958 | 1960 | |
Vostok (Korabl) | Soviet Union | RSC Energia | 38.4 m | 4,550 | 390 to TLI | No | 4 | Baikonur | 1960 | 1960 | |
Vostok-K | Soviet Union | RSC Energia | 30.8 m | 2,460 | No | 16 | Baikonur | 1960 | 1964 | ||
Vostok-2 | Soviet Union | RSC Energia | 30.8 m | 4,730 | No | 45 | Baikonur, Plesetsk |
1962 | 1967 | ||
Vostok-2M | Soviet Union | RSC Energia | 38.8 m | 1,300 | No | 93 | Baikonur, Plesetsk |
1964 | 1991 | ||
Soyuz/Vostok | Soviet Union | RSC Energia | 31 m | 6,000 | No | 2 | Baikonur | 1965 | 1966 | ||
Zenit-2 | Soviet Union | Yuzhnoye | 57 m | 13,740 | No | 36 | Baikonur | 1985 | 2004 | ||
Zenit-2FG | Ukraine | Yuzhnoye | 57 m | No | 1 | Baikonur | 2011 | 2011 | |||
Zenit-2M | Ukraine | Yuzhnoye | 57 m | 13,920 | No | 1 | Baikonur | 2007 | 2007 | ||
Zenit-3F | Ukraine | Yuzhnoye | 59.6 m | 1,740 to GEO | No | 4 | Baikonur | 2011 | 2017 | ||
Zenit-3SL | Ukraine | Yuzhmash | 59.6 m | 7,000 | 6,160 | No | 36 | Ocean Odyssey | 1999 | 2014 | |
Zenit-3SLB | Ukraine | Yuzhmash | 59.5 m | 3,750 | No | 6 | Baikonur | 2008 | 2013 | ||
Zhuque-1 | China | LandSpace | 19 m | 300 | 200 to SSO | No | 1 | JSLC | 2018 | 2018 |
Retired Atlas rockets
Vehicle | Origin | Manufacturer | Height | Mass to ... (kg) | Reuse | Launches (+ suborbital) |
Launch Sites | Date of flight | |||
---|---|---|---|---|---|---|---|---|---|---|---|
LEO | GTO | Other | First | Last | |||||||
Atlas-Able | United States | General Dynamics | 28 m | ~175 to TLI | No | 3 | CCSFS | 1959 | 1960 | ||
Atlas-Agena | United States | Convair/General Dynamics | 36 m | 1,000 | 390 to TLI | No | 109 | VAFB, CCSFS |
1960 | 1978 | |
Atlas-Centaur | United States | Lockheed | 36.2-38.8 m | 1,134 | 2,222 | No | 148 | CCSFS | 1962 | 1983 | |
Atlas B | United States | Lockheed Martin | 24.9 m | ~4,000 | No | 10 | CCSFS | 1958 | 1959 | ||
Atlas-D OV1 | United States | Convair/General Dynamics | 25.9 m | 1,400 | No | 7 | VAFB | 1965 | 1967 | ||
Atlas E/F-Agena | United States | Convair/General Dynamics/Lockheed | 34 m | 1,000 | 390 to TLI | No | 1 | VAFB | 1978 | 1978 | |
Atlas E/F-Altair-3A | United States | Convair/General Dynamics | 27.3 m | 210 | No | 1 | VAFB | 1990 | 1990 | ||
Atlas E/F-Burner-2 | United States | Convair/General Dynamics | 28.9 m | 950 | No | 1 | VAFB | 1972 | 1972 | ||
Atlas E/F-MSD | United States | Convair/General Dynamics | 27.3 m | 800 | No | 4 | VAFB | 1976 | 1980 | ||
Atlas E/F-OIS | United States | Convair/General Dynamics | 28.7 m | 870 | No | 2 | VAFB | 1979 | 1985 | ||
Atlas E/F-OV1 | United States | Convair/General Dynamics | 26.5 m | 363 | No | 4 | VAFB | 1968 | 1971 | ||
Atlas E/F-PTS | United States | Convair/General Dynamics | 26.5 m | 295 | No | 1 | VAFB | 1974 | 1974 | ||
Atlas E/F-SGS-1 | United States | Convair/General Dynamics | 29 m | 450 | No | 8 | VAFB | 1977 | 1981 | ||
Atlas E/F-SGS-2 | United States | Convair/General Dynamics | 29 m | 770 | No | 4 | VAFB | 1983 | 1985 | ||
Atlas E/F-Star-17A | United States | Convair/General Dynamics | 27.4 m | N/A | 800 to MPEO | No | 1 | VAFB | 1975 | 1975 | |
Atlas E/F-Star-37S | United States | Convair/General Dynamics | 29 m | N/A | 1,100 to SSO | No | 19 | VAFB | 1978 | 1995 | |
