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Every launch vehicle that has attempted an orbital launch, ranked by number of flights. Vehicles with at least three launches have their own page with specifications, sites and the full flight list.
442 vehicles295 profiles
699Falcon 92010–2026 · 99.7% success633Soyuz-U1973–2004 · 97.0% success446Kosmos 11K65M1967–2010 · 95.1% success299Voskhod 11A571963–1976 · 95.7% success272Molniya 8K78M1965–2010 · 95.2% success154Soyuz-U-PVB1984–2017 · 97.4% success140Space Shuttle1981–2011 · 99.3% success126Kosmos 11K631965–1977 · 93.7% success
442 vehicles
| # | Rocket | Country | Builder | Launches | Failures | Success | First | Last | To LEO |
|---|---|---|---|---|---|---|---|---|---|
| 1 | Falcon 9 | United States | SpaceX | 699 | 2 | 99.7% | 2010 | 2026 | 13.2 t |
| 2 | Soyuz-U | Soviet Union | Progress Factory | 633 | 19 | 97.0% | 1973 | 2004 | 7,200 kg |
| 3 | Kosmos 11K65M | Soviet Union | PO Polyot | 446 | 22 | 95.1% | 1967 | 2010 | 1,500 kg |
| 4 | Voskhod 11A57 | Soviet Union | OKB-1 im. S.P. Korolev | 299 | 13 | 95.7% | 1963 | 1976 | 5,600 kg |
| 5 | Molniya 8K78M | Soviet Union | Progress Factory | 272 | 13 | 95.2% | 1965 | 2010 | — |
| 6 | Soyuz-U-PVB | Russia | Progress Factory | 154 | 4 | 97.4% | 1984 | 2017 | 5,000 kg |
| 7 | Space Shuttle | United States | Rockwell International (Air Force Plant 42, Palmdale) | 140 | 1 | 99.3% | 1981 | 2011 | 24.4 t |
| 8 | Kosmos 11K63 | Soviet Union | Yangel KB | 126 | 8 | 93.7% | 1965 | 1977 | 500 kg |
| 9 | Tsiklon-3 | Soviet Union | Southern State Design Bureau | 122 | 7 | 94.3% | 1977 | 2009 | 4,100 kg |
| 10 | Proton-K/DM-2 | Russia | Khrunichev State Research and Production Center | 111 | 7 | 93.7% | 1982 | 2012 | 5,000 kg |
| 11 | Tsiklon-2 | Soviet Union | Yangel KB | 105 | 1 | 99.0% | 1969 | 2006 | 3,350 kg |
| 12 | Chang Zheng 2D | China | Shanghai Academy of Space Technology (CASC 8th Acad) | 102 | 0 | 100.0% | 1992 | 2026 | 3,400 kg |
| 13 | Chang Zheng 3B | China | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 102 | 5 | 95.1% | 1996 | 2026 | — |
| 14 | Proton-M/Briz-M | Russia | Khrunichev State Research and Production Center | 101 | 8 | 92.1% | 2001 | 2023 | 21.0 t |
| 15 | Vostok 8A92M | Soviet Union | Progress Factory | 94 | 1 | 98.9% | 1964 | 1991 | 1,280 kg |
| 16 | Electron | New Zealand | Rocket Lab Ltd. | 89 | 4 | 95.5% | 2017 | 2026 | 150 kg |
| 17 | Soyuz-2-1B | Russia | Progress Factory | 87 | 2 | 97.7% | 2006 | 2026 | 7,600 kg |
| 18 | Soyuz-2-1A | Russia | Progress Factory | 82 | 1 | 98.8% | 2006 | 2026 | 7,600 kg |
| 19 | Chang Zheng 2C | China | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 74 | 1 | 98.6% | 1976 | 2026 | 2,800 kg |
| 20 | Soyuz-U2 | Soviet Union | Progress Factory | 72 | 0 | 100.0% | 1982 | 1995 | 7,200 kg |
| 21 | Ariane 5ECA | France | EADS Launch Vehicles (EADS LV) | 72 | 1 | 98.6% | 2002 | 2019 | 10.0 t |
| 22 | Soyuz-FG | Russia | Progress Factory | 70 | 1 | 98.6% | 2001 | 2019 | 7,200 kg |
| 23 | Proton-K/DM | Soviet Union | Khrunichev State Research and Production Center | 66 | 5 | 92.4% | 1974 | 1990 | 5,000 kg |
| 24 | Thor SLV-2A Agena D | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 61 | 4 | 93.4% | 1963 | 1968 | — |
| 25 | Chang Zheng 4B | China | Shanghai Academy of Space Technology (CASC 8th Acad) | 59 | 1 | 98.3% | 1999 | 2026 | 2,800 kg |
| 26 | Chang Zheng 4C | China | Shanghai Academy of Space Technology (CASC 8th Acad) | 59 | 2 | 96.6% | 2006 | 2026 | 2,800 kg |
| 27 | Atlas SLV-3 Agena D | United States | General Dynamics Astronautics | 48 | 4 | 91.7% | 1964 | 1967 | — |
| 28 | Vostok 8A92 | Soviet Union | OKB-1 im. S.P. Korolev | 45 | 4 | 90.9% | 1962 | 1967 | 4,750 kg |
| 29 | Atlas V 401 | United States | Lockheed Martin Astronautics | 41 | 0 | 100.0% | 2002 | 2022 | — |
| 30 | Molniya 8K78 | Soviet Union | OKB-1 im. S.P. Korolev | 40 | 20 | 50.0% | 1960 | 1967 | — |
| 31 | Thor Agena B | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 40 | 7 | 82.5% | 1960 | 1963 | — |
| 32 | Ariane 44L | France | Aerospatiale/Les Mureaux | 40 | 1 | 97.5% | 1989 | 2003 | — |
| 33 | Proton-K/DM-2M | Russia | Khrunichev State Research and Production Center | 40 | 2 | 95.0% | 1994 | 2006 | 5,000 kg |
| 34 | Kosmos 63S1 | Soviet Union | Yangel KB | 38 | 12 | 68.4% | 1961 | 1967 | 500 kg |
| 35 | Proton-K/D | Soviet Union | Khrunichev State Research and Production Center | 38 | 14 | 62.2% | 1967 | 1975 | 5,000 kg |
| 36 | Titan IIIC | United States | Martin Marietta/Denver | 36 | 2 | 94.4% | 1965 | 1982 | 13.3 t |
| 37 | Zenit-3SL | United States | Southern State Design Bureau | 36 | 3 | 91.7% | 1999 | 2014 | — |
| 38 | Zenit-2 | Russia | Southern State Design Bureau | 35 | 6 | 82.9% | 1985 | 2004 | 13.5 t |
| 39 | H-IIA 202 | Japan | National Space Development Adminstration | 35 | 0 | 100.0% | 2001 | 2025 | 10.0 t |
| 40 | Delta 7925 | United States | McDonnell Douglas Astronautics/HB | 34 | 1 | 97.1% | 1990 | 1997 | — |
| 41 | Soyuz 11A511 | Soviet Union | Progress Factory | 32 | 2 | 93.8% | 1966 | 1976 | 6,500 kg |
| 42 | Atlas SLV-3D Centaur | United States | General Dynamics Astronautics | 32 | 3 | 90.6% | 1973 | 1983 | — |
| 43 | Rokot | Russia | Khrunichev State Research and Production Center | 32 | 2 | 93.8% | 1994 | 2019 | 1,850 kg |
| 44 | Kuaizhou-1A | China | CASIC 4th Academy | 31 | 2 | 93.3% | 2017 | 2025 | 250 kg |
| 45 | Thorad SLV-2G Agena D | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 30 | 1 | 96.7% | 1966 | 1971 | 1,500 kg |
| 46 | Delta 2914 | United States | McDonnell Douglas Astronautics/HB | 30 | 1 | 96.7% | 1974 | 1979 | 2,000 kg |
| 47 | PSLV | India | Vikram Sarabhai Space Center | 30 | 1 | 96.7% | 1993 | 2024 | 1,300 kg |
| 48 | Atlas IIAS | United States | Lockheed Martin Astronautics | 30 | 0 | 100.0% | 1993 | 2004 | 8,618 kg |
| 49 | Pegasus XL | United States | Orbital Sciences Corp./Chandler | 30 | 3 | 90.0% | 1994 | 2026 | 440 kg |
| 50 | Proton-K | Soviet Union | Khrunichev State Research and Production Center | 29 | 3 | 89.7% | 1968 | 2000 | 21.0 t |
