Engineering:Comparison of retired orbital launch systems

This comparison of retired orbital launch systems lists the attributes of all retired individual rocket configurations designed to reach orbit. For a list of proposed rocket configurations or individual configurations currently being launched check out: Comparison of Orbital Launch Systems.
Retired rockets
| Vehicle | Origin | Manufacturer | Height | Mass to ... (kg) | Reuse | Launches (+ suborbital) |
Launch Sites | Date of flight | |||
|---|---|---|---|---|---|---|---|---|---|---|---|
| LEO | GTO | Other | First | Last | |||||||
| Antares 110–130 | Orbital | 40.5-41.9 m | 5,100[1] | 1,500 to SSO | No | 5[1] | 2013 | 2014 | |||
| Antares 230 / 230+ | Northrop Grumman | 42.5 m | 8,200[1] | 3,000 to SSO[lower-alpha 1] | No | 13 | 2016 | 2023 | |||
| Ariane 1 | Aérospatiale | 49.1 m | 1,830[2] | No | 11[2] | 1979 | 1986 | ||||
| Ariane 2 | Aérospatiale | 49.1 m | 2,270[2] | No | 6[2] | 1986 | 1989 | ||||
| Ariane 3 | Aérospatiale | 49.1 m | 2,650[2] | No | 11[2] | 1984 | 1989 | ||||
| Ariane 4 40 | Aérospatiale | 58.7 m | 4,600[2] | 2,105 | 2,740 to SSO | No | 7[2] | 1990 | 1999 | ||
| Ariane 4 42L | Aérospatiale | 58.7 m | 7,000[2] | 3,480 | 4,500 to SSO | No | 13[2] | 1993 | 2002 | ||
| Ariane 4 42P | Aérospatiale | 58.7 m | 6,000[2] | 2,930 | 3,400 to SSO | No | 15[2] | 1990 | 2002 | ||
| Ariane 4 44L | Aérospatiale | 58.7 m | 7,000[2] | 4,720 | 6,000 to SSO | No | 40[2] | 1989 | 2003 | ||
| Ariane 4 44LP | Aérospatiale | 58.7 m | 7,000[2] | 4,220 | 5,000 to SSO | No | 26[2] | 1988 | 2001 | ||
| Ariane 4 44P | Aérospatiale | 58.7 m | 6,500[2] | 3,465 | 4,100 to SSO | No | 15[2] | 1991 | 2001 | ||
| Ariane 5 G | EADS Astrium | 47.5 m | 18,000[3] | 6,900[3] | No | 16[3] | 1996 | 2003 | |||
| Ariane 5 G+ | EADS Astrium | 47.8 m | 7,100[3] | No | 3[3] | 2004 | 2004 | ||||
| Ariane 5 GS | EADS Astrium | 47.8 m | 16,000[4] | 6,600[3] | No | 6[3] | 2005 | 2009[5] | |||
| Ariane 5 ES | EADS Astrium | 50.7 m | 21,000[6] | 8,000[3] | No | 8[3] | 2008 | 2018 | |||
| Ariane 5 ECA | EADS Astrium | 52.6 m | 21,000[6] | 11,210[7] | No | 84 | 2002 | 2023 | |||
| ASLV | ISRO[8] | 23.5 m | 150[9] | No | 4[9] | 1987 | 1994 | ||||
| Athena I LLV-1 | Lockheed Martin | 18.4 m | 500 | No | 1 | 1995 | 1995 | ||||
| Athena I | Lockheed Martin | 18.9 m | 795[10] | 515 | No | 3 | 1997 | 2001 | |||
| Athena II | Lockheed Martin | 28.2 m | 1,800[11] | No | 3[12] | 1998 | 1999[13] | ||||