Atlas-F Agena-D | United States | Convair/General Dynamics | 34 m | N/A | 2,300 to Polar | No | 1 | VAFB | 1978 | 1978 | |
Atlas G | United States | Lockheed | 43.9 m | 5,900 | 2,222 | 1,179 to HCO | No | 7 | CCSFS | 1984 | 1989 |
Atlas H MSD | United States | Lockheed | 27 m | 3,630 | No | 5 | VAFB | 1983 | 1987 | ||
Atlas LV-3B | United States | Convair | 28.7 m | 1,360 | No | 9 | CCSFS | 1960 | 1963 | ||
Atlas SLV-3 | United States | Convair | 33.3 m | No | 63 | VAFB, CCSFS |
1966 | 1983 | |||
Atlas SLV-3 Burner-2 | United States | Convair | 30.3 m | ~1,000 | No | 1 | VAFB | 1968 | 1968 | ||
Atlas I | United States | Lockheed Martin | 43.9 m | 5,900 | 2,340 | No | 11 | CCSFS | 1990 | 1997 | |
Atlas II | United States | Lockheed Martin | 47.5 m | 6,780 | 2,810 | 2,000 to HCO | No | 10 | VAFB, CCSFS |
1991 | 1998 |
Atlas IIA | United States | Lockheed Martin | 47.5 m | 7,316 | 3,180 | 2,160 to HCO | No | 23 | VAFB, CCSFS |
1992 | 2002 |
Atlas IIAS | United States | Lockheed Martin | 49 m | 8,618 | 3,833 | 2,680 to HCO | No | 30 | VAFB, CCSFS |
1993 | 2004 |
Atlas IIIA | United States | Lockheed Martin | 52.5 m | 8,686 | 4,060 | 2,970 to HCO | No | 2 | CCSFS | 2000 | 2004 |
Atlas IIIB/DEC | United States | Lockheed Martin | 53.7 m | 10,759 | 4,609 | No | 1 | CCSFS | 2002 | 2002 | |
Atlas IIIB/SEC | United States | Lockheed Martin | 54.7 m | 10,218 | 4,193 | No | 3 | CCSFS | 2003 | 2005 | |
Atlas V 401 | United States | ULA | 57.3 m | 9,050 | 4,950 | 6,670 to SSO | No | 41 | VAFB, CCSFS |
2002 | 2022 |
Atlas V 411 | United States | ULA | 58.2 m | 9,050 | 6,075 | 8,495 to SSO | No | 6 | VAFB, CCSFS |
2006 | 2020 |
Atlas V 421 | United States | ULA | 59.1 m | 9,050 | 7,000 | 9,050 to SSO | No | 9 | VAFB, CCSFS |
2007 | 2022 |
Atlas V 431 | United States | ULA | 59.1 m | 9,050 | 7,800 | 9,050 to SSO | No | 3 | VAFB, CCSFS |
2005 | 2016 |
Atlas V 501 | United States | ULA | 62.5 m | 8,250 | 3,970 | 5,945 to SSO 1,500 to GEO |
No | 8 | VAFB, CCSFS |
2010 | 2023 |
Atlas V 511 | United States | ULA | 62.5 m | 11,000 | 5,250 | 7,820 to SSO
1,750 to GEO |
No | 1 | VAFB, CCSFS |
2022 | 2022 |
Atlas V 521 | United States | ULA | 59.7 m | 13,300 | 6,485 | 9,585 to SSO
2,760 to GEO |
No | 2 | VAFB, CCSFS |
2003 | 2004 |
Atlas V 531 | United States | ULA | 59.7 m | 15,300 | 7,425 | 11,160 to SSO
3,250 to GEO |
No | 5 | VAFB, CCSFS |
2010 | 2022 |
Atlas V 541 | United States | ULA | 59.7 m | 17,100 | 8,240 | 12,435 to SSO
3,730 to GEO |
No | 9 | VAFB, CCSFS |
2011 | 2022 |
Retired Delta rockets
Vehicle | Origin | Manufacturer | Height | Mass to ... (kg) | Reuse | Launches (+ suborbital) |
Launch Sites | Date of flight | |||
---|---|---|---|---|---|---|---|---|---|---|---|
LEO | GTO | Other | First | Last | |||||||
Delta 0300 | United States | McDonnell Douglas | 34 m | 340 | 747 to SSO | No | 3 | VAFB | 1972 | 1973 | |
Delta 0900 | United States | McDonnell Douglas | 34 m | 1,300 | 818 to SSO | No | 2 | VAFB | 1972 | 1972 | |
Delta 1410 | United States | McDonnell Douglas | 35.2 m | 340 | No | 1 | VAFB | 1975 | 1975 | ||
Delta 1604 | United States | McDonnell Douglas | 35.2 m | 390 | No | 2 | CCSFS | 1972 | 1973 | ||