| 51 | Chang Zheng 2F | China | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 29 | 0 | 100.0% | 1999 | 2026 | 9,200 kg |
| 52 | Atlas Agena B | United States | General Dynamics Astronautics | 28 | 7 | 75.0% | 1961 | 1965 | — |
| 53 | Delta 7925-9.5 | United States | McDonnell Douglas Astronautics/HB | 28 | 0 | 100.0% | 1998 | 2009 | — |
| 54 | Chang Zheng 6A | China | Shanghai Academy of Space Technology (CASC 8th Acad) | 28 | 0 | 100.0% | 2022 | 2026 | 1,000 kg |
| 55 | Chang Zheng 3A | China | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 27 | 0 | 100.0% | 1994 | 2018 | — |
| 56 | PSLV-XL | India | Vikram Sarabhai Space Center | 27 | 2 | 92.6% | 2008 | 2025 | 1,800 kg |
| 57 | Ariane 44LP | France | Aerospatiale/Les Mureaux | 26 | 1 | 96.2% | 1988 | 2001 | — |
| 58 | Gushenxing 1 | China | Galactic Energy Co. | 24 | 2 | 91.7% | 2020 | 2026 | 350 kg |
| 59 | Titan 24B | United States | Martin Marietta/Denver | 23 | 2 | 91.3% | 1971 | 1984 | 3,600 kg |
| 60 | Atlas IIA | United States | Lockheed Martin Astronautics | 23 | 0 | 100.0% | 1992 | 2002 | 7,316 kg |
| 61 | Atlas V 551 | United States | Lockheed Martin Astronautics | 23 | 0 | 100.0% | 2006 | 2026 | — |
| 62 | Titan IIIB | United States | Martin Marietta/Denver | 22 | 1 | 95.5% | 1966 | 1969 | 3,700 kg |
| 63 | Titan IIID | United States | Martin Marietta/Denver | 22 | 0 | 100.0% | 1971 | 1982 | 11.2 t |
| 64 | Dnepr | Russia | Southern State Design Bureau | 22 | 1 | 95.5% | 1999 | 2015 | 4,500 kg |
| 65 | Vega | France | ELV SpA | 22 | 2 | 90.9% | 2012 | 2024 | 1,500 kg |
| 66 | Scout B | United States | Ling-Temco-Vought Missile Systems | 20 | 2 | 90.0% | 1965 | 1971 | 143 kg |
| 67 | Delta 7920-10C | United States | McDonnell Douglas Astronautics/HB | 20 | 0 | 100.0% | 1997 | 2017 | — |
| 68 | Thor Ablestar | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 19 | 5 | 73.7% | 1960 | 1965 | 150 kg |
| 69 | Soyuz-ST-B | France | Progress Factory | 18 | 1 | 94.4% | 2011 | 2022 | 7,600 kg |
| 70 | Chang Zheng 11 | China | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 18 | 0 | 100.0% | 2015 | 2025 | 500 kg |
| 71 | Chang Zheng 7A | China | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 18 | 2 | 88.9% | 2020 | 2026 | 13.5 t |
| 72 | Vostok 8K72 | Soviet Union | OKB-1 im. S.P. Korolev | 17 | 3 | 82.4% | 1960 | 1964 | 4,700 kg |
| 73 | Thor Delta E1 | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 17 | 0 | 100.0% | 1966 | 1971 | 540 kg |
| 74 | Atlas SLV-3C Centaur | United States | General Dynamics Astronautics | 17 | 3 | 82.4% | 1967 | 1972 | — |
| 75 | Scout G-1 | United States | Ling-Temco-Vought Missile Systems | 17 | 0 | 100.0% | 1979 | 1994 | 205 kg |
| 76 | Chang Zheng 3C | China | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 17 | 0 | 100.0% | 2008 | 2025 | — |
| 77 | Thor Agena A | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 16 | 6 | 60.0% | 1959 | 1960 | 250 kg |
| 78 | R-36O 8K69 | Soviet Union | Yangel KB | 16 | 2 | 87.5% | 1966 | 1970 | — |
| 79 | Ariane 5G | France | EADS Launch Vehicles (EADS LV) | 16 | 2 | 87.5% | 1996 | 2003 | 10.0 t |
| 80 | Lijian-1 | China | CAS Institute of Mechanics | 16 | 1 | 93.8% | 2022 | 2026 | — |
| 81 | Atlas Agena D | United States | General Dynamics Astronautics | 15 | 0 | 100.0% | 1963 | 1965 | — |
| 82 | Scout D-1 | United States | Ling-Temco-Vought Missile Systems | 15 | 0 | 100.0% | 1972 | 1983 | 183 kg |
| 83 | Atlas E | United States | General Dynamics Astronautics | 15 | 0 | 100.0% | 1982 | 1995 | 1,700 kg |
| 84 | Ariane 42P | France | Aerospatiale/Les Mureaux | 15 | 1 | 93.3% | 1990 | 2002 | — |
| 85 | Ariane 44P | France | Aerospatiale/Les Mureaux | 15 | 0 | 100.0% | 1991 | 2001 | — |
| 86 | Delta 4M+(4,2) | United States | Boeing Space Systems (HB) | 15 | 0 | 100.0% | 2002 | 2019 | 10.4 t |
| 87 | Delta 4H | United States | Boeing Space Systems (HB) | 15 | 1 | 93.3% | 2004 | 2024 | — |
| 88 | Chang Zheng 3B/YZ-1 | China | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 15 | 0 | 100.0% | 2015 | 2024 | — |
| 89 | Chang Zheng 6 | China | Shanghai Academy of Space Technology (CASC 8th Acad) | 15 | 0 | 100.0% | 2015 | 2026 | 1,000 kg |
| 90 | Atlas D | United States | General Dynamics Astronautics | 14 | 4 | 71.4% | 1961 | 1967 | 1,400 kg |
| 91 | Delta 7420-10C | United States | McDonnell Douglas Astronautics/HB | 14 | 0 | 100.0% | 1998 | 2018 | — |
| 92 | Falcon Heavy | United States | SpaceX | 14 | 0 | 100.0% | 2018 | 2026 | 54.4 t |
| 93 | Thor Agena D | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 13 | 2 | 84.6% | 1962 | 1963 | — |
| 94 | Saturn V | United States | NASA Marshall Space Flight Center | 13 | 0 | 100.0% | 1967 | 1973 | 75.0 t |
| 95 | Thorad SLV-2H Agena D | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 13 | 1 | 92.3% | 1969 | 1972 | 1,500 kg |
| 96 | Chang Zheng 3 | China | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 13 | 3 | 76.9% | 1984 | 2000 | — |
| 97 | Titan II SLV | United States | Martin-Denver | 13 | 1 | 92.3% | 1988 | 2003 | 1,900 kg |
| 98 | Delta 6925 | United States | McDonnell Douglas Astronautics/HB | 13 | 0 | 100.0% | 1989 | 1992 | — |
| 99 | Ariane 42L | France | Aerospatiale/Les Mureaux | 13 | 0 | 100.0% | 1993 | 2002 | — |
| 100 | GSLV Mk II | India | Vikram Sarabhai Space Center | 13 | 2 | 84.6% | 2010 | 2026 | — |
| 101 | Soyuz-2-1V | Russia | Progress Factory | 13 | 1 | 92.3% | 2013 | 2025 | 2,800 kg |
| 102 | Thor Delta | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 12 | 1 | 91.7% | 1960 | 1962 | 226 kg |
| 103 | Scout X-4 | United States | Ling-Temco-Vought Missile Systems | 12 | 1 | 91.7% | 1963 | 1965 | 103 kg |
| 104 | Titan II GLV | United States | Martin-Denver | 12 | 0 | 100.0% | 1964 | 1966 | 3,600 kg |
| 105 | Thor Burner 2 | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 12 | 0 | 100.0% | 1966 | 1971 | 500 kg |
| 106 | Atlas SLV-3A Agena D | United States | General Dynamics Astronautics | 12 | 1 | 91.7% | 1968 | 1978 | — |
