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Vehicle | Origin | Manufacturer | Height | Mass to ... (kg) | Reuse | Launches
(+ suborbital) |
Launch Site (s) | Date of flight | |||
---|---|---|---|---|---|---|---|---|---|---|---|
LEO | GTO | Other | First | Last | |||||||
Antares 110–130 | United States | Orbital | 40.5-41.9 m | 5,100 [1] | 1,500 to SSO | No | 5 [1] | 2013 | 2014 | ||
Antares 230 / 230+ | United States | Northrop Grumman | 42.5 m | 8,200 [1] | 3,000 to SSO [a] | No | 13 | 2016 | 2023 | ||
Ariane 1 | Europe | Aérospatiale | 49.1 m | 1,830 [2] | No | 11 [2] | 1979 | 1986 | |||
Ariane 2 | Europe | Aérospatiale | 49.1 m | 2,270 [2] | No | 6 [2] | 1986 | 1989 | |||
Ariane 3 | Europe | Aérospatiale | 49.1 m | 2,650 [2] | No | 11 [2] | 1984 | 1989 | |||
Ariane 4 40 | Europe | Aérospatiale | 58.7 m | 4,600 [2] | 2,105 | 2,740 to SSO | No | 7 [2] | 1990 | 1999 | |
Ariane 4 42L | Europe | Aérospatiale | 58.7 m | 7,000 [2] | 3,480 | 4,500 to SSO | No | 13 [2] | 1993 | 2002 | |
Ariane 4 42P | Europe | Aérospatiale | 58.7 m | 6,000 [2] | 2,930 | 3,400 to SSO | No | 15 [2] | 1990 | 2002 | |
Ariane 4 44L | Europe | Aérospatiale | 58.7 m | 7,000 [2] | 4,720 | 6,000 to SSO | No | 40 [2] | 1989 | 2003 | |
Ariane 4 44LP | Europe | Aérospatiale | 58.7 m | 7,000 [2] | 4,220 | 5,000 to SSO | No | 26 [2] | 1988 | 2001 | |
Ariane 4 44P | Europe | Aérospatiale | 58.7 m | 6,500 [2] | 3,465 | 4,100 to SSO | No | 15 [2] | 1991 | 2001 | |
Ariane 5 G | Europe | EADS Astrium | 47.5 m | 18,000 [3] | 6,900 [3] | No | 16 [3] | 1996 | 2003 | ||
Ariane 5 G+ | Europe | EADS Astrium | 47.8 m | 7,100 [3] | No | 3 [3] | 2004 | 2004 | |||
Ariane 5 GS | Europe | EADS Astrium | 47.8 m | 16,000 [4] | 6,600 [3] | No | 6 [3] | 2005 | 2009 [5] | ||
Ariane 5 ES | Europe | EADS Astrium | 50.7 m | 21,000 [6] | 8,000 [3] | No | 8 [3] | 2008 | 2018 | ||
Ariane 5 ECA | Europe | EADS Astrium | 52.6 m | 21,000 [6] | 11,210 [7] | No | 84 | 2002 | 2023 | ||
ASLV | India | ISRO [8] | 23.5 m | 150 [9] | No | 4 [9] | 1987 | 1994 | |||
Athena I LLV-1 | United States | Lockheed Martin | 18.4 m | 500 | No | 1 | 1995 | 1995 | |||
Athena I | United States | Lockheed Martin | 18.9 m | 795 [10] | 515 | No | 3 | 1997 | 2001 | ||
Athena II | United States | Lockheed Martin | 28.2 m | 1,800 [11] | No | 3 [12] | 1998 | 1999 [13] | |||
Black Arrow | United Kingdom | RAE | 13 m | 73 [14] | No | 2 (+2) | 1969 [b] | 1971 | |||
Blue Scout II | United States | Vought | 24 m | 30 | No | 3 | 1961 | 1961 | |||
Ceres-1 (1) [c] | China | Galactic Energy | 18.5 m | 350 | No | 1 | 2020 | 2020 | |||
Ceres-1 (2) [c] | China | Galactic Energy | 19.5 m | 400 | No | 1 | 2021 | 2021 | |||
Commercial Titan III | United States | Martin Marietta | 47.3 m | 13,100 [15] | No | 4 | 1990 | 1992 | |||
Conestoga 1620 | United States | Space Services | 15.2 m | 1179 | No | 1 | 1995 | 1995 | |||
Diamant A | France | SEREB | 18.9 m | 80 | No | 4 | 1965 | 1967 | |||
Diamant B | France | SEREB | 23.5 m | 115 | No | 5 | 1970 | 1973 | |||
Diamant BP4 | France | SEREB | 21.6 m | 153 | No | 3 | 1975 | 1975 | |||
Dnepr | Ukraine | Yuzhmash | 34.3 m | 3,700 [16] | No | 22 [16] | 1999 | 2015 [17] | |||
Energia [d] | Soviet Union | NPO Energia | 58.8 m | 105,000 | 20,000 to
GEO
[18]
32,000 to TLI [18] |
No | 1 (failed to orbit) | 1987 | 1987 | ||
Energia- Buran | Soviet Union | NPO Energia | 58.8 m | 30,000 [18] [e] | Yes | 1 | 1988 | 1988 | |||
Epsilon | Japan | IHI [19] | 24.4 m | 1,200 | N/A | 450 to SSO | No | 1 | 2013 | 2022 | |
Epsilon (enhanced) | Japan | IHI [19] | 26 m | 1,500 [20] | N/A | 590 to SSO [20] | No | 6 [20] | |||
Europa I | Europe | ELDO | 31.7 m | 1,440 | 200 | No | 3 | 1968 | 1970 | ||
Europa II | Europe | ELDO | 31.7 m | 360 | No | 1 | 1971 | 1971 | |||
Falcon 1 | United States | SpaceX | 21 m | 470 [21] | No | 5 [21] | 2006 | 2009 | |||
Falcon 9 v1.0 | United States | SpaceX | 54.9 m | 9,000 | 3,400 | No | 5 | 2010 | 2013 | ||
Falcon 9 v1.1 | United States | SpaceX | 68.4 m | 13,150 [22] [f] | 4,850 [22] | No | 15 [23] | 2013 | 2016 | ||
Falcon 9 Full Thrust | United States | SpaceX |
70.8 m |
17,400 [24] | 5,500 [24] | 9,600 to polar [25] | Yes | 36 | 2015 | 2018 | |
22,800 [24] | 8,300 [24] | No | |||||||||
Feng Bao 1 | China | Shanghai Bureau No.2 | 33 m | 2,500 [26] | No | 8 (+3) [27] | 1972 | 1981 | |||
GSLV Mk.I(a) | India | ISRO | 49.1 m | 5,000 [28] | 1,540 [29] | No | 1 [29] | 2001 | 2001 | ||
GSLV Mk.I(b) | India | ISRO | 49.1 m | 5,000 [28] | 2,150 [29] | No | 4 [29] | 2003 | 2007 | ||
GSLV Mk.I(c) | India | ISRO | 49.1 m | 5,000 [28] | No | 1 [29] | 2010 | 2010 | |||
H-I | Japan | Mitsubishi | 42 m | 1,400 [30] | No | 9 | 1986 | 1992 | |||
H-II / IIS | Japan | Mitsubishi | 49 m | 10,060 [31] | 4,000 [32] | No | 7 [32] | 1994 | 1999 | ||
H-IIA 204 | Japan | Mitsubishi | 53 m | 15,000 | 5,950 [33]: 48 | No | 5 [34] | 2006 | 2021 | ||
H-IIA 2022 | Japan | Mitsubishi | 53 m | 4,500 [34] | No | 3 [34] | 2005 | 2007 | |||
H-IIA 2024 | Japan | Mitsubishi | 57 m | 11,000 [35] | 5,000 [34] | No | 7 [34] | 2002 | 2008 | ||
H-IIB | Japan | Mitsubishi | 56.6 m | 16,500 ( ISS) [36] | 8,000 | No | 8 [37] | 2009 | 2020 | ||
Hyperbola-1 (1) [g] | China | i-Space | 20.9 m | 260 | No | 1 | 2019 | 2019 | |||
Juno I | United States | Chrysler | 21.2 m | 11 | No | 1 | 1958 | 1959 | |||
Juno II | United States | Chrysler | 24 m | 41 | 6 to TLI | No | 10 | 1958 | 1961 | ||
Kaituozhe-1 | China | CALT | 13.6 m | 40 | No | 2 | 2002 | 2003 | |||
Kaituozhe-2 | China | CASC | 16.8 m | 800 [38] | No | 1 [38] | 2017 | 2017 | |||
Kosmos | Soviet Union | NPO Polyot | 29.6 m | 350 | No | 38 | 1961 | 1967 | |||
Kosmos-1 | Soviet Union | NPO Polyot | 26.3 m | 1,400 | No | 8 | 1964 | 1965 | |||
Kosmos-2 | Soviet Union | NPO Polyot | 31 m | 300 | No | 127 | 1965 | 1977 | |||
Kosmos-3 | Soviet Union | NPO Polyot | 32.4 m | 1,400 | No | 6 | 1966 | 1968 | |||
Kosmos-3M | Soviet Union | NPO Polyot | 32.4 m | 1,500 [39] | No | 445 | 1967 | 2010 | |||
Kosmos-3MRB | Soviet Union | NPO Polyot | 32.4 m | 1,500 | No | 10 | 1980 | 1988 | |||
Lambda 4S | Japan | Nissan Motors [40] | 16.5 m | 26 [41] | No | 5 | 1966 | 1970 | |||
LauncherOne | United States | Virgin Orbit | 21.3 m | 500 | 300 to SSO | No | 6 | 2020 | 2023 | ||
Long March 1 | China | CALT | 29.9 m | 300 [42] | No | 2 [43] | 1970 | 1971 | |||
Long March 1D | China | CALT | 28.2 m | 740 [44] | No | 0 (+3) [43] | 1995 [h] | 2002 | |||
Long March 2A | China | CALT | 32 m | 2,000 [45] | No | 4 [46] | 1974 | 1978 | |||
Long March 2E | China | CALT | 49.7 m | 9,200 [46] | No | 7 [46] | 1990 | 1995 | |||
Long March 3 | China | CALT | 43.3 m | 5,000 [47] | No | 13 [47] | 1984 | 2000 | |||