Delta 1900 | United States | McDonnell Douglas | 35.2 m | 1,800 | No | 1 | VAFB | 1973 | 1973 | ||
Delta 1910 | United States | McDonnell Douglas | 35.2 m | 1,066 | No | 1 | CCSFS | 1975 | 1975 | ||
Delta 1913 | United States | McDonnell Douglas | 35.2 m | 328 | No | 1 | CCSFS | 1973 | 1973 | ||
Delta 1914 | United States | McDonnell Douglas | 35.2 m | 680 | No | 2 | CCSFS | 1972 | 1973 | ||
Delta 2310 | United States | McDonnell Douglas | 35.2 m | 336 | No | 3 | VAFB, CCSFS |
1974 | 1981 | ||
Delta 2313 | United States | McDonnell Douglas | 35.2 m | 243 to GEO | No | 3 | VAFB, CCSFS |
1974 | 1977 | ||
Delta 2910 | United States | McDonnell Douglas | 35.2 m | 1,887 | No | 6 | VAFB, CCSFS |
1975 | 1978 | ||
Delta 2913 | United States | McDonnell Douglas | 35.2 m | 2,000 | 700 | No | 6 | VAFB, CCSFS |
1975 | 1976 | |
Delta 2914 | United States | McDonnell Douglas | 35.2 m | 724 | No | 30 | VAFB, CCSFS |
1974 | 1979 | ||
Delta 3910 | United States | McDonnell Douglas | 35.2 m | 2,494 | 1,154 with PAM-D | No | 10 | VAFB, CCSFS |
1980 | 1988 | |
Delta 3913 | United States | McDonnell Douglas | 35.2 m | 816 | No | 1 | VAFB, CCSFS |
1981 | 1981 | ||
Delta 3914 | United States | McDonnell Douglas | 35.2 m | 954 | No | 13 | VAFB, CCSFS |
1975 | 1987 | ||
Delta 3920 | United States | McDonnell Douglas | 35.2 m | 3,452 | 1,284 with PAM-D | No | 10 | VAFB, CCSFS |
1982 | 1989 | |
Delta 3924 | United States | McDonnell Douglas | 35.2 m | 1,104 | No | 4 | VAFB, CCSFS |
1982 | 1984 | ||
Delta 4925 | United States | McDonnell Douglas | 35.2 m | 3,400 | 1,312 | No | 2 | VAFB, CCSFS |
1989 | 1990 | |
Delta 5920 | United States | McDonnell Douglas | 35.2 m | 3,848 | No | 1 | VAFB | 1989 | 1989 | ||
Delta II 6920 | United States | McDonnell Douglas | 38.8 m | 3,983 | No | 3 | VAFB, CCSFS |
1990 | 1992 | ||
Delta II 6925 | United States | McDonnell Douglas | 39.4 m | 1,447 | 1,447 | No | 14 | VAFB, CCSFS |
1989 | 1992 | |
Delta II 7320 | United States | Boeing IDS / ULA | 38.9 m | 2,865 | 1,651 to SSO | No | 12 | VAFB, CCSFS |
1999 | 2015 | |
Delta II 7326 | United States | Boeing IDS | 38.4 m | 934 | 636 to TLI
629 to HCO |
No | 3 | VAFB, CCSFS |
1998 | 2001 | |
Delta II 7420 | United States | ULA | 39 m | 3,185 | 1,966 to SSO | No | 14 | VAFB, CCSFS |
1998 | 2018 | |
Delta II 7425 | United States | Boeing IDS | 39 m | 1,100 | 804 to HCO | No | 4 | VAFB, CCSFS |
1998 | 2002 | |
Delta II 7426 | United States | Boeing IDS | 39 m | 1,058 | 734 to TLI
711 to HCO |
No | 1 | VAFB, CCSFS |
1999 | 1999 | |
Delta II 7920 | United States | Boeing IDS / ULA | 39.4 m | 5,030 | 3,123 to SSO | No | 29 | VAFB, CCSFS |
1998 | 2017 | |
Delta II 7925 | United States | Boeing IDS / ULA | 39.4 m | 1,819 | 1,177 to TLI
1,265 to HCO |
No | 69 | VAFB, CCSFS |
1990 | 2009 | |
Delta II-H 7920H | United States | Boeing IDS / ULA | 39 m | 6,097 | No | 3 | VAFB, CCSFS |
2003 | 2011 | ||
Delta II-H 7925H | United States | Boeing IDS / ULA | 39.8 m | 2,171 | 1,508 to HCO | No | 3 | VAFB, CCSFS |
2003 | 2007 | |
Delta III 8930 | United States | Boeing IDS | 39 m | 8,292 | 3,810 | No | 3 | CCSFS | 1998 | 2000 | |
Delta IV Heavy | United States | ULA | 72 m | 28,370 | 14,210 | 23,560 to polar