| 107 | Thor Delta M | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 12 | 2 | 83.3% | 1968 | 1971 | — |
| 108 | Proton-K/D-1 | Soviet Union | Khrunichev State Research and Production Center | 12 | 1 | 91.7% | 1975 | 1989 | 5,000 kg |
| 109 | Delta 3914 | United States | McDonnell Douglas Astronautics/HB | 12 | 2 | 83.3% | 1975 | 1986 | 2,700 kg |
| 110 | Minotaur I | United States | Orbital Sciences Corp./Chandler | 12 | 0 | 100.0% | 2000 | 2021 | 340 kg |
| 111 | Ariane 5ECA+ | France | EADS Launch Vehicles (EADS LV) | 12 | 0 | 100.0% | 2019 | 2023 | 10.0 t |
| 112 | Jielong-3 | China | China Long March Rocket Co. Ltd. | 12 | 0 | 100.0% | 2022 | 2026 | 1,500 kg |
| 113 | Chang Zheng 8A | China | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 12 | 0 | 100.0% | 2025 | 2026 | 8,400 kg |
| 114 | Vanguard | United States | Naval Research Lab | 11 | 8 | 27.3% | 1957 | 1959 | 20 kg |
| 115 | Scout A | United States | Ling-Temco-Vought Missile Systems | 11 | 0 | 100.0% | 1965 | 1970 | 121 kg |
| 116 | Titan 34B | United States | Martin Marietta/Denver | 11 | 0 | 100.0% | 1975 | 1987 | 3,600 kg |
| 117 | Ariane 1 | European Space Agency | Aerospatiale/Les Mureaux | 11 | 2 | 81.8% | 1979 | 1986 | — |
| 118 | Ariane 3 | France | Aerospatiale/Les Mureaux | 11 | 1 | 90.9% | 1984 | 1989 | — |
| 119 | Atlas I | United States | Lockheed Martin Astronautics | 11 | 3 | 72.7% | 1990 | 1997 | — |
| 120 | Juno II | United States | Chrysler Michigan Ordnance Missile Plant | 10 | 5 | 50.0% | 1958 | 1961 | 50 kg |
| 121 | Thor Delta C | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 10 | 1 | 90.0% | 1963 | 1967 | 400 kg |
| 122 | Atlas II | United States | Lockheed Martin Astronautics | 10 | 0 | 100.0% | 1991 | 1998 | 6,580 kg |
| 123 | Chang Zheng 7 | China | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 10 | 0 | 100.0% | 2017 | 2026 | 13.5 t |
| 124 | Chang Zheng 5 | China | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 10 | 1 | 90.0% | 2017 | 2026 | 25.0 t |
| 125 | Chang Zheng 2C/YZ-1S | China | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 10 | 0 | 100.0% | 2018 | 2026 | 2,800 kg |
| 126 | Vostok-L 8K72 | Soviet Union | OKB-1 im. S.P. Korolev | 9 | 6 | 33.3% | 1958 | 1960 | 4,000 kg |
| 127 | Thor Delta B | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 9 | 1 | 88.9% | 1962 | 1964 | 370 kg |
| 128 | Atlas F | United States | General Dynamics Astronautics | 9 | 1 | 88.9% | 1968 | 1981 | 1,700 kg |
| 129 | Titan 23B | United States | Martin Marietta/Denver | 9 | 0 | 100.0% | 1969 | 1971 | 3,600 kg |
| 130 | H-1 | Japan | MHI Aerospace Systems, Tobishima Plant | 9 | 0 | 100.0% | 1986 | 1992 | — |
| 131 | Titan 401A/Centaur | United States | Lockheed Martin Astronautics | 9 | 1 | 88.9% | 1994 | 1998 | — |
| 132 | Atlas V 421 | United States | Lockheed Martin Astronautics | 9 | 0 | 100.0% | 2007 | 2022 | — |
| 133 | Safir | Iran | Iran, Islamic Republic of | 9 | 4 | 50.0% | 2008 | 2019 | — |
| 134 | H-IIB | Japan | Japan Aerospace Exploration Agency | 9 | 0 | 100.0% | 2009 | 2020 | 19.0 t |
| 135 | Atlas V 541 | United States | Lockheed Martin Astronautics | 9 | 0 | 100.0% | 2011 | 2022 | — |
| 136 | Soyuz-ST-A | France | Progress Factory | 9 | 0 | 100.0% | 2011 | 2020 | 7,600 kg |
| 137 | Chang Zheng 12 | China | Shanghai Academy of Space Technology (CASC 8th Acad) | 9 | 0 | 100.0% | 2024 | 2026 | — |
| 138 | Thor SLV-2 Agena D | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 8 | 2 | 75.0% | 1963 | 1967 | — |
| 139 | Kosmos 65S3 | Soviet Union | Yangel KB | 8 | 1 | 87.5% | 1964 | 1965 | 1,500 kg |
| 140 | Tsiklon-2A | Soviet Union | Yangel KB | 8 | 1 | 87.5% | 1967 | 1969 | 3,000 kg |
| 141 | Thor Burner 2A | United States | McDonnell Douglas Astronautics/HB | 8 | 0 | 100.0% | 1971 | 1976 | 500 kg |
| 142 | Soyuz 11A511M | Soviet Union | Progress Factory | 8 | 0 | 100.0% | 1971 | 1976 | 6,500 kg |
| 143 | Feng Bao 1 | China | Shanghai Bureau of Astronautics | 8 | 4 | 50.0% | 1973 | 1981 | 2,200 kg |
| 144 | N-2 | Japan | MHI Aerospace Systems, Tobishima Plant | 8 | 0 | 100.0% | 1981 | 1987 | — |
| 145 | Mu-3S-II | Japan | Nissan (Solid propulsion plant) | 8 | 1 | 87.5% | 1985 | 1995 | 800 kg |
| 146 | Molniya 8K78M-PVB | Russia | Progress Factory | 8 | 0 | 100.0% | 1990 | 1992 | — |
| 147 | Delta 7320-10C | United States | McDonnell Douglas Astronautics/HB | 8 | 0 | 100.0% | 2004 | 2015 | — |
| 148 | Delta 4M+(5,4) | United States | Boeing Space Systems (HB) | 8 | 0 | 100.0% | 2009 | 2019 | 11.7 t |
| 149 | Atlas V 501 | United States | Lockheed Martin Astronautics | 8 | 0 | 100.0% | 2010 | 2023 | — |
| 150 | Proton-M/DM-3 | Russia | Khrunichev State Research and Production Center | 8 | 2 | 75.0% | 2010 | 2026 | 21.0 t |
| 151 | Shuang Quxian 1 | China | Beijing Interstellar Glory Space Tech. Co. Ltd. | 8 | 4 | 50.0% | 2019 | 2025 | — |
| 152 | Antares 230+ | United States | Orbital Sciences HIF, Mid-Atlantic Regional Spaceport | 8 | 0 | 100.0% | 2019 | 2023 | 6,250 kg |
| 153 | Vega C | France | Avio s.p.A. | 8 | 1 | 87.5% | 2022 | 2026 | — |
| 154 | Atlas Centaur D | United States | General Dynamics Astronautics | 7 | 1 | 85.7% | 1965 | 1967 | — |
| 155 | Titan IIIE | United States | Martin Marietta/Denver | 7 | 1 | 85.7% | 1974 | 1977 | 14.0 t |
| 156 | N-1 | Japan | MHI Aerospace Systems, Tobishima Plant | 7 | 1 | 85.7% | 1975 | 1982 | 1,200 kg |
| 157 | Atlas F/SVS | United States | General Dynamics Astronautics | 7 | 0 | 100.0% | 1977 | 1980 | 700 kg |
| 158 | Delta 3910/PAM | United States | McDonnell Douglas Astronautics/HB | 7 | 0 | 100.0% | 1980 | 1982 | — |
| 159 | Titan 34D | United States | Martin Marietta/Denver | 7 | 2 | 71.4% | 1983 | 1988 | 15.3 t |
| 160 | Titan 34D/Transtage | United States | Martin Marietta/Denver | 7 | 0 | 100.0% | 1984 | 1989 | — |
| 161 | Atlas G Centaur | United States | General Dynamics Astronautics | 7 | 2 | 71.4% | 1984 | 1989 | 3,630 kg |
| 162 | Ariane 40 | France | Aerospatiale/Les Mureaux | 7 | 0 | 100.0% | 1990 | 1999 | 2,740 kg |
| 163 | Chang Zheng 2E | China | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 7 | 2 | 71.4% | 1990 | 1995 | 9,200 kg |