| Black Arrow | RAE | 13 m | 73[14] | No | 2 (+2) | 1969[lower-alpha 2] | 1971 | ||||
| Blue Scout II | Vought | 24 m | 30 | No | 3 | 1961 | 1961 | ||||
| Ceres-1 (1)[lower-alpha 3] | Galactic Energy | 18.5 m | 350 | No | 1 | 2020 | 2020 | ||||
| Ceres-1 (2)[lower-alpha 3] | Galactic Energy | 19.5 m | 400 | No | 1 | 2021 | 2021 | ||||
| Commercial Titan III | Martin Marietta | 47.3 m | 13,100[15] | No | 4 | 1990 | 1992 | ||||
| Conestoga 1620 | Space Services | 15.2 m | 1179 | No | 1 | 1995 | 1995 | ||||
| Diamant A | SEREB | 18.9 m | 80 | No | 4 | 1965 | 1967 | ||||
| Diamant B | SEREB | 23.5 m | 115 | No | 5 | 1970 | 1973 | ||||
| Diamant BP4 | SEREB | 21.6 m | 153 | No | 3 | 1975 | 1975 | ||||
| Dnepr | Yuzhmash | 34.3 m | 3,700[16] | No | 22[16] | 1999 | 2015[17] | ||||
| Energia[lower-alpha 4] | 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 | NPO Energia | 58.8 m | 30,000[18][lower-alpha 5] | Yes | 1 | 1988 | 1988 | ||||
| Epsilon | IHI[19] | 24.4 m | 1,200 | N/A | 450 to SSO | No | 1 | 2013 | 2022 | ||
| Epsilon (enhanced) | IHI[19] | 26 m | 1,500[20] | N/A | 590 to SSO[20] | No | 6[20] | ||||
| Europa I | ELDO | 31.7 m | 1,440 | 200 | No | 3 | 1968 | 1970 | |||
| Europa II | ELDO | 31.7 m | 360 | No | 1 | 1971 | 1971 | ||||
| Falcon 1 | SpaceX | 21 m | 470[21] | No | 5[21] | 2006 | 2009 | ||||
| Falcon 9 v1.0 | SpaceX | 54.9 m | 9,000 | 3,400 | No | 5 | 2010 | 2013 | |||
| Falcon 9 v1.1 | SpaceX | 68.4 m | 13,150[22][lower-alpha 6] | 4,850[22] | No | 15[23] | 2013 | 2016 | |||
| Falcon 9 Full Thrust | SpaceX |
69.8 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 | Shanghai Bureau No.2 | 33 m | 2,500[26] | No | 8 (+3)[27] | 1972 | 1981 | ||||
| Firefly Alpha Block 1 | Firefly Aerospace | 29 m | 1,030[28] | N/A | 630 to SSO[28] | No | 7[29] | 2021 | 2026 | ||
| GSLV Mk.I(a) | ISRO | 49.1 m | 5,000[30] | 1,540[31] | No | 1[31] | 2001 | 2001 | |||
| GSLV Mk.I(b) | ISRO | 49.1 m | 5,000[30] | 2,150[31] | No | 4[31] | 2003 | 2007 | |||
| GSLV Mk.I(c) | ISRO | 49.1 m | 5,000[30] | No | 1[31] | 2010 | 2010 | ||||
| H-I |
|
Mitsubishi | 42 m | 1,400[32] | No | 9 | 1986 | 1992 | |||
| H-II / IIS | Mitsubishi | 49 m | 10,060[33] | 4,000[34] | No | 7[34] | 1994 | 1999 | |||
| H-IIA 202 | Mitsubishi | 53 m | 10,000[35] | 4,000[35] | 5,100 to SSO[lower-alpha 7] | No | 35[37] | 2001 | 2025 | ||
| H-IIA 204 | Mitsubishi | 53 m | 15,000 | 5,950[38]: 48 | No | 5[39] | 2006 | 2021 | |||