11,290 to TLI 8,000 to TMI |
No | 16 | VAFB, CCSFS |
2004 | 2024 |
Delta IV M | United States | Boeing IDS | 61.3 m | 9,440 | 4,440 | 7,690 to polar | No | 3 | VAFB, CCSFS |
2003 | 2006 |
Delta IV M+(4,2) | United States | ULA | 61.3 m | 13,140 | 6,390 | 10,250 to polar | No | 14 | VAFB, CCSFS |
2002 | 2019 |
Delta IV M+(5,2) | United States | ULA | 65.5 m | 11,470 | 5,490 | 9,600 to polar | No | 3 | VAFB, CCSFS |
2012 | 2018 |
Delta IV M+(5,4) | United States | ULA | 65.5 m | 14,140 | 7,300 | 11,600 to polar | No | 8 | VAFB, CCSFS |
2009 | 2019 |
Retired Thor rockets
Notes
- Reference altitude 500 km
- First suborbital test in 1969, first orbital launch attempt in 1970
- ^ Despite not being officially acknowledged by the manufacturer, significant changes between different iterations of the rocket lead to the identification of different variants.
- Without Buran, and assuming payload providing orbital insertion
- ^ The U.S. Space Shuttle Transportation System and the Soviet Energia-Buran system consist of launch vehicle rockets and returnable spaceplane orbiter. Payload values listed here are for the mass of the payload in cargo bay of the spaceplanes, excluding the mass of the spaceplanes themselves.
- The SpaceX website lists the F9 payload to LEO as 13,150kg. The payload to GTO is listed as 4,850kg. However, SpaceX has stated that these numbers include a 30% margin to accommodate re-usability.
- Despite not being officially acknowledged by the manufacturer, significant changes between different iterations of the rocket lead to the identification of different variants.
- Suborbital test flights in 1995, 1997 and 2002, no orbital launches attempted
- The N1 rocket was initially designed for 75 t LEO capacity and launch attempts were made with this version, but there were studies to increase the payload capacity to 90–95 t, if a liquid-hydrogen upper stage engine could be developed.
- A suborbital test flight was conducted in May 2018.
- The Saturn V made 13 launches, 12 of which reached the correct orbits, and the other (Apollo 6) reached a different orbit than the one which had been planned; however, some mission objectives could still be completed; NASA, Saturn V News Reference, Appendix: Saturn V Flight History (1968) Archived 2011-05-17 at the Wayback Machine. For more information, see the Saturn V article. The Saturn V launch record is usually quoted as having never failed, e.g. "The rocket was masterminded by Wernher Von Braun and did not fail in any of its flights", Alan Lawrie and Robert Godwin; Saturn, but the Apollo 6 launch should be considered a partial mission failure. The 13th launch of Saturn V was in special configuration (SA-513) with the Skylab.
- A prior version of the SS-520 flew twice as a suborbital sounding rocket in 1998 and 2000. In 2017, the addition of a small third stage enabled orbital launches of ultra-light nano- or picosatellites.
- Reference altitude 400 km
- A suborbital test flight failed in 2006. The first two orbital missions failed in 2009 and 2012, and the rocket finally reached orbit in late 2012.
- A third rocket exploded before launch.