| 164 | H-II | Japan | MHI Aerospace Systems, Tobishima Plant | 7 | 2 | 71.4% | 1994 | 1999 | 10.1 t |
| 165 | M-V | Japan | Nissan (Solid propulsion plant) | 7 | 1 | 85.7% | 1997 | 2006 | 1,800 kg |
| 166 | Chang Zheng 2C-III/SD | China | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 7 | 0 | 100.0% | 1997 | 1999 | 2,800 kg |
| 167 | Titan 401B/Centaur | United States | Lockheed Martin Astronautics | 7 | 1 | 85.7% | 1997 | 2003 | — |
| 168 | H-IIA 2024 | Japan | National Space Development Adminstration | 7 | 1 | 85.7% | 2002 | 2008 | — |
| 169 | Shavit 2 | Israel | Israeli Aircraft Industries, Mabat factory | 7 | 0 | 100.0% | 2007 | 2025 | 230 kg |
| 170 | Kuaizhou-11 | China | Academy of Rocket Motors Technology (CASC 4th Academy) | 7 | 1 | 85.7% | 2020 | 2026 | — |
| 171 | Chang Zheng 8 | China | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 7 | 0 | 100.0% | 2020 | 2026 | 8,400 kg |
| 172 | Firefly Alpha | United States | Firefly Aerospace | 7 | 3 | 57.1% | 2021 | 2026 | 1,000 kg |
| 173 | Angara-1.2 | Russia | Khrunichev State Research and Production Center | 7 | 0 | 100.0% | 2022 | 2026 | — |
| 174 | H3-22S | Japan | Japan Aerospace Exploration Agency | 7 | 2 | 71.4% | 2023 | 2026 | — |
| 175 | Zhuque-2E | China | LandSpace Technology | 7 | 1 | 85.7% | 2024 | 2026 | 4,000 kg |
| 176 | Jupiter C | United States | U.S. Army Ballistic Missile Agency | 6 | 3 | 50.0% | 1958 | 1958 | 11 kg |
| 177 | NOTS EV1 | United States | Naval Ordnance Test Station | 6 | 6 | 0.0% | 1958 | 1958 | — |
| 178 | Saturn I | United States | NASA Marshall Space Flight Center | 6 | 0 | 100.0% | 1964 | 1965 | 9,000 kg |
| 179 | Thor Delta E | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 6 | 0 | 100.0% | 1965 | 1967 | 540 kg |
| 180 | Saturn IB | United States | NASA Marshall Space Flight Center | 6 | 0 | 100.0% | 1968 | 1975 | — |
| 181 | Thor Delta N | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 6 | 0 | 100.0% | 1968 | 1972 | — |
| 182 | Delta 2910 | United States | McDonnell Douglas Astronautics/HB | 6 | 0 | 100.0% | 1975 | 1978 | — |
| 183 | Delta 3920/PAM | United States | McDonnell Douglas Astronautics/HB | 6 | 0 | 100.0% | 1982 | 1987 | — |
| 184 | Ariane 2 | France | Aerospatiale/Les Mureaux | 6 | 1 | 83.3% | 1986 | 1989 | — |
| 185 | Delta 7920-10 | United States | McDonnell Douglas Astronautics/HB | 6 | 0 | 100.0% | 1995 | 2001 | 5,118 kg |
| 186 | Proton-K/17S40 | Russia | Khrunichev State Research and Production Center | 6 | 0 | 100.0% | 1997 | 2002 | 5,000 kg |
| 187 | Pegasus XL/HAPS | United States | Orbital Sciences Corp./Chandler | 6 | 0 | 100.0% | 1997 | 2005 | 350 kg |
| 188 | GSLV Mk I | India | Vikram Sarabhai Space Center | 6 | 2 | 66.7% | 2001 | 2010 | — |
| 189 | Ariane 5GS | France | EADS Launch Vehicles (EADS LV) | 6 | 0 | 100.0% | 2005 | 2009 | 10.0 t |
| 190 | Atlas V 411 | United States | Lockheed Martin Astronautics | 6 | 0 | 100.0% | 2006 | 2020 | — |
| 191 | Proton-M/DM-2 | Russia | Khrunichev State Research and Production Center | 6 | 0 | 100.0% | 2007 | 2010 | 21.0 t |
| 192 | Zenit-3SLB | Russia | Southern State Design Bureau | 6 | 0 | 100.0% | 2008 | 2013 | — |
| 193 | Minotaur IV | United States | Orbital Sciences Corp./Chandler | 6 | 0 | 100.0% | 2010 | 2026 | 1,735 kg |
| 194 | Epsilon | Japan | Japan Aerospace Exploration Agency | 6 | 1 | 83.3% | 2013 | 2022 | — |
| 195 | Simorgh | Iran | Iran, Islamic Republic of | 6 | 4 | 33.3% | 2019 | 2024 | 50 kg |
| 196 | LVM3 | India | Indian Space Research Organization | 6 | 0 | 100.0% | 2019 | 2025 | — |
| 197 | LauncherOne | United States | Virgin Orbit LLC | 6 | 2 | 66.7% | 2020 | 2023 | 500 kg |
| 198 | Ariane 62 | France | ArianeGroup | 6 | 0 | 100.0% | 2024 | 2026 | — |
| 199 | Scout X-3 | United States | Ling-Temco-Vought Missile Systems | 5 | 1 | 80.0% | 1962 | 1964 | 87 kg |
| 200 | Lambda 4S | Japan | Institute of Space and Aeronautical Sci | 5 | 4 | 20.0% | 1966 | 1970 | 26 kg |
| 201 | Diamant B | France | Soci\'et\'e pour l'etude et la r\'ealisation d'engins ballistiques | 5 | 2 | 60.0% | 1970 | 1973 | 115 kg |
| 202 | Scout B-1 | United States | Ling-Temco-Vought Missile Systems | 5 | 0 | 100.0% | 1971 | 1976 | 143 kg |
| 203 | Thor DSV-2U | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 5 | 1 | 80.0% | 1976 | 1980 | 500 kg |
| 204 | Delta 3924 | United States | McDonnell Douglas Astronautics/HB | 5 | 0 | 100.0% | 1982 | 1987 | — |
| 205 | Atlas H | United States | General Dynamics Astronautics | 5 | 0 | 100.0% | 1983 | 1987 | 2,000 kg |
| 206 | Titan 403A | United States | Lockheed Martin Astronautics | 5 | 1 | 80.0% | 1991 | 1997 | 17.7 t |
| 207 | Start-1 | Russia | Moscow Inst of Thermal Technology | 5 | 0 | 100.0% | 1993 | 2006 | 500 kg |
| 208 | Titan 402B/IUS | United States | Lockheed Martin Astronautics | 5 | 1 | 80.0% | 1997 | 2004 | — |
| 209 | Falcon 1 | United States | SpaceX | 5 | 3 | 40.0% | 2006 | 2009 | 600 kg |
| 210 | H-IIA 204 | Japan | National Space Development Adminstration | 5 | 0 | 100.0% | 2006 | 2021 | 10.0 t |
| 211 | Ariane 5ES/ATV | France | EADS Launch Vehicles (EADS LV) | 5 | 0 | 100.0% | 2008 | 2014 | 20.0 t |
| 212 | Atlas V 531 | United States | Lockheed Martin Astronautics | 5 | 0 | 100.0% | 2010 | 2022 | — |
| 213 | Antares 230 | United States | Orbital Sciences HIF, Mid-Atlantic Regional Spaceport | 5 | 0 | 100.0% | 2016 | 2019 | 6,250 kg |
| 214 | PSLV-DL | India | Vikram Sarabhai Space Center | 5 | 1 | 80.0% | 2019 | 2026 | 1,300 kg |
| 215 | Astra Rocket 3.3 | United States | Astra Space | 5 | 3 | 40.0% | 2021 | 2022 | 10 kg |
| 216 | Nuri | South Korea | Korea Aerospace Research Institute | 5 | 1 | 80.0% | 2021 | 2026 | — |
| 217 | Starship V2 | United States | SpaceX | 5 | 2 | 60.0% | 2025 | 2025 | 100.0 t |
| 218 | Atlas Agena A | United States | General Dynamics Astronautics | 4 | 2 | 50.0% | 1960 | 1961 | — |
| 219 | Scout X-1 | United States | Ling-Temco-Vought Missile Systems | 4 | 2 | 50.0% | 1960 | 1961 | 59 kg |