Long March 3B | China | CALT | 54.8 m | 11,200 [48] | 5,100 | 5,700 to SSO | No | 12 [47] | 1996 | 2012 | |
Long March 4A | China | CALT | 41.9 m | 4,000 | No | 2 [49] | 1988 | 1990 | |||
M-V | Japan |
Nissan Motors
[40] (1997–2000)
IHI Aerospace [19] (2000–2006) |
30.8 m | 1,850 [41] | No | 7 | 1997 | 2006 | |||
Molniya | Soviet Union | RSC Energia | 43.4 m | 1,800 [50] | No | 40 [51] | 1960 | 1967 | |||
Molniya-M | Soviet Union | RSC Energia | 43.4 m | 2,400 [52] | No | 280 [53] | 1965 | 2010 | |||
Mu-4S | Japan | Nissan Motors [40] | 23.6 m | 180 [41] | No | 4 | 1971 | 1972 | |||
Mu-3C | Japan | Nissan Motors [40] | 20.3 m | 195 [41] | No | 4 | 1974 | 1979 | |||
Mu-3H | Japan | Nissan Motors [40] | 23.8 m | 300 [41] | No | 3 | 1977 | 1978 | |||
Mu-3S | Japan | Nissan Motors [40] | 23.8 m | 300 [41] | No | 4 | 1980 | 1984 | |||
Mu-3SII | Japan | Nissan Motors [40] | 27.8 m | 770 [41] | No | 8 | 1985 | 1995 | |||
N1 | Soviet Union | NPO Energia | 105.3 m | 95,000 [i] | No | 4 | 1969 | 1972 | |||
N-I | Japan | Mitsubishi | 34 m | 1,200 [54] | No | 7 | 1975 | 1982 | |||
N-II | Japan | Mitsubishi | 35 m | 2,000 [55] | No | 8 | 1981 | 1987 | |||
Naro-1 | South Korea | KARI Khrunichev | 33 m | 100 [56] | No | 3 | 2009 | 2013 | |||
OS-M1 | China | OneSpace | 19 m | 205 [57] | 143 to SSO | No | 1 | 2019 [58] [j] | 2019 | ||
Paektusan-1 | North Korea | KCST | 25.8 m | 20 | No | 1 | 1998 | 1998 | |||
Pegasus | United States | Northrop Grumman | 15.4 m | 455 | No | 6 | 1990 | 1994 | |||
Pegasus H | United States | Northrop Grumman | 15.4 m | 544 | No | 4 | 1995 | 2000 | |||
Pilot II | United States | United States Navy | 4.4 m | N/A | 1.05 to MEO | No | 10 | 1958 | 1958 | ||
Polyot | Soviet Union | RSC Energia | 30 m | 1,400 | No | 2 | 1963 | 1964 | |||
Proton (UR-500) | Soviet Union | Khrunichev | 39.8 m | 12,200 | No | 4 | 1965 | 1966 | |||
Proton-K | Soviet Union | Khrunichev | 50 m | 19,760 [60] | 4,930 [61] | No | 311 [62] | 1965 | 2012 | ||
PSLV-G | India | ISRO | 44 m | 3,200 [63] | 1,050 | 1,600 to SSO | No | 12 [63] | 1993 | 2016 [64] | |
Rocket 3.0 | United States | Astra | 11.6 m | 100 | No | 1 | 2020 | 2020 | |||
Rocket 3.1 | United States | Astra | 11.6 m | 100 | No | 1 | 2020 | 2020 | |||
Rocket 3.2 | United States | Astra | 11.6 m | 100 | No | 1 | 2020 | 2020 | |||
Rocket 3.3 | United States | Astra | 13.1 m | 100 [65] | 150 to SSO | No | 5 | 2021 | 2022 | ||
Rokot-K | Russia | Khrunichev | 25.5 m | No | 4 | 1990 | 1999 | ||||
Rokot-KM | Russia | Khrunichev | 29.1 m | 1,950 [66] | 1,200 to SSO | No | 31 | 2000 | 2019 | ||
RS1 B1 | United States | ABL Space Systems | 27 m | 1,350 [67] | 400 | 975 to SSO
750 to MEO |
No | 1 | 2023 [68] | 2023 | |
Safir-1 | Iran | Iranian Space Agency | 22.6 m | 27 | No | 2 | 2008 | 2009 | |||
Safir-1A | Iran | Iranian Space Agency | 22.6 m | 15 | No | 1 | 2011 | 2011 | |||
Safir-1B | Iran | Iranian Space Agency | 22.6 m | 50 | No | 1 | 2012 | 2012 | |||
Safir-1B+ | Iran | Iranian Space Agency | 22.6 m | 52 | No | 5 | 2012 | 2019 | |||
Saturn I | United States | Chrysler (S-I) | 50-57.4 m | 9,000 [69] | No | 10 [70] | 1961 | 1965 [70] | |||
Saturn IB | United States | Chrysler ( S-IB) | 56.1-68.1 m | 18,600 [71] | No | 9 [72] | 1966 | 1975 | |||
Saturn V | United States |
Boeing (
S-IC)
North American ( S-II) Douglas ( S-IVB) |
110.6 m | 140,000 [73] [74] | 47,000 to TLI | No | 13 [k] | 1967 | 1973 | ||
Scout X-1 | United States | Vought | 21.8 m | 59 | No | 4 | 1960 | 1961 | |||
Scout X-2 | United States | Vought | 21.8 m | 76 | No | 1 | 1962 | 1962 | |||
Scout X-2M | United States | Vought | 21.8 m | 76 | No | 3 | 1962 | 1963 | |||
Scout X-2B | United States | Vought | 21.8 m | 76 | No | 1 | 1963 | 1963 | |||
Scout X-3 | United States | Vought | 21.8 m | 87 | No | 5 | 1962 | 1964 | |||
Scout X-3M | United States | Vought | 21.8 m | 87 | No | 1 | 1963 | 1963 | |||
Scout X-4 | United States | Vought | 22.8 m | 103 | No | 11 | 1963 | 1965 | |||
Scout A | United States | NASA | 22.8 m | 110 | No | 11 | 1965 | 1970 | |||
Scout A-1 | United States | NASA | 22.8 m | 122 | No | 1 | 1973 | 1973 | |||
Scout B | United States | NASA | 22.8 m | 110 | No | 20 | 1965 | 1971 | |||
Scout B-1 | United States | NASA | 22.8 m | 143 | No | 5 | 1971 | 1976 | |||
Scout D-1 | United States | NASA | 22.9 m | 182 | No | 14 | 1972 | 1979 | |||
Scout E-1 | United States | NASA | 22.8 m | 193 | No | 1 | 1974 | 1974 | |||
Scout F-1 | United States | NASA | 22.9 m | 192 | No | 2 | 1975 | 1975 | |||
Scout G-1 | United States | NASA | 22.9 m | 208 | No | 18 | 1979 | 1994 | |||
Shavit | Israel | IAI | 17.7 m | 160 | No | 2 | 1988 | 1990 | |||
Shavit-1 | Israel | IAI | 19.7 m | 225 | No | 4 | 1995 | 2004 | |||
Shtil-1 | Russia | Makeyev | 14.8 m | 280–420 [75] | No | 2 [76] | 1998 | 2006 | |||
SLV-3 | India | ISRO | 22 m | 40 [77] | No | 4 [77] | 1979 | 1983 [77] | |||
Soyuz | Soviet Union | RSC Energia | 45.6 m | 6,450 | No | 31 [78] | 1966 | 1976 | |||
Soyuz-FG | Russia | TsSKB-Progress | 49.5 m | 6,900 [79] | No | 70 [80] [81] | 2001 | 2019 | |||
Soyuz-L | Soviet Union | RSC Energia | 50 m | 5,500 | No | 3 [82] | 1970 | 1971 | |||
Soyuz-M | Soviet Union | RSC Energia | 50 m | 6,600 | No | 8 [83] | 1971 | 1976 | |||
Soyuz ST-A | Russia | TsSKB-Progress | 46.3 m | 7,800 from Kourou [84] | 2,810 with Fregat [85] | No | 9 [80] | 2011 | 2021 | ||
Soyuz ST-B | Russia | TsSKB-Progress | 46.3 m | 9,000 from Kourou [86] | 3,250 with Fregat [85] | 4,400 to SSO [87] | No | 18 [80] | 2011 | 2022 | |
Soyuz-U | Soviet Union | TsSKB-Progress | 51.1 m | 6,650 from Baikonour [88] | No | 786 [80] [89] [90] | 1973 | 2017 | |||
Soyuz-U2 | Soviet Union | TsSKB-Progress | 34.5 m | 7,050 | No | 72 [91] | 1982 | 1995 | |||
Space Shuttle | United States | ATK ( SRBs) | 56.1 m | 24,400 [e] | 3,550 to escape with IUS | Yes | 135 [94] | 1981 | 2011 | ||
SPARK | United States | UH Aerojet Rocketdyne Sandia | 17 m | 300 | No | 1 | 2015 | 2015 | |||
Sparta | United States | ABMA/ Chrysler | 21.8 m | 45 | No | 10 | 1966 | 1967 | |||
Sputnik 8K71PS | Soviet Union | RSC Energia | 30 m | 500 [95] | No | 2 | 1957 | 1957 | |||
Sputnik 8A91 | Soviet Union | RSC Energia | 31.1 m | 1,327 | No | 2 | 1958 | 1958 | |||
SS-520 | Japan | IHI Aerospace | 9.5 m | 4 [96] | No | 2 [97] | 2017 [98] [l] | 2018 | |||
Start-1 | Russia | MITT | 22.7 m | 532 | 250 to SSO | No | 5 [99] | 1993 | 2006 | ||
Start-1.2 | Russia | MITT | 22.7 m | 250-300 to SSO | No | 1 | 1997 | 1997 | |||
Start | Russia | MITT | 28.9 m | 300 to SSO | No | 1 | 1995 | 1995 | |||
Strela | Russia | Khrunichev | 24-
27.4 m |
1,400 [100] | No | 3 [101] | 2003 | 2014 | |||
Taurus-1110 | United States | Orbital | 28.2 m | 1180 | 370 | 750 to SSO | No | 3 | 1994 | 2000 | |