| H-IIA 2022 | Mitsubishi | 53 m | 4,500[39] | No | 3[39] | 2005 | 2007 | ||||
| H-IIA 2024 | Mitsubishi | 57 m | 11,000[40] | 5,000[39] | No | 7[39] | 2002 | 2008 | |||
| H-IIB | Mitsubishi | 56.6 m | 16,500 (ISS)[41] | 8,000 | No | 8[42] | 2009 | 2020 | |||
| Hyperbola-1 (1)[lower-alpha 8] | i-Space | 20.9 m | 260 | No | 1 | 2019 | 2019 | ||||
| Juno I | Chrysler | 21.2 m | 11 | No | 1 | 1958 | 1959 | ||||
| Juno II | Chrysler | 24 m | 41 | 6 to TLI | No | 10 | 1958 | 1961 | |||
| Kaituozhe-1 | CALT | 13.6 m | 40 | No | 2 | 2002 | 2003 | ||||
| Kaituozhe-2 | CASC | 16.8 m | 800[43] | No | 1[43] | 2017 | 2017 | ||||
| Kosmos | NPO Polyot | 29.6 m | 350 | No | 38 | 1961 | 1967 | ||||
| Kosmos-1 | NPO Polyot | 26.3 m | 1,400 | No | 8 | 1964 | 1965 | ||||
| Kosmos-2 | NPO Polyot | 31 m | 300 | No | 127 | 1965 | 1977 | ||||
| Kosmos-3 | NPO Polyot | 32.4 m | 1,400 | No | 6 | 1966 | 1968 | ||||
| Kosmos-3M |
|
NPO Polyot | 32.4 m | 1,500[44] | No | 445 | 1967 | 2010 | |||
| Kosmos-3MRB | NPO Polyot | 32.4 m | 1,500 | No | 10 | 1980 | 1988 | ||||
| Lambda 4S | Nissan Motors[45] | 16.5 m | 26[46] | No | 5 | 1966 | 1970 | ||||
| LauncherOne | Virgin Orbit | 21.3 m | 500 | 300 to SSO | No | 6 | 2020 | 2023 | |||
| Long March 1 | CALT | 29.9 m | 300[47] | No | 2[48] | 1970 | 1971 | ||||
| Long March 1D | CALT | 28.2 m | 740[49] | No | 0 (+3)[48] | 1995[lower-alpha 9] | 2002 | ||||
| Long March 2A | CALT | 32 m | 2,000[50] | No | 4[51] | 1974 | 1978 | ||||
| Long March 2E | CALT | 49.7 m | 9,200[51] | No | 7[51] | 1990 | 1995 | ||||
| Long March 3 | CALT | 43.3 m | 5,000[52] | No | 13[52] | 1984 | 2000 | ||||
| Long March 3B | CALT | 54.8 m | 11,200[53] | 5,100 | 5,700 to SSO | No | 12[52] | 1996 | 2012 | ||
| Long March 4A | CALT | 41.9 m | 4,000 | No | 2[54] | 1988 | 1990 | ||||
| M-V | Nissan Motors[45] (1997–2000)
IHI Aerospace[19] (2000–2006) |
30.8 m | 1,850[46] | No | 7 | 1997 | 2006 | ||||
| Molniya | RSC Energia | 43.4 m | 1,800[55] | No | 40[56] | 1960 | 1967 | ||||
| Molniya-M |
|
RSC Energia | 43.4 m | 2,400[57] | No | 280[58] | 1965 | 2010 | |||
| Mu-4S | Nissan Motors[45] | 23.6 m | 180[46] | No | 4 | 1971 | 1972 | ||||
| Mu-3C | Nissan Motors[45] | 20.3 m | 195[46] | No | 4 | 1974 | 1979 | ||||
| Mu-3H | Nissan Motors[45] | 23.8 m | 300[46] | No | 3 | 1977 | 1978 | ||||
| Mu-3S | Nissan Motors[45] | 23.8 m | 300[46] | No | 4 | 1980 | 1984 | ||||
| Mu-3SII | Nissan Motors[45] | 27.8 m | 770[46] | No | 8 | 1985 | 1995 | ||||