| 220 | Atlas Centaur | United States | General Dynamics Astronautics | 4 | 3 | 25.0% | 1963 | 1965 | — |
| 221 | Titan IIIA | United States | Martin-Denver | 4 | 1 | 75.0% | 1964 | 1965 | 4,100 kg |
| 222 | Thor Burner 1 | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 4 | 1 | 75.0% | 1965 | 1966 | 200 kg |
| 223 | UR-500 | Soviet Union | Khrunichev State Research and Production Center | 4 | 1 | 75.0% | 1965 | 1966 | 8,400 kg |
| 224 | Diamant A | France | Soci\'et\'e pour l'etude et la r\'ealisation d'engins ballistiques | 4 | 0 | 100.0% | 1965 | 1967 | 40 kg |
| 225 | Kosmos 11K65 | Soviet Union | Yangel KB | 4 | 2 | 50.0% | 1966 | 1968 | 1,500 kg |
| 226 | N-1 11A52 | Soviet Union | OKB-1 im. S.P. Korolev | 4 | 4 | 0.0% | 1969 | 1972 | 70.0 t |
| 227 | Mu-4S | Japan | Nissan (Solid propulsion plant) | 4 | 1 | 75.0% | 1970 | 1972 | 180 kg |
| 228 | Mu-3C | Japan | Nissan (Solid propulsion plant) | 4 | 1 | 75.0% | 1974 | 1979 | 195 kg |
| 229 | SLV-3 | India | Indian Space Research Organization | 4 | 1 | 75.0% | 1979 | 1983 | 42 kg |
| 230 | Mu-3S | Japan | Nissan (Solid propulsion plant) | 4 | 0 | 100.0% | 1980 | 1984 | 300 kg |
| 231 | K65M-RB | Soviet Union | PO Polyot | 4 | 0 | 100.0% | 1982 | 1984 | 1,500 kg |
| 232 | Atlas E/SGS-2 | United States | General Dynamics Astronautics | 4 | 0 | 100.0% | 1983 | 1985 | 861 kg |
| 233 | ASLV | India | Indian Space Research Organization | 4 | 2 | 50.0% | 1987 | 1994 | 150 kg |
| 234 | Commercial Titan 3 | United States | Martin Marietta/Denver | 4 | 1 | 75.0% | 1990 | 1992 | 14.5 t |
| 235 | Pegasus | United States | Orbital Sciences Corp./Chandler | 4 | 0 | 100.0% | 1990 | 1994 | 350 kg |
| 236 | Pegasus H | United States | Orbital Sciences Corp./Chandler | 4 | 0 | 100.0% | 1995 | 2000 | 350 kg |
| 237 | Shavit 1 | Israel | Israeli Aircraft Industries, Mabat factory | 4 | 2 | 50.0% | 1995 | 2004 | 230 kg |
| 238 | Delta 7320-10 | United States | McDonnell Douglas Astronautics/HB | 4 | 0 | 100.0% | 1999 | 2003 | — |
| 239 | Proton-K/Briz-M | Russia | Khrunichev State Research and Production Center | 4 | 1 | 75.0% | 1999 | 2003 | 21.0 t |
| 240 | Atlas 3B | United States | Lockheed Martin Astronautics | 4 | 0 | 100.0% | 2002 | 2005 | 8,620 kg |
| 241 | Zenit-3SLBF | Russia | Southern State Design Bureau | 4 | 0 | 100.0% | 2011 | 2017 | — |
| 242 | Chang Zheng 2D/YZ-3 | China | Shanghai Academy of Space Technology (CASC 8th Acad) | 4 | 0 | 100.0% | 2018 | 2024 | 3,400 kg |
| 243 | Chang Zheng 5B | China | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 4 | 0 | 100.0% | 2020 | 2022 | 25.0 t |
| 244 | Yinli-1 | China | Orienspace | 4 | 0 | 100.0% | 2024 | 2026 | 6,500 kg |
| 245 | New Glenn 7x2 | United States | Blue Origin Manufacturing Facility, Exploration Park | 4 | 1 | 66.7% | 2025 | 2026 | — |
| 246 | Thor Able I | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 3 | 2 | 33.3% | 1958 | 1958 | 50 kg |
| 247 | Atlas Able | United States | General Dynamics Astronautics | 3 | 3 | 0.0% | 1959 | 1960 | — |
| 248 | Scout X-2M | United States | Ling-Temco-Vought Missile Systems | 3 | 2 | 33.3% | 1962 | 1963 | 90 kg |
| 249 | Thor SLV-2 Agena B | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 3 | 0 | 100.0% | 1964 | 1965 | — |
| 250 | Thor Delta C1 | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 3 | 0 | 100.0% | 1966 | 1969 | 400 kg |
| 251 | Europa I | European Launcher Development Organisation | European Launcher Development Organization | 3 | 3 | 0.0% | 1968 | 1970 | 1,000 kg |
| 252 | Thor Delta N6 | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 3 | 1 | 66.7% | 1970 | 1971 | — |
| 253 | Soyuz 11A511L | Soviet Union | Progress Factory | 3 | 0 | 100.0% | 1970 | 1971 | 6,500 kg |
| 254 | Titan 33B | United States | Martin Marietta/Denver | 3 | 1 | 66.7% | 1971 | 1973 | 3,600 kg |
| 255 | Delta 0300 | United States | McDonnell Douglas Astronautics/HB | 3 | 1 | 66.7% | 1972 | 1973 | 1,000 kg |
| 256 | Delta 2313 | United States | McDonnell Douglas Astronautics/HB | 3 | 1 | 66.7% | 1974 | 1977 | 1,540 kg |
| 257 | Delta 2310 | United States | McDonnell Douglas Astronautics/HB | 3 | 0 | 100.0% | 1974 | 1981 | — |
| 258 | Diamant BP.4 | France | Soci\'et\'e pour l'etude et la r\'ealisation d'engins ballistiques | 3 | 0 | 100.0% | 1975 | 1975 | 150 kg |
| 259 | Atlas F/MSD | United States | General Dynamics Astronautics | 3 | 0 | 100.0% | 1976 | 1980 | 1,200 kg |
| 260 | Mu-3H | Japan | Nissan (Solid propulsion plant) | 3 | 0 | 100.0% | 1977 | 1978 | 300 kg |
| 261 | Delta 3910 | United States | McDonnell Douglas Astronautics/HB | 3 | 0 | 100.0% | 1980 | 1988 | — |
| 262 | Delta 3920 | United States | McDonnell Douglas Astronautics/HB | 3 | 0 | 100.0% | 1982 | 1986 | — |
| 263 | Proton-K/D-2 | Soviet Union | Khrunichev State Research and Production Center | 3 | 0 | 100.0% | 1988 | 1996 | 5,000 kg |
| 264 | Titan 402A/IUS | United States | Lockheed Martin Astronautics | 3 | 0 | 100.0% | 1989 | 1994 | — |
| 265 | Titan 404A | United States | Lockheed Martin Astronautics | 3 | 0 | 100.0% | 1992 | 1996 | 17.7 t |
| 266 | VLS-1 | Brazil | National Institute of Space Research | 3 | 2 | 0.0% | 1997 | 2003 | 120 kg |
| 267 | Athena-2 | United States | Lockheed Missiles and Space Co. | 3 | 1 | 66.7% | 1998 | 1999 | 2,065 kg |
| 268 | Delta 8930 | United States | Boeing Space Systems (HB) | 3 | 2 | 33.3% | 1998 | 2000 | 8,280 kg |
| 269 | Delta 7326-9.5 | United States | McDonnell Douglas Astronautics/HB | 3 | 0 | 100.0% | 1998 | 2001 | — |
| 270 | Delta 7425-9.5 | United States | McDonnell Douglas Astronautics/HB | 3 | 0 | 100.0% | 1998 | 2002 | — |
| 271 | Titan 404B | United States | Lockheed Martin Astronautics | 3 | 0 | 100.0% | 1999 | 2005 | 21.7 t |
| 272 | KT-1 | China | CASIC 4th Academy | 3 | 3 | 0.0% | 2002 | 2005 | 50 kg |
| 273 | Delta 4M | United States | Boeing Space Systems (HB) | 3 | 0 | 100.0% | 2003 | 2006 | 8,120 kg |
| 274 | Delta 7925H | United States | McDonnell Douglas Astronautics/HB | 3 | 0 | 100.0% | 2003 | 2007 | — |
| 275 | Delta 7920H | United States | McDonnell Douglas Astronautics/HB | 3 | 0 | 100.0% | 2003 | 2011 | — |