Taurus-2110 | United States | Orbital | 29.1 m | 1250 | 375 | 900 to SSO | No | 2 | 1999 | 2001 | |
Taurus-2210 | United States | Orbital | 30.9 m | 1050 | 700 to SSO | No | 1 | 1998 | 1998 | ||
Taurus-3110 | United States | Orbital | 30.1 m | 1450 | 445 | 1,050 to SSO | No | 2 | 2009 | 2011 | |
Taurus-3210 [102] | United States | Northrop Grumman | 27.9 m | 1,458 [103] | N/A | 1,054 to SSO [m] | No | 1 | 2004 | 2004 | |
Terran 1 | United States | Relativity Space | 35.2 m | 1,250 [104] | 900 to SSO | No | 1 | 2023 | 2023 | ||
Titan II GLV | United States | Martin Marietta | 33 m | 3,600 [105] | No | 11 (+1) | 1964 | 1966 | |||
Titan II(23)G | United States | Martin Marietta | 31.4 m | 3,600 [106] | No | 13 | 1988 | 2003 | |||
Titan IIIA | United States | Martin Marietta | 38.5 m | 3,500 | No | 4 | 1964 | 1965 | |||
Titan IIIB | United States | Martin Marietta | 42 m | 3,300 | No | 22 | 1966 | 1969 | |||
Titan III(23)B | United States | Martin Marietta | 42 m | 3,350 | No | 9 | 1969 | 1971 | |||
Titan III(33)B | United States | Martin Marietta | 42 m | N/A | 4,500 | No | 3 | 1971 | 1973 | ||
Titan III(24)B | United States | Martin Marietta | 44 m | 4,500 | No | 23 | 1971 | 1984 | |||
Titan III(34)B | United States | Martin Marietta | 45.3 m | N/A | No | 11 | 1975 | 1987 | |||
Titan IIIC | United States | Martin Marietta | 41 m | 11,500 | 3,000 | No | 14 | 1965 | 1970 | ||
Titan III(23)C | United States | Martin Marietta | 42.5 m | 13,100 [107] | 3,000 | No | 22 | 1970 | 1982 | ||
Titan IIID | United States | Martin Marietta | 36 m | 12,300 [108] | No | 22 | 1971 | 1982 | |||
Titan IIIE | United States | Martin Marietta | 48.8 m | 15,400 [109] | No | 7 | 1974 | 1977 | |||
Titan 34D | United States | Martin Marietta | 44.5 m | 14,350 | 3,600 | No | 15 | 1982 | 1989 | ||
Titan IVA | United States | Martin Marietta | 51.36 m(standard) | 17,110 [110] | 4,944 with IUS | 14,090 to SSO
[110]
4,536 to GSO with Centaur 3,550 to escape with IUS |
No | 22 [111] | 1989 | 1998 | |
Titan IVB | United States | Lockheed Martin | 51.36 m(standard) | 21,682 [112] | 5,761
[112]
(9,000 with upper stage) |
No | 17 [111] | 1997 | 2005 | ||
Tysklon-2 | Soviet Union | Yuzhmash | 32 m | 3,350 | No | 18 | 1965 | 1971 | |||
Tsyklon-2A | Soviet Union | Yuzhmash | 39.7 m | 3,350 [113] | No | 8 [114] | 1967 | 1969 | |||
Tsyklon-2M | Soviet Union | Yuzhmash | 39.7 m | 2,820 [115] | No | 106 [116] | 1969 | 2006 [116] | |||
Tsyklon-3 | Soviet Union | Yuzhmash | 39.3 m | 1,920 [117] | No | 122 [118] | 1977 | 2009 [118] | |||
Unha-2 | North Korea | KCST | 29.5 m | 80 | No | 1 | 2009 | 2009 | |||
Unha-3 | North Korea | KCST | 30 m | 110 | No | 4 [119] | 2009 [n] | 2016 | |||
Vanguard | United States | Martin | 22.1 m | 9 [120] | No | 10 (+1) | 1957 | 1959 | |||
Vanguard SLV-7 | United States | Martin | 21.6 m | 20 | No | 1 | 1959 | 1959 | |||
VLS-1 | Brazil | AEB, IAE | 19.5 m | 380 [121] | No | 2 [o] | 1997 | 2003 | |||
Volna-O | Russia | Makeyev | 14.2 m | 100 [122] | No | 1 (+5) [76] | 1995 [p] | 2005 [76] | |||
Voskhod | Soviet Union | RSC Energia | 44.1 m | 5,680 | No | 299 | 1963 | 1976 | |||
Vostok-L (Luna) | Soviet Union | RSC Energia | 30.8 m | 4,000 | 400 to TLI | No | 9 | 1958 | 1960 | ||
Vostok (Korabl) | Soviet Union | RSC Energia | 38.4 m | 4,550 | 390 to TLI [123] | No | 4 | 1960 | 1960 | ||
Vostok-K | Soviet Union | RSC Energia | 30.8 m | 2,460 [124] | No | 16 | 1960 | 1964 | |||
Vostok-2 | Soviet Union | RSC Energia | 30.8 m | 4,730 [124] | No | 45 | 1962 | 1967 | |||
Vostok-2M | Soviet Union | RSC Energia | 38.8 m | 1,300 [125] | No | 93 | 1964 | 1991 | |||
Soyuz/Vostok | Soviet Union | RSC Energia | 31 m | 6,000 [126] | No | 2 | 1965 | 1966 | |||
Zenit-2 | Soviet Union | Yuzhnoye | 57 m | 13,740 [127] | No | 36 [128] | 1985 | 2004 [129] | |||
Zenit-2FG | Ukraine | Yuzhnoye | 57 m | No | 1 | 2011 | 2011 | ||||
Zenit-2M | Ukraine | Yuzhnoye | 57 m | 13,920 [127] | No | 1 | 2007 | 2007 | |||
Zenit-3F | Ukraine | Yuzhnoye | 59.6 m | 1,740 to GEO [130] | No | 4 [131] | 2011 | 2017 | |||
Zenit-3SL | Ukraine | Yuzhmash | 59.6 m | 7,000 [131] | 6,160 | No | 36 [131] | 1999 | 2014 | ||
Zenit-3SLB | Ukraine | Yuzhmash | 59.5 m | 3,750 [131] | No | 6 [131] | 2008 | 2013 | |||
Zhuque-1 | China | LandSpace | 19 m | 300 [132] | 200 to SSO | No | 1 [133] | 2018 [133] | 2018 |
Vehicle | Origin | Manufacturer | Height | Mass to ... (kg) | Reuse | Launches
(+ suborbital) |
Launch Site (s) | Date of flight | |||
---|---|---|---|---|---|---|---|---|---|---|---|
LEO | GTO | Other | First | Last | |||||||
Atlas-Able | United States | General Dynamics | 28 m | ~175 to TLI | No | 3 | 1959 | 1960 | |||
Atlas-Agena | United States | Convair/ General Dynamics | 36 m | 1,000 | 390 to TLI | No | 109 | 1960 | 1978 | ||
Atlas-Centaur | United States | Lockheed | 36.2-38.8 m | 1,134 [134] | 2,222 [135] | No | 148 | 1962 | 1983 | ||
Atlas B | United States | Lockheed Martin | 24.9 m | ~4,000 | No | 10 | 1958 | 1959 | |||
Atlas-D OV1 | United States | Convair/ General Dynamics | 25.9 m | 1,400 | No | 7 | 1965 | 1967 | |||
Atlas E/F- Agena | United States | Convair/ General Dynamics/ Lockheed | 34 m | 1,000 | 390 to TLI | No | 1 | 1978 | 1978 | ||
Atlas E/F- Altair-3A | United States | Convair/ General Dynamics | 27.3 m | 210 | No | 1 | 1990 | 1990 | |||
Atlas E/F- Burner-2 | United States | Convair/ General Dynamics | 28.9 m | 950 | No | 1 | 1972 | 1972 | |||
Atlas E/F-MSD | United States | Convair/ General Dynamics | 27.3 m | 800 | No | 4 | 1976 | 1980 | |||
Atlas E/F-OIS | United States | Convair/ General Dynamics | 28.7 m | 870 | No | 2 | 1979 | 1985 | |||
Atlas E/F- OV1 | United States | Convair/ General Dynamics | 26.5 m | 363 | No | 4 | 1968 | 1971 | |||
Atlas E/F-PTS | United States | Convair/ General Dynamics | 26.5 m | 295 | No | 1 | 1974 | 1974 | |||
Atlas E/F-SGS-1 | United States | Convair/ General Dynamics | 29 m | 450 | No | 8 | 1977 | 1981 | |||
Atlas E/F-SGS-2 | United States | Convair/ General Dynamics | 29 m | 770 | No | 4 | 1983 | 1985 | |||
Atlas E/F- Star-17A | United States | Convair/ General Dynamics | 27.4 m | N/A | 800 to MPEO | No | 1 | 1975 | 1975 | ||
Atlas E/F- Star-37S | United States | Convair/ General Dynamics | 29 m | N/A | 1,100 to SSO | No | 19 | 1978 | 1995 | ||
Atlas-F Agena-D | United States | Convair/ General Dynamics | 34 m | N/A | 2,300 to Polar | No | 1 | 1978 | 1978 | ||
Atlas G | United States | Lockheed | 43.9 m | 5,900 [136] | 2,222 | 1,179 to HCO [136] | No | 7 [136] | 1984 | 1989 | |
Atlas H MSD | United States | Lockheed | 27 m | 3,630 [137] | No | 5 | 1983 | 1987 | |||
Atlas LV-3B | United States | Convair | 28.7 m | 1,360 | No | 9 | 1960 | 1963 | |||