- First orbital launch attempt in 2005
References
- ^ Krebs, Gunter. "Antares (Taurus-2)". Gunter's Space Page. Retrieved 1 December 2019.
- ^ Krebs, Gunter. "Ariane-1, -2, -3, -4". Gunter's Space Page. Retrieved 2 August 2011.
- ^ Krebs, Gunter. "Ariane-5". Gunter's Space Page. Retrieved 31 December 2021.
- "Ariane 5". andegraf.com. Archived from the original on November 28, 2015. Retrieved April 27, 2018.
- "Final launch of Ariane 5 GS completes busy year / Launchers / Our Activities / ESA". European Space Agency. 2009-12-19. Retrieved 2013-11-04.
- ^ "Ariane 5 Users Manual" (PDF). Issue 4. Arianespace. p. 39 (ISS orbit). Archived from the original (PDF) on 27 September 2007. Retrieved 13 November 2007.
- "Ariane 5 sets new record on latest launch". ESA. 24 October 2021. Retrieved 25 October 2021.
- "Welcome To ISRO :: Launch Vehicles". ISRO. Retrieved 2013-11-04.
- ^ Krebs, Gunter. "SLV-3 / ASLV". Gunter's Space Page. Retrieved 18 December 2016.
- "Athena-1 (LLV-1 / LMLV-1)".
- "NASA, Athena Mission Planner's Guide 26 August 2012" (PDF). Archived from the original (PDF) on 7 January 2017. Retrieved 18 December 2015.
- "Athena-2". Astronautix.com. Archived from the original on 2013-11-08. Retrieved 2013-11-04.
- "Athena-2 (LLV-2 / LMLV-2)".
- Encyclopedia Astronautica, Black Arrow Archived 2007-12-06 at the Wayback Machine
- astronautix.com, Titan III Archived 2014-12-25 at the Wayback Machine
- ^ Krebs, Gunter. "Dnepr". Gunter's Space Page. Retrieved 18 December 2016.
- Clark, Stephen (30 December 2016). "Iridium satellites closed up for launch on Falcon 9 rocket". Spaceflight Now. Retrieved 30 December 2016.
Russian officials have said they plan to discontinue Dnepr launches.
- ^ "S. P. Korolev RSC Energia – LAUNCHERS". Energia. Archived from the original on 2016-03-03. Retrieved 2010-08-01.
- ^ "Projects&Products". IHI Aerospace. Archived from the original on 6 April 2011. Retrieved 8 March 2011.
- ^ Krebs, Gunter. "Epsilon". Gunter's Space Page. Retrieved 18 January 2019.
- ^ Krebs, Gunter. "Falcon-1". Gunter's Space Page. Retrieved 18 December 2016.
- ^ "Falcon 9". SpaceX. 2012-11-16. Archived from the original on 5 August 2014.
- Krebs, Gunter. "Falcon-9". Gunter's Space Page. Retrieved 24 May 2018.
- ^ "Capabilities & Services". SpaceX. Archived from the original on 7 October 2013. Retrieved 5 April 2017.
- de Selding, Peter B. (June 15, 2016). "Iridium's SpaceX launch slowed by Vandenberg bottleneck". SpaceNews. Retrieved June 21, 2016.
- Feng Bao 1, part of CZ family
- Krebs, Gunter. "FB-1 (Feng Bao-1)". Gunter's Space Page. Retrieved 17 August 2018.
- ^ "Indian Space Research Organisation - Geosynchronous Satellite Launch Vehicle Mark II". www.isro.gov.in. Retrieved 2023-11-26.
- ^ Krebs, Gunter. "GSLV". Gunter's Space Page. Retrieved 18 December 2016.
- "JERS (Fuyo)".
- astronautix.com, H-2 Archived 2008-07-06 at the Wayback Machine
- ^ Krebs, Gunter. "H-2". Gunter's Space Page. Retrieved 1 August 2011.
- "H-IIA – User's Manual" (PDF). 4.0. Mitsubishi Heavy Industries, MHI Launch Services. February 2015. YET04001. Retrieved 4 September 2018.
- ^ Krebs, Gunter. "H-2A". Gunter's Space Page. Retrieved 12 November 2018.
- astronautix.com H-IIA 2024 Archived 2011-10-11 at the Wayback Machine
- "MHI Launch Services: Launch Vehicles". Mitsubishi Heavy Industries, MHI Launch Services. Retrieved 4 September 2018.