| 276 | Strela | Russia | NPO Mashinostroenie | 3 | 0 | 100.0% | 2003 | 2014 | 1,400 kg |
| 277 | Ariane 5G+ | France | EADS Launch Vehicles (EADS LV) | 3 | 0 | 100.0% | 2004 | 2004 | 10.0 t |
| 278 | H-IIA 2022 | Japan | National Space Development Adminstration | 3 | 0 | 100.0% | 2005 | 2007 | — |
| 279 | Atlas V 431 | United States | Lockheed Martin Astronautics | 3 | 0 | 100.0% | 2005 | 2016 | — |
| 280 | Naro-1 | South Korea | Korea Aerospace Research Institute | 3 | 2 | 33.3% | 2009 | 2013 | 100 kg |
| 281 | Delta 4M+(5,2) | United States | Boeing Space Systems (HB) | 3 | 0 | 100.0% | 2012 | 2018 | 11.7 t |
| 282 | Angara A5 | Russia | Khrunichev State Research and Production Center | 3 | 0 | 100.0% | 2014 | 2025 | 24.5 t |
| 283 | Chang Zheng 3C/YZ-1 | China | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 3 | 0 | 100.0% | 2015 | 2025 | — |
| 284 | Ariane 5ES | France | EADS Launch Vehicles (EADS LV) | 3 | 0 | 100.0% | 2016 | 2018 | 20.0 t |
| 285 | Atlas V N22 | United States | Lockheed Martin Astronautics | 3 | 0 | 100.0% | 2019 | 2024 | — |
| 286 | Qased | Iran | Iran, Islamic Republic of | 3 | 0 | 100.0% | 2020 | 2023 | — |
| 287 | SSLV | India | Indian Space Research Organization | 3 | 1 | 66.7% | 2022 | 2024 | 500 kg |
| 288 | Zhuque-2 | China | LandSpace Technology | 3 | 1 | 66.7% | 2022 | 2023 | — |
| 289 | Qaem-100 | Iran | Sepah-e Pasdaran-e Enghelab-e Eslami (Missile Forces) | 3 | 1 | 66.7% | 2023 | 2024 | — |
| 290 | Cheonlima-1 | North Korea | National Aerospace Development Administration | 3 | 2 | 33.3% | 2023 | 2023 | 50 kg |
| 291 | Kairos | Japan | Space One Co. Ltd. | 3 | 3 | 0.0% | 2024 | 2026 | 250 kg |
| 292 | Starship V1.0 | United States | SpaceX | 3 | 0 | 100.0% | 2024 | 2024 | 100.0 t |
| 293 | Chang Zheng 5B/YZ-2 | China | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 3 | 0 | 100.0% | 2024 | 2025 | 25.0 t |
| 294 | Ariane 64 | France | ArianeGroup | 3 | 0 | 100.0% | 2026 | 2026 | — |
| 295 | Starship V3 | United States | SpaceX | 3 | 0 | 100.0% | 2026 | 2026 | 100.0 t |
| 296 | Sputnik 8K71PS | Soviet Union | OKB-1 im. S.P. Korolev | 2 | 0 | 100.0% | 1957 | 1957 | 500 kg |
| 297 | Sputnik 8A91 | Soviet Union | OKB-1 im. S.P. Korolev | 2 | 1 | 50.0% | 1958 | 1958 | 500 kg |
| 298 | Thor Able II | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 2 | 1 | 50.0% | 1959 | 1960 | 50 kg |
| 299 | Thor Delta A | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 2 | 0 | 100.0% | 1962 | 1962 | 250 kg |
| 300 | Thor SLV-2A Agena B | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 2 | 0 | 100.0% | 1963 | 1966 | — |
| 301 | Polyot 11A59 | Soviet Union | OKB-1 im. S.P. Korolev | 2 | 0 | 100.0% | 1963 | 1964 | 2,250 kg |
| 302 | Thor Delta D | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 2 | 0 | 100.0% | 1964 | 1965 | 450 kg |
| 303 | Thor MG-18 | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 2 | 0 | 100.0% | 1965 | 1965 | 200 kg |
| 304 | Vostok-2A 11A510 | Soviet Union | OKB-1 im. S.P. Korolev | 2 | 0 | 100.0% | 1965 | 1966 | 3,600 kg |
| 305 | Uprated Saturn I | United States | NASA Marshall Space Flight Center | 2 | 0 | 100.0% | 1966 | 1966 | — |
| 306 | Thor Delta G | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 2 | 0 | 100.0% | 1966 | 1967 | — |
| 307 | Atlas Burner 2 | United States | General Dynamics Astronautics | 2 | 1 | 50.0% | 1968 | 1972 | — |
| 308 | Thor Delta L | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 2 | 1 | 50.0% | 1969 | 1972 | — |
| 309 | Chang Zheng 1 | China | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 2 | 0 | 100.0% | 1970 | 1971 | 250 kg |
| 310 | Black Arrow | United Kingdom | Royal Aircraft Establishment | 2 | 1 | 50.0% | 1970 | 1971 | — |
| 311 | R-36O 8K69M | Soviet Union | Yangel KB | 2 | 0 | 100.0% | 1970 | 1971 | — |
| 312 | Delta 0900 | United States | McDonnell Douglas Astronautics/HB | 2 | 0 | 100.0% | 1972 | 1972 | 1,300 kg |
| 313 | Delta 1604 | United States | McDonnell Douglas Astronautics/HB | 2 | 0 | 100.0% | 1972 | 1973 | — |
| 314 | Delta 1914 | United States | McDonnell Douglas Astronautics/HB | 2 | 0 | 100.0% | 1972 | 1973 | — |
| 315 | Chang Zheng 2 | China | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 2 | 1 | 50.0% | 1974 | 1975 | 2,200 kg |
| 316 | Scout F-1 | Italy | Ling-Temco-Vought Missile Systems | 2 | 1 | 50.0% | 1975 | 1975 | 192 kg |
| 317 | Delta 2913 | United States | McDonnell Douglas Astronautics/HB | 2 | 0 | 100.0% | 1975 | 1976 | 2,000 kg |
| 318 | Chang Zheng 4 | China | Shanghai Academy of Space Technology (CASC 8th Acad) | 2 | 0 | 100.0% | 1988 | 1990 | 1,650 kg |
| 319 | Shavit | Israel | Israeli Aircraft Industries, Mabat factory | 2 | 0 | 100.0% | 1988 | 1990 | 200 kg |
| 320 | Delta 4925-8 | United States | McDonnell Douglas Astronautics/HB | 2 | 0 | 100.0% | 1989 | 1990 | — |
| 321 | Delta 6920-10 | United States | McDonnell Douglas Astronautics/HB | 2 | 0 | 100.0% | 1990 | 1992 | — |
| 322 | Titan 405A | United States | Lockheed Martin Astronautics | 2 | 0 | 100.0% | 1990 | 1996 | 17.7 t |
| 323 | Pegasus/HAPS | United States | Orbital Sciences Corp./Chandler | 2 | 1 | 50.0% | 1991 | 1994 | 250 kg |
| 324 | Delta 7925-8 | United States | McDonnell Douglas Astronautics/HB | 2 | 0 | 100.0% | 1994 | 1996 | — |
| 325 | ARPA Taurus | United States | Orbital Sciences Corp./Chandler | 2 | 0 | 100.0% | 1994 | 1998 | 1,320 kg |
| 326 | Delta 7925-10 | United States | McDonnell Douglas Astronautics/HB | 2 | 0 | 100.0% | 1994 | 1996 | — |
| 327 | Shtil'-1 | Russia | Makeev Design Bureau | 2 | 0 | 100.0% | 1998 | 2006 | 430 kg |
| 328 | Athena-1 | United States | Lockheed Missiles and Space Co. | 2 | 0 | 100.0% | 1999 | 2001 | 820 kg |
| 329 | Taurus 2110 | United States | Orbital Sciences Corp./Chandler | 2 | 1 | 50.0% | 1999 | 2001 | 1,380 kg |
| 330 | Atlas 3A | United States | Lockheed Martin Astronautics | 2 | 0 | 100.0% | 2000 | 2004 | 8,620 kg |
| 331 | Delta 7920-10L | United States | McDonnell Douglas Astronautics/HB | 2 | 0 | 100.0% | 2002 | 2004 | — |