Atlas SLV-3 | United States | Convair | 33.3 m | No | 63 | 1966 | 1983 | ||||
Atlas SLV-3 Burner-2 | United States | Convair | 30.3 m | ~1,000 | No | 1 | 1968 | 1968 | |||
Atlas I | United States | Lockheed Martin | 43.9 m | 5,900 [136] | 2,340 [136] | No | 11 [136] | 1990 | 1997 | ||
Atlas II | United States | Lockheed Martin | 47.5 m | 6,780 [136] | 2,810 | 2,000 to HCO [136] | No | 10 [136] | 1991 | 1998 | |
Atlas IIA | United States | Lockheed Martin | 47.5 m | 7,316 [136] | 3,180 | 2,160 to HCO [136] | No | 23 [136] | 1992 | 2002 | |
Atlas IIAS | United States | Lockheed Martin | 49 m | 8,618 [136] | 3,833 | 2,680 to HCO [136] | No | 30 [136] | 1993 | 2004 | |
Atlas IIIA | United States | Lockheed Martin | 52.5 m | 8,686 [136] | 4,060 | 2,970 to HCO [136] | No | 2 [136] | 2000 | 2004 | |
Atlas IIIB/ DEC | United States | Lockheed Martin | 53.7 m | 10,759 [136] | 4,609 [136] | No | 1 [136] | 2002 | 2002 | ||
Atlas IIIB/ SEC | United States | Lockheed Martin | 54.7 m | 10,218 [138] | 4,193 [136] | No | 3 [136] | 2003 | 2005 | ||
Atlas V 401 | United States | ULA | 57.3 m | 9,050 [139] | 4,950 | 6,670 to SSO | No | 41 [139] | 2002 | 2022 | |
Atlas V 411 | United States | ULA | 58.2 m | 9,050 [139] | 6,075 | 8,495 to SSO | No | 6 [139] | 2006 | 2020 | |
Atlas V 421 | United States | ULA | 59.1 m | 9,050 [139] | 7,000 | 9,050 to SSO | No | 9 [139] | 2007 | 2022 | |
Atlas V 431 | United States | ULA | 59.1 m | 9,050 [139] | 7,800 | 9,050 to SSO | No | 3 [139] | 2005 | 2016 | |
Atlas V 501 | United States | ULA | 62.5 m | 8,250 [139] | 3,970 | 5,945 to SSO 1,500 to GEO |
No | 8 [139] | 2010 | 2023 | |
Atlas V 511 | United States | ULA | 62.5 m | 11,000 [139] | 5,250 | 7,820 to SSO
1,750 to GEO |
No | 1 [140] | 2022 | 2022 | |
Atlas V 521 | United States | ULA | 59.7 m | 13,300 [139] | 6,485 | 9,585 to SSO
2,760 to GEO |
No | 2 [139] | 2003 | 2004 | |
Atlas V 531 | United States | ULA | 59.7 m | 15,300 [139] | 7,425 | 11,160 to SSO
3,250 to GEO |
No | 5 [139] | 2010 | 2022 | |
Atlas V 541 | United States | ULA | 59.7 m | 17,100 [139] | 8,240 | 12,435 to SSO
3,730 to GEO |
No | 9 [139] | 2011 | 2022 |
Vehicle | Origin | Manufacturer | Height | Mass to ... (kg) | Reuse | Launches
(+ suborbital) |
Launch Site (s) | Date of flight | |||
---|---|---|---|---|---|---|---|---|---|---|---|
LEO | GTO | Other | First | Last | |||||||
Delta 0300 | United States | McDonnell Douglas | 34 m | 340 [141] | 747 to SSO [142] | No | 3 [143] | 1972 | 1973 [144] | ||
Delta 0900 | United States | McDonnell Douglas | 34 m | 1,300 [145] | 818 to SSO [143] | No | 2 [143] | 1972 | 1972 | ||
Delta 1410 | United States | McDonnell Douglas | 35.2 m | 340 [146] | No | 1 [143] | 1975 | 1975 | |||
Delta 1604 | United States | McDonnell Douglas | 35.2 m | 390 [147] | No | 2 [143] | 1972 | 1973 | |||
Delta 1900 | United States | McDonnell Douglas | 35.2 m | 1,800 [143] | No | 1 [143] | 1973 | 1973 | |||
Delta 1910 | United States | McDonnell Douglas | 35.2 m | 1,066 [148] | No | 1 [143] | 1975 | 1975 | |||
Delta 1913 | United States | McDonnell Douglas | 35.2 m | 328 [149] | No | 1 [143] | 1973 | 1973 | |||
Delta 1914 | United States | McDonnell Douglas | 35.2 m | 680 [150] | No | 2 [143] | 1972 | 1973 | |||
Delta 2310 | United States | McDonnell Douglas | 35.2 m | 336 [151] | No | 3 [143] | 1974 | 1981 | |||
Delta 2313 | United States | McDonnell Douglas | 35.2 m | 243 to GEO [152] | No | 3 [143] | 1974 | 1977 | |||
Delta 2910 | United States | McDonnell Douglas | 35.2 m | 1,887 [143] | No | 6 [143] | 1975 | 1978 | |||
Delta 2913 | United States | McDonnell Douglas | 35.2 m | 2,000 [153] | 700 [153] | No | 6 [143] | 1975 | 1976 | ||
Delta 2914 | United States | McDonnell Douglas | 35.2 m | 724 [143] | No | 30 [143] | 1974 | 1979 | |||
Delta 3910 | United States | McDonnell Douglas | 35.2 m | 2,494 [143] | 1,154 with PAM-D | No | 10 [143] | 1980 | 1988 | ||
Delta 3913 | United States | McDonnell Douglas | 35.2 m | 816 [154] | No | 1 [143] | 1981 | 1981 | |||
Delta 3914 | United States | McDonnell Douglas | 35.2 m | 954 [143] | No | 13 [143] | 1975 | 1987 | |||
Delta 3920 | United States | McDonnell Douglas | 35.2 m | 3,452 [143] | 1,284 with PAM-D | No | 10 [143] | 1982 | 1989 | ||
Delta 3924 | United States | McDonnell Douglas | 35.2 m | 1,104 [143] | No | 4 [143] | 1982 | 1984 | |||
Delta 4925 | United States | McDonnell Douglas | 35.2 m | 3,400 [155] | 1,312 [143] | No | 2 [143] | 1989 | 1990 | ||
Delta 5920 | United States | McDonnell Douglas | 35.2 m | 3,848 [156] | No | 1 [143] | 1989 | 1989 | |||
Delta II 6920 | United States | McDonnell Douglas | 38.8 m | 3,983 [143] | No | 3 [143] | 1990 | 1992 | |||
Delta II 6925 | United States | McDonnell Douglas | 39.4 m | 1,447 | 1,447 [143] | No | 14 [143] | 1989 | 1992 | ||
Delta II 7320 | United States | Boeing IDS / ULA | 38.9 m | 2,865 [143] | 1,651 to SSO | No | 12 [143] | 1999 | 2015 | ||
Delta II 7326 | United States | Boeing IDS | 38.4 m | 934 [143] | 636 to TLI
629 to HCO |
No | 3 [143] | 1998 | 2001 | ||
Delta II 7420 | United States | ULA | 39 m | 3,185 [143] | 1,966 to SSO | No | 14 [143] | 1998 | 2018 | ||
Delta II 7425 | United States | Boeing IDS | 39 m | 1,100 [143] | 804 to HCO | No | 4 [143] | 1998 | 2002 | ||
Delta II 7426 | United States | Boeing IDS | 39 m | 1,058 [143] | 734 to TLI
711 to HCO |
No | 1 [143] | 1999 | 1999 | ||
Delta II 7920 | United States | Boeing IDS / ULA | 39.4 m | 5,030 [143] | 3,123 to SSO | No | 29 [143] | 1998 | 2017 | ||
Delta II 7925 | United States | Boeing IDS / ULA | 39.4 m | 1,819 [143] | 1,177 to TLI
1,265 to HCO |
No | 69 [143] | 1990 | 2009 | ||
Delta II-H 7920H | United States | Boeing IDS / ULA | 39 m | 6,097 [143] | No | 3 [143] | 2003 | 2011 | |||
Delta II-H 7925H | United States | Boeing IDS / ULA | 39.8 m | 2,171 | 1,508 to HCO [143] | No | 3 [143] | 2003 | 2007 | ||
Delta III 8930 | United States | Boeing IDS | 39 m | 8,292 [143] | 3,810 | No | 3 [143] | 1998 | 2000 | ||
Delta IV Heavy | United States | ULA | 72 m | 28,370 [157] | 14,210 [157] | 23,560 to polar
[157]
11,290 to TLI 8,000 to TMI |
No | 16 [158] | 2004 | 2024 | |
Delta IV M | United States | Boeing IDS | 61.3 m | 9,440 [157] | 4,440 | 7,690 to polar | No | 3 [158] | 2003 | 2006 | |
Delta IV M+(4,2) | United States | ULA | 61.3 m | 13,140 [157] | 6,390 | 10,250 to polar | No | 14 [158] | 2002 | 2019 | |
Delta IV M+(5,2) | United States | ULA | 65.5 m | 11,470 [157] | 5,490 | 9,600 to polar | No | 3 [158] | 2012 | 2018 | |
Delta IV M+(5,4) | United States | ULA | 65.5 m | 14,140 [157] | 7,300 | 11,600 to polar | No | 8 [158] | 2009 | 2019 |
Russian officials have said they plan to discontinue Dnepr launches.
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).