- Krebs, Gunter. "H-2B". Gunter's Space Page. Retrieved 24 September 2019.
- ^ Krebs, Gunter. "Kaituozhe-2 (KT-2)". Gunter's Space Page. Retrieved 2 November 2019.
- "Cosmos-1, 3, 3M and 3MU – SL-8 – C-1".
- ^ "Nissan Heritage Collection online【その他】プリンス自動車工業小史". Nissan Motors. Retrieved 8 March 2011.
- ^ "Satellite Launch Vehicles". Institute of Space and Astronautical Science (ISAS). Retrieved 4 March 2011.
- astronautix.com, Long March 1, also called CZ-1
- ^ Krebs, Gunter. "CZ-1 (Chang Zheng-1)". Gunter's Space Page. Retrieved 12 February 2014.
- astronautix.com, Long March 1D (CZ-1D) Archived 2002-05-25 at the Wayback Machine
- astronautix.com Long March 2A – CZ-2A Archived 2008-05-16 at the Wayback Machine
- ^ Krebs, Gunter. "CZ-2 (Chang Zheng-2)". Gunter's Space Page. Retrieved 5 October 2021.
- ^ Krebs, Gunter. "CZ-3 (Chang Zheng-3)". Gunter's Space Page. Retrieved 5 October 2021.
- "LM-3A Series Launch Vehicles User's Manual Issue 2011" (PDF). 2011. Archived from the original (PDF) on 17 July 2015. Retrieved 17 August 2015.
- "CZ-4B (Chang Zheng-4B)". Gunter's Space Page. Retrieved 2023-12-04.
- astronautix.com, Encyclopedia Astronautica, Molniya 8K78M Archived 2012-05-08 at the Wayback Machine
- Krebs, Gunter. "Molniya (8K78)". Gunter's Space Page. Retrieved 18 December 2016.
- "US-K (73D6)".
- Krebs, Gunter. "Molniya and Soyuz with upper stages". Gunter's Space Page. Retrieved 18 December 2016.
- astronautix.com, N-I- Delta Archived 2008-07-24 at the Wayback Machine
- astronautix.com, Encyclopedia Astronautica, N-2 Archived 2013-11-08 at the Wayback Machine
- "STSAT 2C".
- Goh, Deyana (5 July 2018). "Chinese startup One Space successfully tests first stage engine for orbital rocket". Spacetech Asia. Retrieved 16 August 2018.
- Krebs, Gunter. "OS-M (Chongqing SQX)". Gunter's Space Page. Retrieved 15 April 2019.
- Jones, Andrew (17 May 2018). "Chinese company OneSpace sends OS-X rocket to 40 km in maiden flight". GBTimes. Archived from the original on 25 February 2020. Retrieved 17 May 2018.
- Encyclopedia Astronautica, Proton-K
- "Launch Vehicles". Archived from the original on 2015-11-06. Retrieved 2015-12-18.
- "Proton". Astronautix.com. Archived from the original on September 13, 2008. Retrieved 2013-11-04.
- ^ "PSLV-CA (2)". Gunter's Space Page. Retrieved 2023-12-10.
- "Outcome Budget 2016–2017" (PDF). Government of India, Department of Space. 2016. Archived from the original (PDF) on 25 June 2017. Retrieved 15 September 2018.
Currently, two versions of PSLV are operational, namely PSLV-XL (with six extended version of Strap-on motors) and the PSLV Core-alone (without Strap-on motors).
- Vance, Ashlee (3 February 2020). "A Small-Rocket Maker Is Running a Different Kind of Space Race". Bloomberg News. Retrieved 3 February 2020.
- Krebs, Gunter. "Rokot (Rockot)". Gunter's Space Page. Retrieved 31 August 2019.
- "ABL Space Systems".
- "ABL Space Systems maiden flight fails after liftoff". 10 February 2023.
- astronautix.com, Saturn I Archived 2010-12-07 at the Wayback Machine
- ^ "Saturn-1 & Saturn-1B". Space.skyrocket.de. Retrieved 2013-11-04.
- Encyclopedia Astronautica, Saturn IB Archived 2011-05-14 at the Wayback Machine
- Bilstein, Roger E. "Appendix C: Saturn Family/Mission Data". Stages to Saturn A Technological History of the Apollo/Saturn Launch Vehicles. NASA History Office. Retrieved 7 April 2011.