| 332 | Atlas V 521 | United States | Lockheed Martin Astronautics | 2 | 0 | 100.0% | 2003 | 2004 | 14.0 t |
| 333 | Delta 7925-10L | United States | McDonnell Douglas Astronautics/HB | 2 | 0 | 100.0% | 2006 | 2009 | — |
| 334 | Taurus 3110 | United States | Orbital Sciences Corp./Chandler | 2 | 2 | 0.0% | 2009 | 2011 | 1,380 kg |
| 335 | Unha-3 | North Korea | Korean People's Army | 2 | 1 | 50.0% | 2012 | 2012 | 50 kg |
| 336 | Antares 110 | United States | Orbital Sciences HIF, Mid-Atlantic Regional Spaceport | 2 | 0 | 100.0% | 2013 | 2013 | 4,600 kg |
| 337 | Kuaizhou | China | CASIC 4th Academy | 2 | 0 | 100.0% | 2013 | 2014 | 250 kg |
| 338 | Antares 120 | United States | Orbital Sciences HIF, Mid-Atlantic Regional Spaceport | 2 | 0 | 100.0% | 2014 | 2014 | 4,600 kg |
| 339 | SS-520 | Japan | Nissan (Solid propulsion plant) | 2 | 1 | 50.0% | 2017 | 2018 | — |
| 340 | GSLV Mk III | India | Indian Space Research Organization | 2 | 0 | 100.0% | 2017 | 2018 | — |
| 341 | PSLV-QL | India | Vikram Sarabhai Space Center | 2 | 0 | 100.0% | 2019 | 2019 | 1,300 kg |
| 342 | SLS Block 1 | United States | Boeing SLS Operations, NASA Michoud Assembly Facility | 2 | 0 | 100.0% | 2022 | 2026 | — |
| 343 | Vulcan Centaur VC2S | United States | United Launch Alliance, Decatur | 2 | 0 | 100.0% | 2024 | 2024 | 27.2 t |
| 344 | Chang Zheng 6C | China | Shanghai Academy of Space Technology (CASC 8th Acad) | 2 | 0 | 100.0% | 2024 | 2026 | 1,000 kg |
| 345 | Spectrum | Germany | Isar Aerospace Technologies GmbH | 2 | 1 | 50.0% | 2025 | 2026 | 1,000 kg |
| 346 | Vulcan Centaur VC4S | United States | United Launch Alliance, Decatur | 2 | 0 | 100.0% | 2025 | 2026 | 27.2 t |
| 347 | Zhuque-3 | China | LandSpace Technology | 2 | 0 | 100.0% | 2025 | 2026 | 12.0 t |
| 348 | Atlas B | United States | General Dynamics Astronautics | 1 | 0 | 100.0% | 1958 | 1958 | 68 kg |
| 349 | Thor Able III | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 1 | 0 | 100.0% | 1959 | 1959 | 100 kg |
| 350 | Atlas C Able | United States | General Dynamics Astronautics | 1 | 0 | — | 1959 | 1959 | 170 kg |
| 351 | Thor Able IV | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 1 | 0 | 100.0% | 1960 | 1960 | 100 kg |
| 352 | Blue Scout II | United States | Ling-Temco-Vought Missile Systems | 1 | 1 | 0.0% | 1961 | 1961 | 50 kg |
| 353 | Scout X-2 | United States | Ling-Temco-Vought Missile Systems | 1 | 1 | 0.0% | 1962 | 1962 | 76 kg |
| 354 | Scout X-3M | United States | Ling-Temco-Vought Missile Systems | 1 | 0 | 100.0% | 1963 | 1963 | 90 kg |
| 355 | Scout X-2B | United States | Ling-Temco-Vought Missile Systems | 1 | 1 | 0.0% | 1963 | 1963 | 90 kg |
| 356 | Atlas SLV-3 | United States | General Dynamics Astronautics | 1 | 0 | 100.0% | 1966 | 1966 | — |
| 357 | Atlas SLV-3 Agena B | United States | General Dynamics Astronautics | 1 | 0 | 100.0% | 1966 | 1966 | — |
| 358 | UR-500K/Blok D | Soviet Union | Khrunichev State Research and Production Center | 1 | 0 | 100.0% | 1967 | 1967 | 5,000 kg |
| 359 | SPARTA | United States | Chrysler Michigan Ordnance Missile Plant | 1 | 0 | 100.0% | 1967 | 1967 | 45 kg |
| 360 | Thor Delta J | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 1 | 0 | 100.0% | 1968 | 1968 | — |
| 361 | Thor Delta M6 | United States | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 1 | 0 | 100.0% | 1971 | 1971 | — |
| 362 | Europa II | European Launcher Development Organisation | European Launcher Development Organization | 1 | 1 | 0.0% | 1971 | 1971 | 1,160 kg |
| 363 | Delta 1913 | United States | McDonnell Douglas Astronautics/HB | 1 | 0 | 100.0% | 1973 | 1973 | — |
| 364 | Scout A-1 | United States | Ling-Temco-Vought Missile Systems | 1 | 0 | 100.0% | 1973 | 1973 | 121 kg |
| 365 | Delta 1900 | United States | McDonnell Douglas Astronautics/HB | 1 | 0 | 100.0% | 1973 | 1973 | — |
| 366 | Scout E-1 | United States | Ling-Temco-Vought Missile Systems | 1 | 0 | 100.0% | 1974 | 1974 | 200 kg |
| 367 | Atlas F/PTS | United States | General Dynamics Astronautics | 1 | 0 | 100.0% | 1974 | 1974 | 295 kg |
| 368 | Delta 1410 | United States | McDonnell Douglas Astronautics/HB | 1 | 0 | 100.0% | 1975 | 1975 | 1,000 kg |
| 369 | Delta 1910 | United States | McDonnell Douglas Astronautics/HB | 1 | 0 | 100.0% | 1975 | 1975 | — |
| 370 | Atlas F/Agena D | United States | General Dynamics Astronautics | 1 | 0 | 100.0% | 1978 | 1978 | — |
| 371 | Atlas F/OIS | United States | General Dynamics Astronautics | 1 | 0 | 100.0% | 1979 | 1979 | — |
| 372 | Atlas E/MSD | United States | General Dynamics Astronautics | 1 | 1 | 0.0% | 1980 | 1980 | 1,200 kg |
| 373 | Delta 3913 | United States | McDonnell Douglas Astronautics/HB | 1 | 0 | 100.0% | 1981 | 1981 | — |
| 374 | Atlas E/SVS | United States | General Dynamics Astronautics | 1 | 1 | 0.0% | 1981 | 1981 | 700 kg |
| 375 | Titan 34D/IUS | United States | Martin Marietta/Denver | 1 | 0 | 100.0% | 1982 | 1982 | — |
| 376 | Atlas E/OIS | United States | General Dynamics Astronautics | 1 | 0 | 100.0% | 1985 | 1985 | — |
| 377 | Energiya | Soviet Union | NPO Energiya | 1 | 1 | 0.0% | 1987 | 1987 | 88.0 t |
| 378 | Energiya/Buran | Soviet Union | NPO Energiya | 1 | 0 | 100.0% | 1988 | 1988 | 88.0 t |
| 379 | Delta 3920-8 | United States | McDonnell Douglas Astronautics/HB | 1 | 0 | 100.0% | 1989 | 1989 | — |
| 380 | Delta 5920-8 | United States | McDonnell Douglas Astronautics/HB | 1 | 0 | 100.0% | 1989 | 1989 | 3,850 kg |
| 381 | Delta 6920-8 | United States | McDonnell Douglas Astronautics/HB | 1 | 0 | 100.0% | 1990 | 1990 | — |
| 382 | Atlas E Altair | United States | General Dynamics Astronautics | 1 | 0 | 100.0% | 1990 | 1990 | — |
| 383 | Delta 6925-8 | United States | McDonnell Douglas Astronautics/HB | 1 | 0 | 100.0% | 1990 | 1990 | — |
| 384 | Start | Russia | Moscow Inst of Thermal Technology | 1 | 1 | 0.0% | 1995 | 1995 | 650 kg |
| 385 | LLV-1 | United States | Lockheed Missiles and Space Co. | 1 | 1 | 0.0% | 1995 | 1995 | 820 kg |
| 386 | Conestoga 1620 | United States | EER Systems Inc. SSI Division | 1 | 1 | 0.0% | 1995 | 1995 | 900 kg |