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Vehicle | Origin | Manufacturer | Height | Mass to ... (kg) | Reuse | Launches
(+ suborbital) |
Launch Site (s) | Date of flight | |||
---|---|---|---|---|---|---|---|---|---|---|---|
LEO | GTO | Other | First | Last | |||||||
Antares 110–130 | United States | Orbital | 40.5-41.9 m | 5,100 [1] | 1,500 to SSO | No | 5 [1] | 2013 | 2014 | ||
Antares 230 / 230+ | United States | Northrop Grumman | 42.5 m | 8,200 [1] | 3,000 to SSO [a] | No | 13 | 2016 | 2023 | ||
Ariane 1 | Europe | Aérospatiale | 49.1 m | 1,830 [2] | No | 11 [2] | 1979 | 1986 | |||
Ariane 2 | Europe | Aérospatiale | 49.1 m | 2,270 [2] | No | 6 [2] | 1986 | 1989 | |||
Ariane 3 | Europe | Aérospatiale | 49.1 m | 2,650 [2] | No | 11 [2] | 1984 | 1989 | |||
Ariane 4 40 | Europe | Aérospatiale | 58.7 m | 4,600 [2] | 2,105 | 2,740 to SSO | No | 7 [2] | 1990 | 1999 | |
Ariane 4 42L | Europe | Aérospatiale | 58.7 m | 7,000 [2] | 3,480 | 4,500 to SSO | No | 13 [2] | 1993 | 2002 | |
Ariane 4 42P | Europe | Aérospatiale | 58.7 m | 6,000 [2] | 2,930 | 3,400 to SSO | No | 15 [2] | 1990 | 2002 | |
Ariane 4 44L | Europe | Aérospatiale | 58.7 m | 7,000 [2] | 4,720 | 6,000 to SSO | No | 40 [2] | 1989 | 2003 | |
Ariane 4 44LP | Europe | Aérospatiale | 58.7 m | 7,000 [2] | 4,220 | 5,000 to SSO | No | 26 [2] | 1988 | 2001 | |
Ariane 4 44P | Europe | Aérospatiale | 58.7 m | 6,500 [2] | 3,465 | 4,100 to SSO | No | 15 [2] | 1991 | 2001 | |
Ariane 5 G | Europe | EADS Astrium | 47.5 m | 18,000 [3] | 6,900 [3] | No | 16 [3] | 1996 | 2003 | ||
Ariane 5 G+ | Europe | EADS Astrium | 47.8 m | 7,100 [3] | No | 3 [3] | 2004 | 2004 | |||
Ariane 5 GS | Europe | EADS Astrium | 47.8 m | 16,000 [4] | 6,600 [3] | No | 6 [3] | 2005 | 2009 [5] | ||
Ariane 5 ES | Europe | EADS Astrium | 50.7 m | 21,000 [6] | 8,000 [3] | No | 8 [3] | 2008 | 2018 | ||
Ariane 5 ECA | Europe | EADS Astrium | 52.6 m | 21,000 [6] | 11,210 [7] | No | 84 | 2002 | 2023 | ||
ASLV | India | ISRO [8] | 23.5 m | 150 [9] | No | 4 [9] | 1987 | 1994 | |||
Athena I LLV-1 | United States | Lockheed Martin | 18.4 m | 500 | No | 1 | 1995 | 1995 | |||
Athena I | United States | Lockheed Martin | 18.9 m | 795 [10] | 515 | No | 3 | 1997 | 2001 | ||
Athena II | United States | Lockheed Martin | 28.2 m | 1,800 [11] | No | 3 [12] | 1998 | 1999 [13] | |||
Black Arrow | United Kingdom | RAE | 13 m | 73 [14] | No | 2 (+2) | 1969 [b] | 1971 | |||
Blue Scout II | United States | Vought | 24 m | 30 | No | 3 | 1961 | 1961 | |||
Ceres-1 (1) [c] | China | Galactic Energy | 18.5 m | 350 | No | 1 | 2020 | 2020 | |||
Ceres-1 (2) [c] | China | Galactic Energy | 19.5 m | 400 | No | 1 | 2021 | 2021 | |||
Commercial Titan III | United States | Martin Marietta | 47.3 m | 13,100 [15] | No | 4 | 1990 | 1992 | |||
Conestoga 1620 | United States | Space Services | 15.2 m | 1179 | No | 1 | 1995 | 1995 | |||
Diamant A | France | SEREB | 18.9 m | 80 | No | 4 | 1965 | 1967 | |||
Diamant B | France | SEREB | 23.5 m | 115 | No | 5 | 1970 | 1973 | |||
Diamant BP4 | France | SEREB | 21.6 m | 153 | No | 3 | 1975 | 1975 | |||
Dnepr | Ukraine | Yuzhmash | 34.3 m | 3,700 [16] | No | 22 [16] | 1999 | 2015 [17] | |||
Energia [d] | Soviet Union | NPO Energia | 58.8 m | 105,000 | 20,000 to
GEO
[18]
32,000 to TLI [18] |
No | 1 (failed to orbit) | 1987 | 1987 | ||
Energia- Buran | Soviet Union | NPO Energia | 58.8 m | 30,000 [18] [e] | Yes | 1 | 1988 | 1988 | |||
Epsilon | Japan | IHI [19] | 24.4 m | 1,200 | N/A | 450 to SSO | No | 1 | 2013 | 2022 | |
Epsilon (enhanced) | Japan | IHI [19] | 26 m | 1,500 [20] | N/A | 590 to SSO [20] | No | 6 [20] | |||
Europa I | Europe | ELDO | 31.7 m | 1,440 | 200 | No | 3 | 1968 | 1970 | ||
Europa II | Europe | ELDO | 31.7 m | 360 | No | 1 | 1971 | 1971 | |||
Falcon 1 | United States | SpaceX | 21 m | 470 [21] | No | 5 [21] | 2006 | 2009 | |||
Falcon 9 v1.0 | United States | SpaceX | 54.9 m | 9,000 | 3,400 | No | 5 | 2010 | 2013 | ||
Falcon 9 v1.1 | United States | SpaceX | 68.4 m | 13,150 [22] [f] | 4,850 [22] | No | 15 [23] | 2013 | 2016 | ||
Falcon 9 Full Thrust | United States | SpaceX |
70.8 m |
17,400 [24] | 5,500 [24] | 9,600 to polar [25] | Yes | 36 | 2015 | 2018 | |
22,800 [24] | 8,300 [24] | No | |||||||||
Feng Bao 1 | China | Shanghai Bureau No.2 | 33 m | 2,500 [26] | No | 8 (+3) [27] | 1972 | 1981 | |||
GSLV Mk.I(a) | India | ISRO | 49.1 m | 5,000 [28] | 1,540 [29] | No | 1 [29] | 2001 | 2001 | ||
GSLV Mk.I(b) | India | ISRO | 49.1 m | 5,000 [28] | 2,150 [29] | No | 4 [29] | 2003 | 2007 | ||
GSLV Mk.I(c) | India | ISRO | 49.1 m | 5,000 [28] | No | 1 [29] | 2010 | 2010 | |||
H-I | Japan | Mitsubishi | 42 m | 1,400 [30] | No | 9 | 1986 | 1992 | |||
H-II / IIS | Japan | Mitsubishi | 49 m | 10,060 [31] | 4,000 [32] | No | 7 [32] | 1994 | 1999 | ||
H-IIA 204 | Japan | Mitsubishi | 53 m | 15,000 | 5,950 [33]: 48 | No | 5 [34] | 2006 | 2021 | ||
H-IIA 2022 | Japan | Mitsubishi | 53 m | 4,500 [34] | No | 3 [34] | 2005 | 2007 | |||
H-IIA 2024 | Japan | Mitsubishi | 57 m | 11,000 [35] | 5,000 [34] | No | 7 [34] | 2002 | 2008 | ||
H-IIB | Japan | Mitsubishi | 56.6 m | 16,500 ( ISS) [36] | 8,000 | No | 8 [37] | 2009 | 2020 | ||
Hyperbola-1 (1) [g] | China | i-Space | 20.9 m | 260 | No | 1 | 2019 | 2019 | |||
Juno I | United States | Chrysler | 21.2 m | 11 | No | 1 | 1958 | 1959 | |||
Juno II | United States | Chrysler | 24 m | 41 | 6 to TLI | No | 10 | 1958 | 1961 | ||
Kaituozhe-1 | China | CALT | 13.6 m | 40 | No | 2 | 2002 | 2003 | |||
Kaituozhe-2 | China | CASC | 16.8 m | 800 [38] | No | 1 [38] | 2017 | 2017 | |||
Kosmos | Soviet Union | NPO Polyot | 29.6 m | 350 | No | 38 | 1961 | 1967 | |||
Kosmos-1 | Soviet Union | NPO Polyot | 26.3 m | 1,400 | No | 8 | 1964 | 1965 | |||
Kosmos-2 | Soviet Union | NPO Polyot | 31 m | 300 | No | 127 | 1965 | 1977 | |||
Kosmos-3 | Soviet Union | NPO Polyot | 32.4 m | 1,400 | No | 6 | 1966 | 1968 | |||
Kosmos-3M | Soviet Union | NPO Polyot | 32.4 m | 1,500 [39] | No | 445 | 1967 | 2010 | |||
Kosmos-3MRB | Soviet Union | NPO Polyot | 32.4 m | 1,500 | No | 10 | 1980 | 1988 | |||
Lambda 4S | Japan | Nissan Motors [40] | 16.5 m | 26 [41] | No | 5 | 1966 | 1970 | |||
LauncherOne | United States | Virgin Orbit | 21.3 m | 500 | 300 to SSO | No | 6 | 2020 | 2023 | ||
Long March 1 | China | CALT | 29.9 m | 300 [42] | No | 2 [43] | 1970 | 1971 | |||
Long March 1D | China | CALT | 28.2 m | 740 [44] | No | 0 (+3) [43] | 1995 [h] | 2002 | |||
Long March 2A | China | CALT | 32 m | 2,000 [45] | No | 4 [46] | 1974 | 1978 | |||
Long March 2E | China | CALT | 49.7 m | 9,200 [46] | No | 7 [46] | 1990 | 1995 | |||
Long March 3 | China | CALT | 43.3 m | 5,000 [47] | No | 13 [47] | 1984 | 2000 | |||