| N1 | NPO Energia | 105.3 m | 95,000[lower-alpha 10] | No | 4 | 1969 | 1972 | ||||
| N-I |
|
Mitsubishi | 34 m | 1,200[59] | No | 7 | 1975 | 1982 | |||
| N-II |
|
Mitsubishi | 35 m | 2,000[60] | No | 8 | 1981 | 1987 | |||
| Naro-1 |
|
KARI Khrunichev | 33 m | 100[61] | No | 3 | 2009 | 2013 | |||
| OS-M1 | OneSpace | 19 m | 205[62] | 143 to SSO | No | 1 | 2019[63][lower-alpha 11] | 2019 | |||
| Paektusan-1 | KCST | 25.8 m | 20 | No | 1 | 1998 | 1998 | ||||
| Pegasus | Northrop Grumman | 15.4 m | 455 | No | 6 | 1990 | 1994 | ||||
| Pegasus H | Northrop Grumman | 15.4 m | 544 | No | 4 | 1995 | 2000 | ||||
| Pilot II | United States Navy | 4.4 m | N/A | 1.05 to MEO | No | 10 | 1958 | 1958 | |||
| Polyot | RSC Energia | 30 m | 1,400 | No | 2 | 1963 | 1964 | ||||
| Proton (UR-500) | Khrunichev | 39.8 m | 12,200 | No | 4 | 1965 | 1966 | ||||
| Proton-K |
|
Khrunichev | 50 m | 19,760[65] | 4,930[66] | No | 311[67] | 1965 | 2012 | ||
| Proton-M / Blok DM-03 | Khrunichev | 57.2 m | N/A | 6,000[68] | 3,200 to GEO[69] | No | 8[70] | 2010 | 2026 | ||
| PSLV-G | ISRO | 44 m | 3,200[71] | 1,050 | 1,600 to SSO | No | 12[71] | 1993 | 2016[72] | ||
| Rocket 3.0 | Astra | 11.6 m | 100 | No | 1 | 2020 | 2020 | ||||
| Rocket 3.1 | Astra | 11.6 m | 100 | No | 1 | 2020 | 2020 | ||||
| Rocket 3.2 | Astra | 11.6 m | 100 | No | 1 | 2020 | 2020 | ||||
| Rocket 3.3 | Astra | 13.1 m | 150 to SSO | No | 5 | 2021 | 2022 | ||||
| Rokot-K | Khrunichev | 25.5 m | No | 4 | 1990 | 1999 | |||||
| Rokot-KM | Khrunichev | 29.1 m | 1,950[73] | 1,200 to SSO | No | 31 | 2000 | 2019 | |||
| RS1 B1 | ABL Space Systems | 27 m | 1,350[74] | 400 | 975 to SSO
750 to MEO |
No | 1 | 2023[75] | 2023 | ||
| Safir-1 | Iranian Space Agency | 22.6 m | 27 | No | 2 | 2008 | 2009 | ||||
| Safir-1A | Iranian Space Agency | 22.6 m | 15 | No | 1 | 2011 | 2011 | ||||
| Safir-1B | Iranian Space Agency | 22.6 m | 50 | No | 1 | 2012 | 2012 | ||||
| Safir-1B+ | Iranian Space Agency | 22.6 m | 52 | No | 5 | 2012 | 2019 | ||||
| Saturn I | Chrysler (S-I) | 50-57.4 m | 9,000[76] | No | 10[77] | 1961 | 1965[77] | ||||
| Saturn IB | Chrysler (S-IB) | 56.1-68.1 m | 18,600[78] | No | 9[79] | 1966 | 1975 | ||||
| Saturn V | Boeing (S-IC) | 110.6 m | 47,000 to TLI | No | 13[lower-alpha 12] | 1967 | 1973 | ||||
| Scout X-1 | Vought | 21.8 m | 59 | No | 4 | 1960 | 1961 | ||||
| Scout X-2 | Vought | 21.8 m | 76 | No | 1 | 1962 | 1962 | ||||
