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Lanzadores
Cohetes de los satélites activos
Los lanzadores que pusieron en órbita los satélites que hoy siguen activos, con su capacidad según GCAT. El Falcon 9 domina por los lanzamientos de Starlink, pero la flota activa viajó en 179 modelos distintos.
179 cohetes
179 de 179
| # | Cohete | Fabricante | Satélites activos | Lanzamientos | Carga a LEO | Carga a GTO | Altura |
|---|---|---|---|---|---|---|---|
| 1 | Falcon 9 | SpaceX | 13.200 | 627 | 13,2 t | 4.850 kg | 71,0 m |
| 2 | Soyuz-2-1B | Progress Factory | 665 | 65 | 7.600 kg | — | 50,7 m |
| 3 | Atlas V 551 | Lockheed Martin Astronautics | 245 | 23 | — | 8.900 kg | 59,7 m |
| 4 | Chang Zheng 6A | Shanghai Academy of Space Technology (CASC 8th Acad) | 185 | 28 | 1.000 kg | — | 50,0 m |
| 5 | Chang Zheng 2D | Shanghai Academy of Space Technology (CASC 8th Acad) | 151 | 66 | 3.400 kg | — | 38,3 m |
| 6 | Electron | Rocket Lab Ltd. | 133 | 67 | 150 kg | — | 17,0 m |
| 7 | Chang Zheng 8A | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 119 | 12 | 8.400 kg | 2.800 kg | 50,5 m |
| 8 | Ariane 5ECA | EADS Launch Vehicles (EADS LV) | 112 | 63 | 10,0 t | 10,0 t | 57,7 m |
| 9 | Chang Zheng 2C | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 101 | 41 | 2.800 kg | — | 37,2 m |
| 10 | Ariane 64 | ArianeGroup | 100 | 3 | — | 11,5 t | 60,0 m |
| 11 | Proton-M/Briz-M | Khrunichev State Research and Production Center | 89 | 81 | 21,0 t | 6.320 kg | 53,0 m |
| 12 | Lijian-1 | CAS Institute of Mechanics | 85 | 14 | — | — | 50,0 m |
| 13 | Chang Zheng 3B | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 84 | 82 | — | 5.400 kg | 58,0 m |
| 14 | Jielong-3 | China Long March Rocket Co. Ltd. | 80 | 12 | 1.500 kg | — | 31,0 m |
| 15 | Chang Zheng 4B | Shanghai Academy of Space Technology (CASC 8th Acad) | 78 | 42 | 2.800 kg | 1.500 kg | 43,1 m |
| 16 | Soyuz-ST-B | Progress Factory | 76 | 17 | 7.600 kg | — | 50,7 m |
| 17 | LVM3 | Indian Space Research Organization | 76 | 6 | — | 4.000 kg | 42,4 m |
| 18 | Chang Zheng 8 | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 74 | 6 | 8.400 kg | 2.800 kg | 53,1 m |
| 19 | Chang Zheng 12 | Shanghai Academy of Space Technology (CASC 8th Acad) | 74 | 9 | — | 6.000 kg | 62,0 m |
| 20 | Gushenxing 1 | Galactic Energy Co. | 68 | 19 | 350 kg | — | 20,0 m |
| 21 | Soyuz-2-1A | Progress Factory | 64 | 25 | 7.600 kg | — | 50,7 m |
| 22 | Chang Zheng 4C | Shanghai Academy of Space Technology (CASC 8th Acad) | 58 | 41 | 2.800 kg | 1.500 kg | 43,1 m |
| 23 | Kuaizhou-1A | CASIC 4th Academy | 48 | 22 | 250 kg | — | 20,0 m |
| 24 | PSLV | Vikram Sarabhai Space Center | 46 | 16 | 1.300 kg | 1.000 kg | 44,4 m |
| 25 | Atlas V 401 | Lockheed Martin Astronautics | 42 | 31 | — | 4.750 kg | 58,3 m |