Long March 3B | China | CALT | 54.8 m | 11,200 [48] | 5,100 | 5,700 to SSO | No | 12 [47] | 1996 | 2012 | |
Long March 4A | China | CALT | 41.9 m | 4,000 | No | 2 [49] | 1988 | 1990 | |||
M-V | Japan |
Nissan Motors
[40] (1997–2000)
IHI Aerospace [19] (2000–2006) |
30.8 m | 1,850 [41] | No | 7 | 1997 | 2006 | |||
Molniya | Soviet Union | RSC Energia | 43.4 m | 1,800 [50] | No | 40 [51] | 1960 | 1967 | |||
Molniya-M | Soviet Union | RSC Energia | 43.4 m | 2,400 [52] | No | 280 [53] | 1965 | 2010 | |||
Mu-4S | Japan | Nissan Motors [40] | 23.6 m | 180 [41] | No | 4 | 1971 | 1972 | |||
Mu-3C | Japan | Nissan Motors [40] | 20.3 m | 195 [41] | No | 4 | 1974 | 1979 | |||
Mu-3H | Japan | Nissan Motors [40] | 23.8 m | 300 [41] | No | 3 | 1977 | 1978 | |||
Mu-3S | Japan | Nissan Motors [40] | 23.8 m | 300 [41] | No | 4 | 1980 | 1984 | |||
Mu-3SII | Japan | Nissan Motors [40] | 27.8 m | 770 [41] | No | 8 | 1985 | 1995 | |||
N1 | Soviet Union | NPO Energia | 105.3 m | 95,000 [i] | No | 4 | 1969 | 1972 | |||
N-I | Japan | Mitsubishi | 34 m | 1,200 [54] | No | 7 | 1975 | 1982 | |||
N-II | Japan | Mitsubishi | 35 m | 2,000 [55] | No | 8 | 1981 | 1987 | |||
Naro-1 | South Korea | KARI Khrunichev | 33 m | 100 [56] | No | 3 | 2009 | 2013 | |||
OS-M1 | China | OneSpace | 19 m | 205 [57] | 143 to SSO | No | 1 | 2019 [58] [j] | 2019 | ||
Paektusan-1 | North Korea | KCST | 25.8 m | 20 | No | 1 | 1998 | 1998 | |||
Pegasus | United States | Northrop Grumman | 15.4 m | 455 | No | 6 | 1990 | 1994 | |||
Pegasus H | United States | Northrop Grumman | 15.4 m | 544 | No | 4 | 1995 | 2000 | |||
Pilot II | United States | United States Navy | 4.4 m | N/A | 1.05 to MEO | No | 10 | 1958 | 1958 | ||
Polyot | Soviet Union | RSC Energia | 30 m | 1,400 | No | 2 | 1963 | 1964 | |||
Proton (UR-500) | Soviet Union | Khrunichev | 39.8 m | 12,200 | No | 4 | 1965 | 1966 | |||
Proton-K | Soviet Union | Khrunichev | 50 m | 19,760 [60] | 4,930 [61] | No | 311 [62] | 1965 | 2012 | ||
PSLV-G | India | ISRO | 44 m | 3,200 [63] | 1,050 | 1,600 to SSO | No | 12 [63] | 1993 | 2016 [64] | |
Rocket 3.0 | United States | Astra | 11.6 m | 100 | No | 1 | 2020 | 2020 | |||
Rocket 3.1 | United States | Astra | 11.6 m | 100 | No | 1 | 2020 | 2020 | |||
Rocket 3.2 | United States | Astra | 11.6 m | 100 | No | 1 | 2020 | 2020 | |||
Rocket 3.3 | United States | Astra | 13.1 m | 100 [65] | 150 to SSO | No | 5 | 2021 | 2022 | ||
Rokot-K | Russia | Khrunichev | 25.5 m | No | 4 | 1990 | 1999 | ||||
Rokot-KM | Russia | Khrunichev | 29.1 m | 1,950 [66] | 1,200 to SSO | No | 31 | 2000 | 2019 | ||
RS1 B1 | United States | ABL Space Systems | 27 m | 1,350 [67] | 400 | 975 to SSO
750 to MEO |
No | 1 | 2023 [68] | 2023 | |
Safir-1 | Iran | Iranian Space Agency | 22.6 m | 27 | No | 2 | 2008 | 2009 | |||
Safir-1A | Iran | Iranian Space Agency | 22.6 m | 15 | No | 1 | 2011 | 2011 | |||
Safir-1B | Iran | Iranian Space Agency | 22.6 m | 50 | No | 1 | 2012 | 2012 | |||
Safir-1B+ | Iran | Iranian Space Agency | 22.6 m | 52 | No | 5 | 2012 | 2019 | |||
Saturn I | United States | Chrysler (S-I) | 50-57.4 m | 9,000 [69] | No | 10 [70] | 1961 | 1965 [70] | |||
Saturn IB | United States | Chrysler ( S-IB) | 56.1-68.1 m | 18,600 [71] | No | 9 [72] | 1966 | 1975 | |||
Saturn V | United States |
Boeing (
S-IC)
North American ( S-II) Douglas ( S-IVB) |
110.6 m | 140,000 [73] [74] | 47,000 to TLI | No | 13 [k] | 1967 | 1973 | ||
Scout X-1 | United States | Vought | 21.8 m | 59 | No | 4 | 1960 | 1961 | |||
Scout X-2 | United States | Vought | 21.8 m | 76 | No | 1 | 1962 | 1962 | |||
Scout X-2M | United States | Vought | 21.8 m | 76 | No | 3 | 1962 | 1963 | |||
Scout X-2B | United States | Vought | 21.8 m | 76 | No | 1 | 1963 | 1963 | |||
Scout X-3 | United States | Vought | 21.8 m | 87 | No | 5 | 1962 | 1964 | |||
Scout X-3M | United States | Vought | 21.8 m | 87 | No | 1 | 1963 | 1963 | |||
Scout X-4 | United States | Vought | 22.8 m | 103 | No | 11 | 1963 | 1965 | |||
Scout A | United States | NASA | 22.8 m | 110 | No | 11 | 1965 | 1970 | |||
Scout A-1 | United States | NASA | 22.8 m | 122 | No | 1 | 1973 | 1973 | |||
Scout B | United States | NASA | 22.8 m | 110 | No | 20 | 1965 | 1971 | |||
Scout B-1 | United States | NASA | 22.8 m | 143 | No | 5 | 1971 | 1976 | |||
Scout D-1 | United States | NASA | 22.9 m | 182 | No | 14 | 1972 | 1979 | |||
Scout E-1 | United States | NASA | 22.8 m | 193 | No | 1 | 1974 | 1974 | |||
Scout F-1 | United States | NASA | 22.9 m | 192 | No | 2 | 1975 | 1975 | |||
Scout G-1 | United States | NASA | 22.9 m | 208 | No | 18 | 1979 | 1994 | |||
Shavit | Israel | IAI | 17.7 m | 160 | No | 2 | 1988 | 1990 | |||
Shavit-1 | Israel | IAI | 19.7 m | 225 | No | 4 | 1995 | 2004 | |||
Shtil-1 | Russia | Makeyev | 14.8 m | 280–420 [75] | No | 2 [76] | 1998 | 2006 | |||
SLV-3 | India | ISRO | 22 m | 40 [77] | No | 4 [77] | 1979 | 1983 [77] | |||
Soyuz | Soviet Union | RSC Energia | 45.6 m | 6,450 | No | 31 [78] | 1966 | 1976 | |||
Soyuz-FG | Russia | TsSKB-Progress | 49.5 m | 6,900 [79] | No | 70 [80] [81] | 2001 | 2019 | |||
Soyuz-L | Soviet Union | RSC Energia | 50 m | 5,500 | No | 3 [82] | 1970 | 1971 | |||
Soyuz-M | Soviet Union | RSC Energia | 50 m | 6,600 | No | 8 [83] | 1971 | 1976 | |||
Soyuz ST-A | Russia | TsSKB-Progress | 46.3 m | 7,800 from Kourou [84] | 2,810 with Fregat [85] | No | 9 [80] | 2011 | 2021 | ||
Soyuz ST-B | Russia | TsSKB-Progress | 46.3 m | 9,000 from Kourou [86] | 3,250 with Fregat [85] | 4,400 to SSO [87] | No | 18 [80] | 2011 | 2022 | |
Soyuz-U | Soviet Union | TsSKB-Progress | 51.1 m | 6,650 from Baikonour [88] | No | 786 [80] [89] [90] | 1973 | 2017 | |||
Soyuz-U2 | Soviet Union | TsSKB-Progress | 34.5 m | 7,050 | No | 72 [91] | 1982 | 1995 | |||
Space Shuttle | United States | ATK ( SRBs) | 56.1 m | 24,400 [e] | 3,550 to escape with IUS | Yes | 135 [94] | 1981 | 2011 | ||
SPARK | United States | UH Aerojet Rocketdyne Sandia | 17 m | 300 | No | 1 | 2015 | 2015 | |||
Sparta | United States | ABMA/ Chrysler | 21.8 m | 45 | No | 10 | 1966 | 1967 | |||
Sputnik 8K71PS | Soviet Union | RSC Energia | 30 m | 500 [95] | No | 2 | 1957 | 1957 | |||
Sputnik 8A91 | Soviet Union | RSC Energia | 31.1 m | 1,327 | No | 2 | 1958 | 1958 | |||
SS-520 | Japan | IHI Aerospace | 9.5 m | 4 [96] | No | 2 [97] | 2017 [98] [l] | 2018 | |||
Start-1 | Russia | MITT | 22.7 m | 532 | 250 to SSO | No | 5 [99] | 1993 | 2006 | ||
Start-1.2 | Russia | MITT | 22.7 m | 250-300 to SSO | No | 1 | 1997 | 1997 | |||
Start | Russia | MITT | 28.9 m | 300 to SSO | No | 1 | 1995 | 1995 | |||
Strela | Russia | Khrunichev | 24-
27.4 m |
1,400 [100] | No | 3 [101] | 2003 | 2014 | |||
Taurus-1110 | United States | Orbital | 28.2 m | 1180 | 370 | 750 to SSO | No | 3 | 1994 | 2000 | |