- Alternatives for Future U.S. Space-Launch Capabilities (PDF), The Congress of the United States. Congressional Budget Office, October 2006, pp. X, 1, 4, 9
- Stafford, Thomas P. (1991), America at the Threshold – Report of the Synthesis Group on America's Space Exploration Initiative, p. 31
- "Vysota / Volna / Shtil".
- ^ "Vysota / Volna / Shtil". Retrieved 2014-12-23.
- ^ "SLV-3". Retrieved 13 February 2014.
- Krebs, Gunter. "Soyuz (11A511)". Gunter's Space Page. Retrieved 20 December 2016.
- "Soyuz-FG Launch Vehicle". Progress Rocket Space Centre. Retrieved 16 May 2015.
- ^ Krebs, Gunter. "Soyuz with Fregat upper stage". Gunter's Space Page. Retrieved 26 September 2019.
- Krebs, Gunter. "Soyuz-FG (11A511U-FG)". Gunter's Space Page. Retrieved 25 September 2019.
- Krebs, Gunter. "Soyuz-L (11A511L)". Gunter's Space Page. Retrieved 20 December 2016.
- Krebs, Gunter. "Soyuz-M (11A511M)". Gunter's Space Page. Retrieved 20 December 2016.
- "Soyuz-ST". Encyclopedia Astronautica. Archived from the original on 24 August 2015. Retrieved 17 May 2015.
- ^ "Soyuz-ST Launch Vehicle". Progress Rocket Space Centre. Retrieved 17 May 2015.
- "Soyuz 2 Launch Vehicle". Russian Space Web. Retrieved 19 May 2015.
- "Soyuz overview". Arianespace. Retrieved 7 June 2018.
- ^ "Soyuz-U Launch Vehicle". JSC "RCC" Progress. Retrieved 16 May 2015.
- Krebs, Gunter. "Soyuz with Ikar and Volga upper stages". Gunter's Space Page. Retrieved 20 December 2016.
- Krebs, Gunter. "Soyuz-U (11A511U)". Gunter's Space Page. Retrieved 20 December 2016.
- Krebs, Gunter. "Soyuz-U2 (11A511U2)". Gunter's Space Page. Retrieved 20 December 2016.
- Krebs, Gunter. "Shuttle (STS)". Gunter's Space Page. Retrieved 14 July 2014.
- "SPACE TRANSPORTATION SYSTEM PAYLOADS". Kennedy Space Center. 2000. Archived from the original on 17 July 2014. Retrieved 14 July 2014.
- "NASA – Space Shuttle". NASA. Retrieved 2012-07-25.
- "Sputnik 2 (PS-2 #1)".
- ^ Krebs, Gunter. "SS-520". Gunter's Space Page. Retrieved 5 November 2017.
- Graham, William (3 February 2018). "Japanese sounding rocket claims record-breaking orbital launch". NASASpaceFlight. Retrieved 3 February 2018.
- "Experimental Launch of World's Smallest Orbital Space Rocket ends in Failure". Spaceflight 101. 14 January 2017. Retrieved 5 November 2017.
- "Start-1".
- "Strela launcher".
- "Strela". Gunter's Space Page. Retrieved 23 Dec 2014.
- "Taurus". Orbital Sciences Corporation. 2012. Archived from the original on 22 July 2012.
- "Taurus / Minotaur-C". Gunter's Space Page. Retrieved 2023-12-10.
- "Terran". Relativity Space. Retrieved 3 February 2022.
- astronautix.com, Titan II GLV Archived 2016-02-28 at the Wayback Machine
- astronautix.com, Titan 23G Archived 2016-03-04 at the Wayback Machine
- astronautix.com, Titan IIIC Archived 2014-12-25 at the Wayback Machine
- astronautix.com, Titan IIID Archived 2016-03-04 at the Wayback Machine
- astronautix.com, Titan IIIE Archived 2015-12-02 at the Wayback Machine
- ^ "Titan-4". Gunter's Space Page. Retrieved 14 July 2014.
- ^ "Titan-4". Space.skyrocket.de. Retrieved 2013-11-04.
- ^ "Fact Sheet – Titan IVB". United States Air Force. Retrieved 2007-11-12.
- astronautix.com, Tsyklon-2A Archived 2013-05-22 at the Wayback Machine
- "Tsiklon-2A (11K67)". Space.skyrocket.de. Retrieved 2013-11-04.
- astronautix.com, Tsyklon-2 Archived 2013-05-22 at the Wayback Machine
- ^ "Tsiklon-2 (11K69)". Space.skyrocket.de. Retrieved 2013-11-04.
