Country | Company | Vehicle | LEO | GTO | First Launch |
USA | Orbital ATK | Antares 200 | 7,000 kg | | 2016 |
USA | ULA | Atlas V 401 | 9,800 kg | 4,750 kg | 2002 |
USA | ULA | Atlas V 431 | 15,718 kg | 7,700 kg | 2005 |
USA | ULA | Atlas V 501 | 8,123 kg | 3,775 kg | 2010 |
USA | ULA | Atlas V 551 | 18,814 kg | 8,900 kg | 2006 |
USA | ULA | Delta IV M+(4,2) | 13,140 kg | 6,390 kg | 2002 |
USA | ULA | Delta IV M+(5,2) | 11,470 kg | 5,490 kg | 2012 |
USA | ULA | Delta IV M+(5,4) | 14,140 kg | 7,300 kg | 2009 |
USA | ULA | Delta IV Heavy | 28,790 kg | 14,220 kg | 2004 |
USA | SpaceX | Falcon 9 Full Thrust | 22,800 kg | Expendable: 8,300 kgReusable: 5,500 kg | 2015 |
USA | SpaceX | Falcon Heavy | 63,800 kg | 26,700 kg | 2018 |
USA | SpaceX | ITS | 550,000 kg | | 2022 |
USA | Virgin Orbit | LauncherOne | 500 kg | N/A | 2018 |
USA | Orbital ATK | Minotaur I | 580 kg | N/A | 2000 |
USA | Orbital ATK | Minotaur IV | 1600 kg | N/A | 2010 |
USA | Orbital ATK | Minotaur V | N/A | 532 kg | 2013 |
USA | Orbital ATK | Minotaur VI | 3,100 kg | 860 kg | TBD |
USA | Orbital ATK | Minotaur C | 1,458 kg | N/A | 1994 |
USA | Blue Origin | New Glenn | 45,000 kg | 13,000 kg | 2020 |
USA | Orbital ATK | Pegasus | 450 kg | N/A | |
USA | NASA | Space Launch System Block 1 | 70,000 kg | | 2019 |
USA | NASA | Space Launch System Block 1B | 105,000 kg | | 2021 |
USA | NASA | Space Launch System Block 2 | 130,000 kg | | 2029 |
USA | Vector Space Systems | Vector-R | 64 kg | N/A | 2018 |
USA | ULA | Vulcan Centaur | | | 2019 |
USA | ULA | Vulcan 561 ACES | | 15,059 kg | 2023 |
USA | ULA | Vulcan Heavy | | 23,000 kg | |
USA & New Zealand | Rocket Lab | Electron | 150 kg (SSO) | N/A | 2017 |
Europe | EADS Astrium | Ariane 5 ECA | 21,000 kg | 10,865 kg | 2002 |
Europe | EADS Astrium | Ariane 5 ES | N/A | 8,000 kg | 2008 |
Europe | ArianeGroup | Ariane 6 A62 | N/A | 4,500 kg | 2020 |
Europe | ArianeGroup | Ariane 6 A64 | 20,000 kg | 12,000 kg | 2020 |
Europe | ESA / ASI | Vega | 1,330 kg (SSO) | N/A | 2012 |
Europe | ESA / ASI | Vega C | 2,300 kg | N/A | 2019 |
Russia | Kruchinev | Proton M+ | 23,000 kg | 6,920 kg | 2007 |
Russia | Kruchinev | Proton Light | N/A | 3,600 kg | 2019 |
Russia | Kruchinev | Proton Medium | N/A | 5,000 kg | 2018 |
Russia | Eurockot | Rokot | 1,950 kg | N/A | 1994 |
Russia | Kruchinev | Strela | 1,400 kg | N/A | 2003 |
Russian | OKB-1 | Soyuz-2.1v | 2,850 kg | N/A | 2013 |
Russia | OKB-1 | Soyuz-FG | 6,900 kg | N/A | 2001 |
Russia | OKB-1 | Soyuz-2.1b | 8,200 kg | 2,400 kg | 2006 |
Russia | OKB-1 | Soyuz ST-B | 9,000 kg | 3,250 kg using Fregat-MT | 2011 |
Russia | Kruchinev | Angara 1.2 | 3,175 kg | N/A | 2014 |
Russia | Kruchinev | Angara A3 | 12,700 kg | 2,177 kg (Briz-M) | |
Russia | Kruchinev | Angara A5 | 21,772 kg | 4,899 kg (Briz-M)6,804 (KVTK) | 2014 |
Russia | RKK Energia | Soyuz 5 | 9,000 kg | | 2022 |
China | CALT, SAST | Long March 2 | 3,850-8,600 kg | 1,250 kg | 1982 |
China | CALT | Long March 3 | 6,000-11,500 kg | 2,600-5,500 kg | 1994 |
China | CALT | Long March 4 | 4,200 kg | 1,500 kg | 1999 |
China | CALT | Long March 5 | 25,000 kg | 14,000 kg | 2016 |
China | SAST | Long March 6 | 1,080 kg (SSO) | | 2015 |
China | CALT | Long March 7 | 13,500 kg | | 2016 |
China | CALT | Long March 8 | 7,600 kg | 2,500 kg | 2018 |
China | CALT | Long March 9 | 140,000 kg | 66,000 kg | 2028 |
China | CALT | Long March 11 | 700 kg | | 2015 |
India | ISRO | GSLV Mk II | 5,000 kg | 2,500 kg | 2010 |
India | ISRO | GSLV Mk III | 10,000 kg | 4,000 kg | 2014 |
India | ISRO | PSLV | 2,800-3,800 kg | 1,050-1,300 kg | 1993 |
India | ISRO | ULV | 15,000 kg | 6,000 kg | 2021 |
Japan | IHI | Epsilon | 1,200 kg | | 2013 |
Japan | Mitsubishi | H-IIA 202 | 10,000 kg | 4,100 kg | 2001 |
Japan | Mitsubishi | H-IIA 204 | | 6,000 kg | 2006 |
Japan | Mitsubishi | H-IIB | 16,500 kg | 8,000 kg | 2009 |
Japan | Mitsubishi | H-III | | 6,500 kg | 2020 |
Ukraine | Yuzhnoye / Yuzhma | Cyclone-4M | 5,000 kg | 1,000 kg | 2020 |
Ukraine | Yuzhnoye / RKK Energia | Zenit-3 | 7,000 kg | 3,750 – 6,100 kg | 1999 |