Taurus-2110 | United States | Orbital | 29.1 m | 1250 | 375 | 900 to SSO | No | 2 | 1999 | 2001 | |
Taurus-2210 | United States | Orbital | 30.9 m | 1050 | 700 to SSO | No | 1 | 1998 | 1998 | ||
Taurus-3110 | United States | Orbital | 30.1 m | 1450 | 445 | 1,050 to SSO | No | 2 | 2009 | 2011 | |
Taurus-3210 [102] | United States | Northrop Grumman | 27.9 m | 1,458 [103] | N/A | 1,054 to SSO [m] | No | 1 | 2004 | 2004 | |
Terran 1 | United States | Relativity Space | 35.2 m | 1,250 [104] | 900 to SSO | No | 1 | 2023 | 2023 | ||
Titan II GLV | United States | Martin Marietta | 33 m | 3,600 [105] | No | 11 (+1) | 1964 | 1966 | |||
Titan II(23)G | United States | Martin Marietta | 31.4 m | 3,600 [106] | No | 13 | 1988 | 2003 | |||
Titan IIIA | United States | Martin Marietta | 38.5 m | 3,500 | No | 4 | 1964 | 1965 | |||
Titan IIIB | United States | Martin Marietta | 42 m | 3,300 | No | 22 | 1966 | 1969 | |||
Titan III(23)B | United States | Martin Marietta | 42 m | 3,350 | No | 9 | 1969 | 1971 | |||
Titan III(33)B | United States | Martin Marietta | 42 m | N/A | 4,500 | No | 3 | 1971 | 1973 | ||
Titan III(24)B | United States | Martin Marietta | 44 m | 4,500 | No | 23 | 1971 | 1984 | |||
Titan III(34)B | United States | Martin Marietta | 45.3 m | N/A | No | 11 | 1975 | 1987 | |||
Titan IIIC | United States | Martin Marietta | 41 m | 11,500 | 3,000 | No | 14 | 1965 | 1970 | ||
Titan III(23)C | United States | Martin Marietta | 42.5 m | 13,100 [107] | 3,000 | No | 22 | 1970 | 1982 | ||
Titan IIID | United States | Martin Marietta | 36 m | 12,300 [108] | No | 22 | 1971 | 1982 | |||
Titan IIIE | United States | Martin Marietta | 48.8 m | 15,400 [109] | No | 7 | 1974 | 1977 | |||
Titan 34D | United States | Martin Marietta | 44.5 m | 14,350 | 3,600 | No | 15 | 1982 | 1989 | ||
Titan IVA | United States | Martin Marietta | 51.36 m(standard) | 17,110 [110] | 4,944 with IUS | 14,090 to SSO
[110]
4,536 to GSO with Centaur 3,550 to escape with IUS |
No | 22 [111] | 1989 | 1998 | |
Titan IVB | United States | Lockheed Martin | 51.36 m(standard) | 21,682 [112] | 5,761
[112]
(9,000 with upper stage) |
No | 17 [111] | 1997 | 2005 | ||
Tysklon-2 | Soviet Union | Yuzhmash | 32 m | 3,350 | No | 18 | 1965 | 1971 | |||
Tsyklon-2A | Soviet Union | Yuzhmash | 39.7 m | 3,350 [113] | No | 8 [114] | 1967 | 1969 | |||
Tsyklon-2M | Soviet Union | Yuzhmash | 39.7 m | 2,820 [115] | No | 106 [116] | 1969 | 2006 [116] | |||
Tsyklon-3 | Soviet Union | Yuzhmash | 39.3 m | 1,920 [117] | No | 122 [118] | 1977 | 2009 [118] | |||
Unha-2 | North Korea | KCST | 29.5 m | 80 | No | 1 | 2009 | 2009 | |||
Unha-3 | North Korea | KCST | 30 m | 110 | No | 4 [119] | 2009 [n] | 2016 | |||
Vanguard | United States | Martin | 22.1 m | 9 [120] | No | 10 (+1) | 1957 | 1959 | |||
Vanguard SLV-7 | United States | Martin | 21.6 m | 20 | No | 1 | 1959 | 1959 | |||
VLS-1 | Brazil | AEB, IAE | 19.5 m | 380 [121] | No | 2 [o] | 1997 | 2003 | |||
Volna-O | Russia | Makeyev | 14.2 m | 100 [122] | No | 1 (+5) [76] | 1995 [p] | 2005 [76] | |||
Voskhod | Soviet Union | RSC Energia | 44.1 m | 5,680 | No | 299 | 1963 | 1976 | |||
Vostok-L (Luna) | Soviet Union | RSC Energia | 30.8 m | 4,000 | 400 to TLI | No | 9 | 1958 | 1960 | ||
Vostok (Korabl) | Soviet Union | RSC Energia | 38.4 m | 4,550 | 390 to TLI [123] | No | 4 | 1960 | 1960 | ||
Vostok-K | Soviet Union | RSC Energia | 30.8 m | 2,460 [124] | No | 16 | 1960 | 1964 | |||
Vostok-2 | Soviet Union | RSC Energia | 30.8 m | 4,730 [124] | No | 45 | 1962 | 1967 | |||
Vostok-2M | Soviet Union | RSC Energia | 38.8 m | 1,300 [125] | No | 93 | 1964 | 1991 | |||
Soyuz/Vostok | Soviet Union | RSC Energia | 31 m | 6,000 [126] | No | 2 | 1965 | 1966 | |||
Zenit-2 | Soviet Union | Yuzhnoye | 57 m | 13,740 [127] | No | 36 [128] | 1985 | 2004 [129] | |||
Zenit-2FG | Ukraine | Yuzhnoye | 57 m | No | 1 | 2011 | 2011 | ||||
Zenit-2M | Ukraine | Yuzhnoye | 57 m | 13,920 [127] | No | 1 | 2007 | 2007 | |||
Zenit-3F | Ukraine | Yuzhnoye | 59.6 m | 1,740 to GEO [130] | No | 4 [131] | 2011 | 2017 | |||
Zenit-3SL | Ukraine | Yuzhmash | 59.6 m | 7,000 [131] | 6,160 | No | 36 [131] | 1999 | 2014 | ||
Zenit-3SLB | Ukraine | Yuzhmash | 59.5 m | 3,750 [131] | No | 6 [131] | 2008 | 2013 | |||
Zhuque-1 | China | LandSpace | 19 m | 300 [132] | 200 to SSO | No | 1 [133] | 2018 [133] | 2018 |
Vehicle | Origin | Manufacturer | Height | Mass to ... (kg) | Reuse | Launches
(+ suborbital) |
Launch Site (s) | Date of flight | |||
---|---|---|---|---|---|---|---|---|---|---|---|
LEO | GTO | Other | First | Last | |||||||
Atlas-Able | United States | General Dynamics | 28 m | ~175 to TLI | No | 3 | 1959 | 1960 | |||
Atlas-Agena | United States | Convair/ General Dynamics | 36 m | 1,000 | 390 to TLI | No | 109 | 1960 | 1978 | ||
Atlas-Centaur | United States | Lockheed | 36.2-38.8 m | 1,134 [134] | 2,222 [135] | No | 148 | 1962 | 1983 | ||
Atlas B | United States | Lockheed Martin | 24.9 m | ~4,000 | No | 10 | 1958 | 1959 | |||
Atlas-D OV1 | United States | Convair/ General Dynamics | 25.9 m | 1,400 | No | 7 | 1965 | 1967 | |||
Atlas E/F- Agena | United States | Convair/ General Dynamics/ Lockheed | 34 m | 1,000 | 390 to TLI | No | 1 | 1978 | 1978 | ||
Atlas E/F- Altair-3A | United States | Convair/ General Dynamics | 27.3 m | 210 | No | 1 | 1990 | 1990 | |||
Atlas E/F- Burner-2 | United States | Convair/ General Dynamics | 28.9 m | 950 | No | 1 | 1972 | 1972 | |||
Atlas E/F-MSD | United States | Convair/ General Dynamics | 27.3 m | 800 | No | 4 | 1976 | 1980 | |||
Atlas E/F-OIS | United States | Convair/ General Dynamics | 28.7 m | 870 | No | 2 | 1979 | 1985 | |||
Atlas E/F- OV1 | United States | Convair/ General Dynamics | 26.5 m | 363 | No | 4 | 1968 | 1971 | |||
Atlas E/F-PTS | United States | Convair/ General Dynamics | 26.5 m | 295 | No | 1 | 1974 | 1974 | |||
Atlas E/F-SGS-1 | United States | Convair/ General Dynamics | 29 m | 450 | No | 8 | 1977 | 1981 | |||
Atlas E/F-SGS-2 | United States | Convair/ General Dynamics | 29 m | 770 | No | 4 | 1983 | 1985 | |||
Atlas E/F- Star-17A | United States | Convair/ General Dynamics | 27.4 m | N/A | 800 to MPEO | No | 1 | 1975 | 1975 | ||
Atlas E/F- Star-37S | United States | Convair/ General Dynamics | 29 m | N/A | 1,100 to SSO | No | 19 | 1978 | 1995 | ||
Atlas-F Agena-D | United States | Convair/ General Dynamics | 34 m | N/A | 2,300 to Polar | No | 1 | 1978 | 1978 | ||
Atlas G | United States | Lockheed | 43.9 m | 5,900 [136] | 2,222 | 1,179 to HCO [136] | No | 7 [136] | 1984 | 1989 | |
Atlas H MSD | United States | Lockheed | 27 m | 3,630 [137] | No | 5 | 1983 | 1987 | |||
Atlas LV-3B | United States | Convair | 28.7 m | 1,360 | No | 9 | 1960 | 1963 | |||
Atlas SLV-3 | United States | Convair | 33.3 m | No | 63 | 1966 | 1983 | ||||