| 26 | Dnepr | Southern State Design Bureau | 41 | 15 | 4.500 kg | — | 34,3 m |
| 27 | Vega | ELV SpA | 39 | 16 | 1.500 kg | — | 30,1 m |
| 28 | Rokot | Khrunichev State Research and Production Center | 38 | 19 | 1.850 kg | — | 29,0 m |
| 29 | H-IIA 202 | National Space Development Adminstration | 37 | 28 | 10,0 t | 4.100 kg | 53,0 m |
| 30 | Nuri | Korea Aerospace Research Institute | 37 | 4 | — | — | 47,2 m |
| 31 | Chang Zheng 6 | Shanghai Academy of Space Technology (CASC 8th Acad) | 35 | 12 | 1.000 kg | — | 29,0 m |
| 32 | Falcon Heavy | SpaceX | 33 | 12 | 54,4 t | 22,2 t | 69,2 m |
| 33 | PSLV-XL | Vikram Sarabhai Space Center | 30 | 20 | 1.800 kg | 1.000 kg | 44,4 m |
| 34 | Chang Zheng 3B/YZ-1 | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 30 | 15 | — | 4.800 kg | 54,8 m |
| 35 | Chang Zheng 11 | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 30 | 14 | 500 kg | — | 20,0 m |
| 36 | Zhuque-2E | LandSpace Technology | 30 | 5 | 4.000 kg | — | 55,9 m |
| 37 | Chang Zheng 5B/YZ-2 | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 30 | 3 | 25,0 t | 14,0 t | 59,5 m |
| 38 | Starship V3 | SpaceX | 26 | 1 | 100,0 t | — | 123,0 m |
| 39 | Yinli-1 | Orienspace | 24 | 4 | 6.500 kg | — | 29,0 m |
| 40 | Space Shuttle | Rockwell International (Air Force Plant 42, Palmdale) | 23 | 18 | 24,4 t | — | 38,1 m |
| 41 | Ariane 5ECA+ | EADS Launch Vehicles (EADS LV) | 23 | 12 | 10,0 t | 10,0 t | 57,7 m |
| 42 | Chang Zheng 2C/YZ-1S | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 21 | 10 | 2.800 kg | — | 41,0 m |
| 43 | Kuaizhou-11 | Academy of Rocket Motors Technology (CASC 4th Academy) | 21 | 6 | — | — | 11,0 m |
| 44 | Zenit-3SL | Southern State Design Bureau | 20 | 20 | — | 5.000 kg | 59,6 m |
| 45 | Chang Zheng 2D/YZ-3 | Shanghai Academy of Space Technology (CASC 8th Acad) | 20 | 4 | 3.400 kg | — | 38,3 m |
| 46 | Pegasus XL/HAPS | Orbital Sciences Corp./Chandler | 18 | 4 | 350 kg | — | 17,4 m |
| 47 | Chang Zheng 7A | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 18 | 16 | 13,5 t | 7.000 kg | 55,0 m |
| 48 | Delta 7925-9.5 | McDonnell Douglas Astronautics/HB | 15 | 15 | — | — | 39,0 m |
| 49 | Angara-1.2 | Khrunichev State Research and Production Center | 15 | 5 | — | — | 42,8 m |
| 50 | Minotaur IV | Orbital Sciences Corp./Chandler | 14 | 6 | 1.735 kg | — | 23,9 m |
| 51 | Vega C | Avio s.p.A. | 14 | 7 | — | 3.300 kg | 35,0 m |
| 52 | Ariane 62 | ArianeGroup | 13 | 6 | — | 5.000 kg | 60,0 m |
| 53 | Pegasus XL | Orbital Sciences Corp./Chandler | 12 | 6 | 440 kg | — | 17,4 m |
| 54 | Delta 4M+(4,2) | Boeing Space Systems (HB) | 12 | 11 | 10,4 t | 5.845 kg | 66,2 m |
| 55 | Atlas V 421 | Lockheed Martin Astronautics | 12 | 9 | — | 6.890 kg | 58,3 m |
| 56 | Delta 4H | Boeing Space Systems (HB) | 12 | 12 | — | — | 70,7 m |