| 387 | Start-1.2 | Russia | Moscow Inst of Thermal Technology | 1 | 0 | 100.0% | 1997 | 1997 | 500 kg |
| 388 | LMLV-1 | United States | Lockheed Missiles and Space Co. | 1 | 0 | 100.0% | 1997 | 1997 | 820 kg |
| 389 | Delta 7920-8 | United States | McDonnell Douglas Astronautics/HB | 1 | 0 | 100.0% | 1997 | 1997 | 5,118 kg |
| 390 | Taurus 2210 | United States | Orbital Sciences Corp./Chandler | 1 | 0 | 100.0% | 1998 | 1998 | 1,380 kg |
| 391 | Paektusan 1 | North Korea | Korean People's Army | 1 | 1 | 0.0% | 1998 | 1998 | 50 kg |
| 392 | Zenit-2 11K77.05 | Russia | Southern State Design Bureau | 1 | 1 | 0.0% | 1998 | 1998 | 13.5 t |
| 393 | Delta 7426-9.5 | United States | McDonnell Douglas Astronautics/HB | 1 | 0 | 100.0% | 1999 | 1999 | — |
| 394 | Taurus 1110 | United States | Orbital Sciences Corp./Chandler | 1 | 0 | 100.0% | 2000 | 2000 | 1,320 kg |
| 395 | Titan 403B | United States | Lockheed Martin Astronautics | 1 | 0 | 100.0% | 2000 | 2000 | 21.7 t |
| 396 | Delta 7425-10 | United States | McDonnell Douglas Astronautics/HB | 1 | 0 | 100.0% | 2001 | 2001 | — |
| 397 | Taurus 3210 | United States | Orbital Sciences Corp./Chandler | 1 | 0 | 100.0% | 2004 | 2004 | 1,380 kg |
| 398 | Titan 405B | United States | Lockheed Martin Astronautics | 1 | 0 | 100.0% | 2005 | 2005 | 21.7 t |
| 399 | Volna | Russia | Makeev Design Bureau | 1 | 1 | 0.0% | 2005 | 2005 | — |
| 400 | Delta 7925-10C | United States | McDonnell Douglas Astronautics/HB | 1 | 0 | 100.0% | 2007 | 2007 | — |
| 401 | Zenit-2M | Russia | Southern State Design Bureau | 1 | 0 | 100.0% | 2007 | 2007 | 13.5 t |
| 402 | Unha-2 | North Korea | Korean People's Army | 1 | 1 | 0.0% | 2009 | 2009 | 50 kg |
| 403 | Minotaur IV+ | United States | Orbital Sciences Corp./Chandler | 1 | 0 | 100.0% | 2011 | 2011 | 1,735 kg |
| 404 | Zenit-2SB | Russia | Southern State Design Bureau | 1 | 0 | 100.0% | 2011 | 2011 | — |
| 405 | Minotaur V | United States | Orbital Sciences Corp./Chandler | 1 | 0 | 100.0% | 2013 | 2013 | 1,735 kg |
| 406 | Antares 130 | United States | Orbital Sciences HIF, Mid-Atlantic Regional Spaceport | 1 | 1 | 0.0% | 2014 | 2014 | 5,100 kg |
| 407 | Super Strypi | United States | Sandia Laboratories | 1 | 1 | 0.0% | 2015 | 2015 | 300 kg |
| 408 | Kwangmyongsong | North Korea | Korean People's Army | 1 | 0 | 100.0% | 2016 | 2016 | 50 kg |
| 409 | Chang Zheng 7/YZ-1A | China | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 1 | 0 | 100.0% | 2016 | 2016 | 13.5 t |
| 410 | Chang Zheng 5/YZ-2 | China | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 1 | 0 | 100.0% | 2016 | 2016 | 25.0 t |
| 411 | KT-2 | China | CASIC 4th Academy | 1 | 0 | 100.0% | 2017 | 2017 | 250 kg |
| 412 | Minotaur-C 3210 | United States | Orbital Sciences Corp./Chandler | 1 | 0 | 100.0% | 2017 | 2017 | 1,380 kg |
| 413 | Delta 4H/Star 48BV | United States | Boeing Space Systems (HB) | 1 | 0 | 100.0% | 2018 | 2018 | — |
| 414 | Zhuque-1 | China | CASIC 4th Academy | 1 | 1 | 0.0% | 2018 | 2018 | 400 kg |
| 415 | OS-M1 | China | OneSpace | 1 | 1 | 0.0% | 2019 | 2019 | — |
| 416 | Jielong-1 | China | China Long March Rocket Co. Ltd. | 1 | 0 | 100.0% | 2019 | 2019 | 150 kg |
| 417 | Astra Rocket 3.1 | United States | Astra Space | 1 | 1 | 0.0% | 2020 | 2020 | 10 kg |
| 418 | Astra Rocket 3.2 | United States | Astra Space | 1 | 1 | 0.0% | 2020 | 2020 | 10 kg |
| 419 | Proton-M | Russia | Khrunichev State Research and Production Center | 1 | 0 | 100.0% | 2021 | 2021 | 21.0 t |
| 420 | Angara A5/Persei | Russia | Khrunichev State Research and Production Center | 1 | 1 | 0.0% | 2021 | 2021 | 24.5 t |
| 421 | Atlas V 511 | United States | Lockheed Martin Astronautics | 1 | 0 | 100.0% | 2022 | 2022 | 14.0 t |
| 422 | RS1 | United States | ABL Space Systems | 1 | 1 | 0.0% | 2023 | 2023 | 1,300 kg |
| 423 | Terran 1 | United States | Relativity Space | 1 | 1 | 0.0% | 2023 | 2023 | 1,500 kg |
| 424 | Tianlong-2 | China | Beijing Tianbing Tech. Co. Ltd (Space Pioneer) | 1 | 0 | 100.0% | 2023 | 2023 | 2,000 kg |
| 425 | ADD TV2 | South Korea | Agency for Defense Development | 1 | 0 | 100.0% | 2023 | 2023 | — |
| 426 | Angara A5/Orion | Russia | Khrunichev State Research and Production Center | 1 | 0 | 100.0% | 2024 | 2024 | 24.5 t |
| 427 | NK Kerolox LV | North Korea | National Aerospace Development Administration | 1 | 1 | 0.0% | 2024 | 2024 | 50 kg |
| 428 | Eris Block 1 | Australia | Gilmour Space Technologies | 1 | 1 | 0.0% | 2025 | 2025 | 300 kg |
| 429 | Zoljanah | Iran | Iran, Islamic Republic of | 1 | 1 | 0.0% | 2025 | 2025 | 220 kg |
| 430 | H3-24W | Japan | Japan Aerospace Exploration Agency | 1 | 0 | 100.0% | 2025 | 2025 | — |
| 431 | HANBIT-NANO | South Korea | Innospace Co. Ltd. | 1 | 1 | 0.0% | 2025 | 2025 | 90 kg |
| 432 | Chang Zheng 12A | China | Shanghai Academy of Space Technology (CASC 8th Acad) | 1 | 0 | 100.0% | 2025 | 2025 | — |
| 433 | Gushenxing-2 | China | Galactic Energy Co. | 1 | 1 | 0.0% | 2026 | 2026 | 1,600 kg |
| 434 | Lijian-2 | China | Beijing CAS Space Exploration Tech. Co. Ltd. | 1 | 0 | 100.0% | 2026 | 2026 | 22.0 t |
| 435 | Tianlong-3 | China | Beijing Tianbing Tech. Co. Ltd (Space Pioneer) | 1 | 1 | 0.0% | 2026 | 2026 | — |
| 436 | Chang Zheng 12B | China | CASC Commercial Rocket YG | 1 | 0 | 100.0% | 2026 | 2026 | 20.0 t |
| 437 | HASTE | United States | Rocket Lab Ltd. | 1 | 0 | 100.0% | 2026 | 2026 | 150 kg |
| 438 | H3-30S | Japan | Japan Aerospace Exploration Agency | 1 | 0 | 100.0% | 2026 | 2026 | 4,000 kg |
| 439 | Chang Zheng 10B | China | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 1 | 0 | 100.0% | 2026 | 2026 | — |
| 440 | Vikram-1 | India | Skyroot Aerospace | 1 | 0 | 100.0% | 2026 | 2026 | — |
| 441 | Zhishenxing-1 | China | Galactic Energy Co. | 1 | 0 | 100.0% | 2026 | 2026 | 7,000 kg |
| 442 | H3-24L | Japan | Japan Aerospace Exploration Agency | 1 | 0 | 100.0% | 2026 | 2026 | — |
Source: GCAT launch list and launch vehicle tables (CC BY 4.0). Success rate counts launches GCAT codes as successes (OS) or failures (OF).