Atlas SLV-3 Burner-2 | United States | Convair | 30.3 m | ~1,000 | No | 1 | 1968 | 1968 | |||
Atlas I | United States | Lockheed Martin | 43.9 m | 5,900 [136] | 2,340 [136] | No | 11 [136] | 1990 | 1997 | ||
Atlas II | United States | Lockheed Martin | 47.5 m | 6,780 [136] | 2,810 | 2,000 to HCO [136] | No | 10 [136] | 1991 | 1998 | |
Atlas IIA | United States | Lockheed Martin | 47.5 m | 7,316 [136] | 3,180 | 2,160 to HCO [136] | No | 23 [136] | 1992 | 2002 | |
Atlas IIAS | United States | Lockheed Martin | 49 m | 8,618 [136] | 3,833 | 2,680 to HCO [136] | No | 30 [136] | 1993 | 2004 | |
Atlas IIIA | United States | Lockheed Martin | 52.5 m | 8,686 [136] | 4,060 | 2,970 to HCO [136] | No | 2 [136] | 2000 | 2004 | |
Atlas IIIB/ DEC | United States | Lockheed Martin | 53.7 m | 10,759 [136] | 4,609 [136] | No | 1 [136] | 2002 | 2002 | ||
Atlas IIIB/ SEC | United States | Lockheed Martin | 54.7 m | 10,218 [138] | 4,193 [136] | No | 3 [136] | 2003 | 2005 | ||
Atlas V 401 | United States | ULA | 57.3 m | 9,050 [139] | 4,950 | 6,670 to SSO | No | 41 [139] | 2002 | 2022 | |
Atlas V 411 | United States | ULA | 58.2 m | 9,050 [139] | 6,075 | 8,495 to SSO | No | 6 [139] | 2006 | 2020 | |
Atlas V 421 | United States | ULA | 59.1 m | 9,050 [139] | 7,000 | 9,050 to SSO | No | 9 [139] | 2007 | 2022 | |
Atlas V 431 | United States | ULA | 59.1 m | 9,050 [139] | 7,800 | 9,050 to SSO | No | 3 [139] | 2005 | 2016 | |
Atlas V 501 | United States | ULA | 62.5 m | 8,250 [139] | 3,970 | 5,945 to SSO 1,500 to GEO |
No | 8 [139] | 2010 | 2023 | |
Atlas V 511 | United States | ULA | 62.5 m | 11,000 [139] | 5,250 | 7,820 to SSO
1,750 to GEO |
No | 1 [140] | 2022 | 2022 | |
Atlas V 521 | United States | ULA | 59.7 m | 13,300 [139] | 6,485 | 9,585 to SSO
2,760 to GEO |
No | 2 [139] | 2003 | 2004 | |
Atlas V 531 | United States | ULA | 59.7 m | 15,300 [139] | 7,425 | 11,160 to SSO
3,250 to GEO |
No | 5 [139] | 2010 | 2022 | |
Atlas V 541 | United States | ULA | 59.7 m | 17,100 [139] | 8,240 | 12,435 to SSO
3,730 to GEO |
No | 9 [139] | 2011 | 2022 |
Vehicle | Origin | Manufacturer | Height | Mass to ... (kg) | Reuse | Launches
(+ suborbital) |
Launch Site (s) | Date of flight | |||
---|---|---|---|---|---|---|---|---|---|---|---|
LEO | GTO | Other | First | Last | |||||||
Delta 0300 | United States | McDonnell Douglas | 34 m | 340 [141] | 747 to SSO [142] | No | 3 [143] | 1972 | 1973 [144] | ||
Delta 0900 | United States | McDonnell Douglas | 34 m | 1,300 [145] | 818 to SSO [143] | No | 2 [143] | 1972 | 1972 | ||
Delta 1410 | United States | McDonnell Douglas | 35.2 m | 340 [146] | No | 1 [143] | 1975 | 1975 | |||
Delta 1604 | United States | McDonnell Douglas | 35.2 m | 390 [147] | No | 2 [143] | 1972 | 1973 | |||
Delta 1900 | United States | McDonnell Douglas | 35.2 m | 1,800 [143] | No | 1 [143] | 1973 | 1973 | |||
Delta 1910 | United States | McDonnell Douglas | 35.2 m | 1,066 [148] | No | 1 [143] | 1975 | 1975 | |||
Delta 1913 | United States | McDonnell Douglas | 35.2 m | 328 [149] | No | 1 [143] | 1973 | 1973 | |||
Delta 1914 | United States | McDonnell Douglas | 35.2 m | 680 [150] | No | 2 [143] | 1972 | 1973 | |||
Delta 2310 | United States | McDonnell Douglas | 35.2 m | 336 [151] | No | 3 [143] | 1974 | 1981 | |||
Delta 2313 | United States | McDonnell Douglas | 35.2 m | 243 to GEO [152] | No | 3 [143] | 1974 | 1977 | |||
Delta 2910 | United States | McDonnell Douglas | 35.2 m | 1,887 [143] | No | 6 [143] | 1975 | 1978 | |||
Delta 2913 | United States | McDonnell Douglas | 35.2 m | 2,000 [153] | 700 [153] | No | 6 [143] | 1975 | 1976 | ||
Delta 2914 | United States | McDonnell Douglas | 35.2 m | 724 [143] | No | 30 [143] | 1974 | 1979 | |||
Delta 3910 | United States | McDonnell Douglas | 35.2 m | 2,494 [143] | 1,154 with PAM-D | No | 10 [143] | 1980 | 1988 | ||
Delta 3913 | United States | McDonnell Douglas | 35.2 m | 816 [154] | No | 1 [143] | 1981 | 1981 | |||
Delta 3914 | United States | McDonnell Douglas | 35.2 m | 954 [143] | No | 13 [143] | 1975 | 1987 | |||
Delta 3920 | United States | McDonnell Douglas | 35.2 m | 3,452 [143] | 1,284 with PAM-D | No | 10 [143] | 1982 | 1989 | ||
Delta 3924 | United States | McDonnell Douglas | 35.2 m | 1,104 [143] | No | 4 [143] | 1982 | 1984 | |||
Delta 4925 | United States | McDonnell Douglas | 35.2 m | 3,400 [155] | 1,312 [143] | No | 2 [143] | 1989 | 1990 | ||
Delta 5920 | United States | McDonnell Douglas | 35.2 m | 3,848 [156] | No | 1 [143] | 1989 | 1989 | |||
Delta II 6920 | United States | McDonnell Douglas | 38.8 m | 3,983 [143] | No | 3 [143] | 1990 | 1992 | |||
Delta II 6925 | United States | McDonnell Douglas | 39.4 m | 1,447 | 1,447 [143] | No | 14 [143] | 1989 | 1992 | ||
Delta II 7320 | United States | Boeing IDS / ULA | 38.9 m | 2,865 [143] | 1,651 to SSO | No | 12 [143] | 1999 | 2015 | ||
Delta II 7326 | United States | Boeing IDS | 38.4 m | 934 [143] | 636 to TLI
629 to HCO |
No | 3 [143] | 1998 | 2001 | ||
Delta II 7420 | United States | ULA | 39 m | 3,185 [143] | 1,966 to SSO | No | 14 [143] | 1998 | 2018 | ||
Delta II 7425 | United States | Boeing IDS | 39 m | 1,100 [143] | 804 to HCO | No | 4 [143] | 1998 | 2002 | ||
Delta II 7426 | United States | Boeing IDS | 39 m | 1,058 [143] | 734 to TLI
711 to HCO |
No | 1 [143] | 1999 | 1999 | ||
Delta II 7920 | United States | Boeing IDS / ULA | 39.4 m | 5,030 [143] | 3,123 to SSO | No | 29 [143] | 1998 | 2017 | ||
Delta II 7925 | United States | Boeing IDS / ULA | 39.4 m | 1,819 [143] | 1,177 to TLI
1,265 to HCO |
No | 69 [143] | 1990 | 2009 | ||
Delta II-H 7920H | United States | Boeing IDS / ULA | 39 m | 6,097 [143] | No | 3 [143] | 2003 | 2011 | |||
Delta II-H 7925H | United States | Boeing IDS / ULA | 39.8 m | 2,171 | 1,508 to HCO [143] | No | 3 [143] | 2003 | 2007 | ||
Delta III 8930 | United States | Boeing IDS | 39 m | 8,292 [143] | 3,810 | No | 3 [143] | 1998 | 2000 | ||
Delta IV Heavy | United States | ULA | 72 m | 28,370 [157] | 14,210 [157] | 23,560 to polar
[157]
11,290 to TLI 8,000 to TMI |
No | 16 [158] | 2004 | 2024 | |
Delta IV M | United States | Boeing IDS | 61.3 m | 9,440 [157] | 4,440 | 7,690 to polar | No | 3 [158] | 2003 | 2006 | |
Delta IV M+(4,2) | United States | ULA | 61.3 m | 13,140 [157] | 6,390 | 10,250 to polar | No | 14 [158] | 2002 | 2019 | |
Delta IV M+(5,2) | United States | ULA | 65.5 m | 11,470 [157] | 5,490 | 9,600 to polar | No | 3 [158] | 2012 | 2018 | |
Delta IV M+(5,4) | United States | ULA | 65.5 m | 14,140 [157] | 7,300 | 11,600 to polar | No | 8 [158] | 2009 | 2019 |
Russian officials have said they plan to discontinue Dnepr launches.
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).
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