| 57 | Ariane 5ES | EADS Launch Vehicles (EADS LV) | 12 | 3 | 20,0 t | 6.200 kg | 45,7 m |
| 58 | Chang Zheng 3C | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 11 | 11 | — | 4.800 kg | 54,8 m |
| 59 | Atlas V 541 | Lockheed Martin Astronautics | 11 | 9 | — | 7.700 kg | 60,0 m |
| 60 | Kosmos 11K65M | PO Polyot | 10 | 10 | 1.500 kg | — | 32,4 m |
| 61 | Chang Zheng 3A | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 9 | 9 | — | 2.300 kg | 52,5 m |
| 62 | Soyuz-ST-A | Progress Factory | 9 | 7 | 7.600 kg | — | 50,7 m |
| 63 | GSLV Mk II | Vikram Sarabhai Space Center | 9 | 9 | — | 2.500 kg | 50,1 m |
| 64 | Chang Zheng 6C | Shanghai Academy of Space Technology (CASC 8th Acad) | 9 | 2 | 1.000 kg | — | 29,0 m |
| 65 | Delta 4M+(5,4) | Boeing Space Systems (HB) | 8 | 8 | 11,7 t | 6.565 kg | 70,7 m |
| 66 | Titan 401A/Centaur | Lockheed Martin Astronautics | 7 | 7 | — | — | 63,1 m |
| 67 | Atlas V 411 | Lockheed Martin Astronautics | 7 | 6 | — | 5.950 kg | 58,3 m |
| 68 | Delta 7420-10C | McDonnell Douglas Astronautics/HB | 7 | 6 | — | — | 39,0 m |
| 69 | Soyuz-2-1V | Progress Factory | 7 | 5 | 2.800 kg | — | 41,1 m |
| 70 | Proton-M/DM-3 | Khrunichev State Research and Production Center | 7 | 6 | 21,0 t | 4.500 kg | 53,0 m |
| 71 | Epsilon | Japan Aerospace Exploration Agency | 7 | 3 | — | 500 kg | 26,0 m |
| 72 | Chang Zheng 5 | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 7 | 7 | 25,0 t | 14,0 t | 59,5 m |
| 73 | Vulcan Centaur VC4S | United Launch Alliance, Decatur | 7 | 2 | 27,2 t | 15,3 t | 67,0 m |
| 74 | Atlas IIA | Lockheed Martin Astronautics | 6 | 6 | 7.316 kg | 3.066 kg | 47,4 m |
| 75 | Delta 7920-10C | McDonnell Douglas Astronautics/HB | 6 | 5 | — | — | 39,0 m |
| 76 | Proton-M/DM-2 | Khrunichev State Research and Production Center | 6 | 3 | 21,0 t | 4.500 kg | 53,0 m |
| 77 | Zenit-3SLB | Southern State Design Bureau | 6 | 6 | — | 5.000 kg | 59,6 m |
| 78 | Atlas V 531 | Lockheed Martin Astronautics | 6 | 5 | — | 7.700 kg | 60,0 m |
| 79 | Minotaur-C 3210 | Orbital Sciences Corp./Chandler | 6 | 1 | 1.380 kg | — | 31,6 m |
| 80 | H3-22S | Japan Aerospace Exploration Agency | 6 | 5 | — | — | 57,0 m |
| 81 | Atlas IIAS | Lockheed Martin Astronautics | 5 | 5 | 8.618 kg | 3.719 kg | 47,4 m |
| 82 | Titan 401B/Centaur | Lockheed Martin Astronautics | 5 | 5 | — | 9.000 kg | 62,2 m |
| 83 | Proton-K/DM-2M | Khrunichev State Research and Production Center | 5 | 5 | 5.000 kg | 4.350 kg | 57,2 m |
| 84 | Soyuz-FG | Progress Factory | 5 | 5 | 7.200 kg | — | 46,0 m |
| 85 | Delta 7925-10C | McDonnell Douglas Astronautics/HB | 5 | 1 | — | — | 38,9 m |
| 86 | Atlas V 501 | Lockheed Martin Astronautics | 5 | 3 | — | 3.775 kg | 58,3 m |
| 87 | Firefly Alpha | Firefly Aerospace | 5 | 1 | 1.000 kg | — | 13,7 m |