| Scout X-2M | Vought | 21.8 m | 76 | No | 3 | 1962 | 1963 | ||||
| Scout X-2B | Vought | 21.8 m | 76 | No | 1 | 1963 | 1963 | ||||
| Scout X-3 | Vought | 21.8 m | 87 | No | 5 | 1962 | 1964 | ||||
| Scout X-3M | Vought | 21.8 m | 87 | No | 1 | 1963 | 1963 | ||||
| Scout X-4 | Vought | 22.8 m | 103 | No | 11 | 1963 | 1965 | ||||
| Scout A | NASA | 22.8 m | 110 | No | 11 | 1965 | 1970 | ||||
| Scout A-1 | NASA | 22.8 m | 122 | No | 1 | 1973 | 1973 | ||||
| Scout B | NASA | 22.8 m | 110 | No | 20 | 1965 | 1971 | ||||
| Scout B-1 | NASA | 22.8 m | 143 | No | 5 | 1971 | 1976 | ||||
| Scout D-1 | NASA | 22.9 m | 182 | No | 14 | 1972 | 1979 | ||||
| Scout E-1 | NASA | 22.8 m | 193 | No | 1 | 1974 | 1974 | ||||
| Scout F-1 | NASA | 22.9 m | 192 | No | 2 | 1975 | 1975 | ||||
| Scout G-1 | NASA | 22.9 m | 208 | No | 18 | 1979 | 1994 | ||||
| Shavit | IAI | 17.7 m | 160 | No | 2 | 1988 | 1990 | ||||
| Shavit-1 | IAI | 19.7 m | 225 | No | 4 | 1995 | 2004 | ||||
| Shtil-1 | Makeyev | 14.8 m | 280–420[80] | No | 2[81] | 1998 | 2006 | ||||
| SLV-3 | ISRO | 22 m | 40[82] | No | 4[82] | 1979 | 1983[82] | ||||
| Soyuz | RSC Energia | 45.6 m | 6,450 | No | 31[83] | 1966 | 1976 | ||||
| Soyuz-FG | TsSKB-Progress | 49.5 m | 6,900[84] | No | 70[85][86] | 2001 | 2019 | ||||
| Soyuz-L | RSC Energia | 50 m | 5,500 | No | 3[87] | 1970 | 1971 | ||||
| Soyuz-M | RSC Energia | 50 m | 6,600 | No | 8[88] | 1971 | 1976 | ||||
| Soyuz ST-A |
|
TsSKB-Progress | 46.3 m | 7,800 from Kourou[89] | 2,810 with Fregat[90] | No | 9[85] | 2011 | 2021 | ||
| Soyuz ST-B |
|
TsSKB-Progress | 46.3 m | 9,000 from Kourou[91] | 3,250 with Fregat[90] | 4,400 to SSO[92] | No | 18[85] | 2011 | 2022 | |
| Soyuz-U |
|
TsSKB-Progress | 51.1 m | 6,650 from Baikonour[93]
6,150 from Plesetsk[93] |
No | 786[85][94][95] | 1973 | 2017 | |||
| Soyuz-U2 |
|
TsSKB-Progress | 34.5 m | 7,050 | No | 72[96] | 1982 | 1995 | |||
| Soyuz-2.1v | TsSKB-Progress | 44.1 m | 2,800[97] | N/A | 2,630 to polar[97] | No | 5[97] | 2018 | 2024 | ||
| Soyuz-2.1v / Volga | TsSKB-Progress | 44.1 m | N/A | N/A | 1,400 to SSO[98] | No | 8[98] | 2013 | 2025 | ||
| Space Shuttle | ATK (SRBs) | 56.1 m | 24,400[lower-alpha 5] | 3,550 to escape with IUS | Yes | 135[101] | 1981 | 2011 | |||
| SPARK | UHAerojet RocketdyneSandia | 17 m | 300 | No | 1 | 2015 | 2015 | ||||
| Sparta | ABMA/Chrysler | 21.8 m | 45 | No | 10 | 1966 | 1967 | ||||
| Sputnik 8K71PS | RSC Energia | 30 m | 500[102] | No | 2 | 1957 | 1957 | ||||