- nasaspaceflight.com, Tsyklon-3
- ^ "Tsiklon-3 (11K68)". Space.skyrocket.de. Retrieved 2013-11-04.
- ^ Krebs, Gunter. "Unha ("Taepodong-2")". Gunter's Space Page. Retrieved 20 December 2016.
- astronautix.com, vanguard Archived 2002-05-06 at the Wayback Machine
- Krebs, Gunter. "Vega (P80 based)". Gunter's Space Page. Retrieved 3 September 2024.
- "Vega User's Manual, Issue 4, Revision 0" (PDF). arianespace.com. Arianespace. April 2014. p. 38. Retrieved 3 September 2024.
- "Vega". arianespace.com. Arianespace. Retrieved 3 September 2024.
- Parsonson, Andrew (2024-09-05). "First-Gen Vega Rocket Retired After Successful Sentinel-2C Launch". European Spaceflight. Retrieved 2024-09-05.
- "VLS".
- "IRDT 1, 2, 2R".
- "NASA – NSSDCA – Spacecraft – Details".
- ^ "Spacecraft – Vostok".
- "Meteor-2 (11F632)".
- astronautix.com, Soyuz/Vostok Archived 2010-01-07 at the Wayback Machine
- ^ Kyle, Ed. "Zenit Data Sheet". Spacelaunchreport.com. Archived from the original on August 21, 2010. Retrieved 2013-11-04.
{{cite web}}
: CS1 maint: unfit URL (link) - Krebs, Gunter. "Zenit-2". Gunter's Space Pages. Retrieved 20 December 2016.
- "Zenit launch vehicle". Russianspaceweb.com. Retrieved 2013-11-04.
- "Elektro-L 1, 2, 3".
- ^ Krebs, Gunter. "Zenit-3". Gunter's Space Page. Retrieved 28 December 2017.
- Jones, Andrew (2 August 2018). "Landspace of China to launch first rocket in Q4 2018". SpaceNews. Retrieved 16 August 2018.
- ^ Barbosa, Rui C. (27 October 2018). "Chinese commercial provider LandSpace launches Weilai-1 on a Zhuque-1 rockets – fails to make orbit". NASASpaceFlight.com. Retrieved 27 October 2018.
- "Atlas Centaur LV-3C Development". 25 March 2023. Archived from the original on August 21, 2010.
{{cite web}}
: CS1 maint: unfit URL (link) - "Atlas Centaur".
- ^ Krebs, Gunter. "Atlas Centaur". Gunter's Space Page. Retrieved 1 August 2011.
- astronautix.com, Atlas H
- astronautix.com, Atlas IIIB Archived 2002-05-01 at the Wayback Machine
- ^ "Atlas V". www.ulalaunch.com. Retrieved 2023-11-20.
- "ULA launches two space surveillance satellites for U.S. Space Force". SpaceNews. 2022-01-21. Retrieved 2022-01-24.
- "WMO OSCAR – Satellite: NOAA-3".
- "NASA – NSSDCA – Spacecraft – Details".
- ^ Krebs, Gunter. "Delta". Gunter's Space Page. Retrieved 16 September 2018.
- Wade, Mark. "Delta 0300". Encyclopedia Astronautica. Archived from the original on 11 October 2011. Retrieved 2 August 2011.
- Wade, Mark. "Delta 0900". Encyclopedia Astronautica. Archived from the original on 11 October 2011. Retrieved 2 August 2011.
- "GEOS 3".
- "1972 – 2616 – Flight Archive".
- "OSO 8".
- "Explorer: RAE B".
- "Delta-1914".
- "NASA – NSSDCA – Spacecraft – Details".
- "Skynet 2A, 2B".
- ^ Wade, Mark. "Delta 2913". Encyclopedia Astronautica. Archived from the original on 11 October 2011. Retrieved 2 August 2011.
- "Explorer: DE 1, 2".
- Wade, Mark. "Delta 4000". Encyclopedia Astronautica. Archived from the original on 11 October 2011. Retrieved 2 August 2011.
- Wade, Mark. "Delta 5000". Encyclopedia Astronautica. Archived from the original on 11 October 2011. Retrieved 2 August 2011.
- ^ "Delta IV". www.ulalaunch.com. Retrieved 2023-11-23.
- ^ Krebs, Gunter. "Delta-4". Gunter's Space Page. Retrieved 17 March 2019.
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