| 88 | H3-24W | Japan Aerospace Exploration Agency | 5 | 1 | — | 6.500 kg | 63,0 m |
| 89 | Spectrum | Isar Aerospace Technologies GmbH | 5 | 1 | 1.000 kg | — | 28,0 m |
| 90 | Ariane 40 | Aerospatiale/Les Mureaux | 4 | 2 | 2.740 kg | — | 58,4 m |
| 91 | Minotaur I | Orbital Sciences Corp./Chandler | 4 | 2 | 340 kg | — | 19,2 m |
| 92 | Ariane 44L | Aerospatiale/Les Mureaux | 4 | 4 | — | 4.820 kg | 58,4 m |
| 93 | Atlas 3B | Lockheed Martin Astronautics | 4 | 3 | 8.620 kg | 4.060 kg | 53,6 m |
| 94 | Ariane 5GS | EADS Launch Vehicles (EADS LV) | 4 | 4 | 10,0 t | 6.200 kg | 45,7 m |
| 95 | Shavit 2 | Israeli Aircraft Industries, Mabat factory | 4 | 4 | 230 kg | — | 18,0 m |
| 96 | H-IIA 204 | National Space Development Adminstration | 4 | 4 | 10,0 t | 4.100 kg | 53,0 m |
| 97 | PSLV-DL | Vikram Sarabhai Space Center | 4 | 3 | 1.300 kg | 1.000 kg | 44,4 m |
| 98 | H3-30S | Japan Aerospace Exploration Agency | 4 | 1 | 4.000 kg | — | 57,0 m |
| 99 | Atlas SLV-3 Agena D | General Dynamics Astronautics | 3 | 2 | — | 850 kg | 32,1 m |
| 100 | Proton-K/DM-2 | Khrunichev State Research and Production Center | 3 | 2 | 5.000 kg | 4.350 kg | 57,2 m |
| 101 | Delta 7920-10 | McDonnell Douglas Astronautics/HB | 3 | 3 | 5.118 kg | — | 39,0 m |
| 102 | Ariane 5G | EADS Launch Vehicles (EADS LV) | 3 | 3 | 10,0 t | 6.200 kg | 45,7 m |
| 103 | Delta 4M | Boeing Space Systems (HB) | 3 | 3 | 8.120 kg | 4.210 kg | 63,0 m |
| 104 | Atlas V 431 | Lockheed Martin Astronautics | 3 | 3 | — | 7.700 kg | 59,1 m |
| 105 | Delta 4M+(5,2) | Boeing Space Systems (HB) | 3 | 3 | 11,7 t | 6.565 kg | 70,7 m |
| 106 | Chang Zheng 5B | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 3 | 3 | 25,0 t | 14,0 t | 59,5 m |
| 107 | Simorgh | Iran, Islamic Republic of | 3 | 1 | 50 kg | — | 27,0 m |
| 108 | Chang Zheng 2F | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 3 | 2 | 9.200 kg | 3.500 kg | 51,2 m |
| 109 | Lijian-2 | Beijing CAS Space Exploration Tech. Co. Ltd. | 3 | 1 | 22,0 t | — | 56,0 m |
| 110 | Thorad SLV-2G Agena D | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 2 | 2 | 1.500 kg | — | 32,9 m |
| 111 | Titan IIIE | Martin Marietta/Denver | 2 | 2 | 14,0 t | — | 48,8 m |
| 112 | Ariane 44LP | Aerospatiale/Les Mureaux | 2 | 2 | — | 4.220 kg | 58,4 m |
| 113 | Proton-K | Khrunichev State Research and Production Center | 2 | 2 | 21,0 t | — | 50,0 m |
| 114 | Delta 7920-10L | McDonnell Douglas Astronautics/HB | 2 | 2 | — | — | 40,0 m |
| 115 | Delta 7320-10C | McDonnell Douglas Astronautics/HB | 2 | 2 | — | — | 38,9 m |
| 116 | Chang Zheng 3C/YZ-1 | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 2 | 2 | — | 4.800 kg | 54,8 m |
| 117 | GSLV Mk III | Indian Space Research Organization | 2 | 2 | — | 4.000 kg | 42,4 m |
| 118 | PSLV-QL | Vikram Sarabhai Space Center | 2 | 2 | 1.300 kg | 1.000 kg | 44,4 m |
| 119 | Atlas V 511 | Lockheed Martin Astronautics | 2 | 1 | 14,0 t | 6.475 kg | 59,7 m |
| 120 | Chang Zheng 7 | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 2 | 2 | 13,5 t | 7.000 kg | 53,1 m |
| 121 | Angara A5 | Khrunichev State Research and Production Center | 2 | 1 | 24,5 t | 5.400 kg | 42,8 m |
| 122 | New Glenn 7x2 | Blue Origin Manufacturing Facility, Exploration Park | 2 | 1 | — | — | 98,0 m |
| 123 | SLS Block 1 | Boeing SLS Operations, NASA Michoud Assembly Facility | 2 | 2 | — | — | 98,1 m |
| 124 | Chang Zheng 12B | CASC Commercial Rocket YG | 2 | 1 | 20,0 t | — | 72,0 m |
| 125 | Vikram-1 | Skyroot Aerospace | 2 | 1 | — | — | 24,0 m |
| 126 | Thor Ablestar | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 1 | 1 | 150 kg | — | 23,8 m |
| 127 | Titan IIIA | Martin-Denver | 1 | 1 | 4.100 kg | — | 42,0 m |
| 128 | Thor SLV-2 Agena D | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 1 | 1 | — | — | 27,2 m |
| 129 | Thor Delta C | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 1 | 1 | 400 kg | 81 kg | 27,5 m |
| 130 | Thor SLV-2 Agena B | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 1 | 1 | — | — | 27,2 m |
| 131 | Scout B | Ling-Temco-Vought Missile Systems | 1 | 1 | 143 kg | — | 22,0 m |
| 132 | Titan IIIC | Martin Marietta/Denver | 1 | 1 | 13,3 t | 3.000 kg | 38,3 m |
| 133 | Thor Delta E1 | Douglas Aircraft Corp. Missiles and Space Systems Division (MSSD) | 1 | 1 | 540 kg | 150 kg | 28,0 m |
| 134 | Mu-4S | Nissan (Solid propulsion plant) | 1 | 1 | 180 kg | — | 23,6 m |
| 135 | Black Arrow | Royal Aircraft Establishment | 1 | 1 | — | — | 12,9 m |
| 136 | Delta 0300 | McDonnell Douglas Astronautics/HB | 1 | 1 | 1.000 kg | — | 34,0 m |
| 137 | Delta 2310 | McDonnell Douglas Astronautics/HB | 1 | 1 | — | — | 35,0 m |
| 138 | Atlas SLV-3D Centaur | General Dynamics Astronautics | 1 | 1 | — | 1.900 kg | 40,3 m |
| 139 | Atlas F | General Dynamics Astronautics | 1 | 1 | 1.700 kg | — | 20,0 m |
| 140 | Ariane 1 | Aerospatiale/Les Mureaux | 1 | 1 | — | 1.400 kg | 47,4 m |
| 141 | Delta 3920 | McDonnell Douglas Astronautics/HB | 1 | 1 | — | — | 36,0 m |
| 142 | Atlas E | General Dynamics Astronautics | 1 | 1 | 1.700 kg | — | 20,0 m |
| 143 | Atlas E/OIS | General Dynamics Astronautics | 1 | 1 | — | — | 28,7 m |
| 144 | Titan 34D/Transtage | Martin Marietta/Denver | 1 | 1 | — | 5.000 kg | 50,0 m |
| 145 | Atlas G Centaur | General Dynamics Astronautics | 1 | 1 | 3.630 kg | 2.400 kg | 41,8 m |
| 146 | Vostok 8A92M | Progress Factory | 1 | 1 | 1.280 kg | — | 38,8 m |
| 147 | Pegasus | Orbital Sciences Corp./Chandler | 1 | 1 | 350 kg | — | 15,5 m |
| 148 | Atlas I | Lockheed Martin Astronautics | 1 | 1 | — | 2.250 kg | 41,8 m |
| 149 | Delta 7925-10 | McDonnell Douglas Astronautics/HB | 1 | 1 | — | — | 38,9 m |
| 150 | Atlas II | Lockheed Martin Astronautics | 1 | 1 | 6.580 kg | 2.770 kg | 45,0 m |
| 151 | H-II | MHI Aerospace Systems, Tobishima Plant | 1 | 1 | 10,1 t | 3.930 kg | 49,0 m |
| 152 | Delta 7925 | McDonnell Douglas Astronautics/HB | 1 | 1 | — | 1.816 kg | 39,7 m |
| 153 | Delta 7920-8 | McDonnell Douglas Astronautics/HB | 1 | 1 | 5.118 kg | — | 39,0 m |
| 154 | Taurus 2210 | Orbital Sciences Corp./Chandler | 1 | 1 | 1.380 kg | — | 29,7 m |
| 155 | Zenit-2 | Southern State Design Bureau | 1 | 1 | 13,5 t | — | 57,0 m |
| 156 | Pegasus H | Orbital Sciences Corp./Chandler | 1 | 1 | 350 kg | — | 15,5 m |
| 157 | Athena-1 | Lockheed Missiles and Space Co. | 1 | 1 | 820 kg | — | 18,9 m |
| 158 | Proton-K/17S40 | Khrunichev State Research and Production Center | 1 | 1 | 5.000 kg | 4.350 kg | 57,2 m |
| 159 | Titan II SLV | Martin-Denver | 1 | 1 | 1.900 kg | — | 34,6 m |
| 160 | Atlas 3A | Lockheed Martin Astronautics | 1 | 1 | 8.620 kg | 4.060 kg | 52,8 m |
| 161 | Ariane 5G+ | EADS Launch Vehicles (EADS LV) | 1 | 1 | 10,0 t | 6.200 kg | 45,7 m |
| 162 | Titan 404B | Lockheed Martin Astronautics | 1 | 1 | 21,7 t | — | 54,0 m |
| 163 | M-V | Nissan (Solid propulsion plant) | 1 | 1 | 1.800 kg | — | 30,7 m |
| 164 | Delta 7925-10L | McDonnell Douglas Astronautics/HB | 1 | 1 | — | — | 38,9 m |
| 165 | Delta 7920H | McDonnell Douglas Astronautics/HB | 1 | 1 | — | 1.816 kg | 39,7 m |
| 166 | Soyuz-U-PVB | Progress Factory | 1 | 1 | 5.000 kg | — | 42,5 m |
| 167 | Zenit-3SLBF | Southern State Design Bureau | 1 | 1 | — | 5.000 kg | 59,6 m |
| 168 | Chang Zheng 5/YZ-2 | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 1 | 1 | 25,0 t | 14,0 t | 59,5 m |
| 169 | Delta 4H/Star 48BV | Boeing Space Systems (HB) | 1 | 1 | — | — | 70,7 m |
| 170 | Proton-M | Khrunichev State Research and Production Center | 1 | 1 | 21,0 t | 4.500 kg | 53,0 m |
| 171 | Cheonlima-1 | National Aerospace Development Administration | 1 | 1 | 50 kg | — | 25,0 m |
| 172 | ADD TV2 | Agency for Defense Development | 1 | 1 | — | — | 20,6 m |
| 173 | Zhuque-2 | LandSpace Technology | 1 | 1 | — | — | 49,5 m |
| 174 | Vulcan Centaur VC2S | United Launch Alliance, Decatur | 1 | 1 | 27,2 t | 15,3 t | 67,0 m |
| 175 | SSLV | Indian Space Research Organization | 1 | 1 | 500 kg | — | 34,0 m |
| 176 | Shuang Quxian 1 | Beijing Interstellar Glory Space Tech. Co. Ltd. | 1 | 1 | — | — | 8,4 m |
| 177 | Chang Zheng 10B | Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) | 1 | 1 | — | — | 70,2 m |
| 178 | Zhuque-3 | LandSpace Technology | 1 | 1 | 12,0 t | — | 66,1 m |
| 179 | H3-24L | Japan Aerospace Exploration Agency | 1 | 1 | — | 6.500 kg | 63,0 m |
Lanzadores y sus características: tabla de vehículos de GCAT (CC BY 4.0). Capacidades nominales del modelo.