| Sputnik 8A91 | RSC Energia | 31.1 m | 1,327 | No | 2 | 1958 | 1958 | ||||
| SS-520 | IHI Aerospace | 9.5 m | 4[103] | No | 2[104] | 2017[105][lower-alpha 13] | 2018 | ||||
| Start-1 | MITT | 22.7 m | 532 | 250 to SSO | No | 5[106] | 1993 | 2006 | |||
| Start-1.2 | MITT | 22.7 m | 250-300 to SSO | No | 1 | 1997 | 1997 | ||||
| Start | MITT | 28.9 m | 300 to SSO | No | 1 | 1995 | 1995 | ||||
| Strela | Khrunichev | 24-
27.4 m |
1,400[107] | No | 3[108] | 2003 | 2014 | ||||
| Taurus-1110 | Orbital
Sciences, Orbital ATK |
28.2 m | 1180 | 370 | 750 to SSO | No | 3 | 1994 | 2000 | ||
| Taurus-2110 | Orbital
Sciences, Orbital ATK |
29.1 m | 1250 | 375 | 900 to SSO | No | 2 | 1999 | 2001 | ||
| Taurus-2210 | Orbital
Sciences, Orbital ATK |
30.9 m | 1050 | 700 to SSO | No | 1 | 1998 | 1998 | |||
| Taurus-3110 | Orbital
Sciences, Orbital ATK |
30.1 m | 1450 | 445 | 1,050 to SSO | No | 2 | 2009 | 2011 | ||
| Taurus-3210[109] | Northrop Grumman | 27.9 m | 1,458[110] | N/A | 1,054 to SSO[lower-alpha 14] | No | 1 | 2004 | 2004 | ||
| Terran 1 | Relativity Space | 35.2 m | 1,250[111] | 900 to SSO | No | 1 | 2023 | 2023 | |||
| Titan II GLV | Martin Marietta | 33 m | 3,600[112] | No | 11 (+1) | 1964 | 1966 | ||||
| Titan II(23)G | Martin Marietta | 31.4 m | 3,600[113] | No | 13 | 1988 | 2003 | ||||
| Titan IIIA | Martin Marietta | 38.5 m | 3,500 | No | 4 | 1964 | 1965 | ||||
| Titan IIIB | Martin Marietta | 42 m | 3,300 | No | 22 | 1966 | 1969 | ||||
| Titan III(23)B | Martin Marietta | 42 m | 3,350 | No | 9 | 1969 | 1971 | ||||
| Titan III(33)B | Martin Marietta | 42 m | N/A | 4,500 | No | 3 | 1971 | 1973 | |||
| Titan III(24)B | Martin Marietta | 44 m | 4,500 | No | 23 | 1971 | 1984 | ||||
| Titan III(34)B | Martin Marietta | 45.3 m | N/A | No | 11 | 1975 | 1987 | ||||
| Titan IIIC | Martin Marietta | 41 m | 11,500 | 3,000 | No | 14 | 1965 | 1970 | |||
| Titan III(23)C | Martin Marietta | 42.5 m | 13,100[114] | 3,000 | No | 22 | 1970 | 1982 | |||
| Titan IIID | Martin Marietta | 36 m | 12,300[115] | No | 22 | 1971 | 1982 | ||||
| Titan IIIE | Martin Marietta | 48.8 m | 15,400[116] | No | 7 | 1974 | 1977 | ||||
| Titan 34D | Martin Marietta | 44.5 m | 14,350 | 3,600 | No | 15 | 1982 | 1989 | |||
| Titan IVA | Martin Marietta | 51.36 m(standard) | 17,110[117] | 4,944 with IUS | 14,090 to SSO[117]
4,536 to GSO with Centaur 3,550 to escape with IUS |
No | 22[118] | 1989 | 1998 | ||
| Titan IVB | Lockheed Martin | 51.36 m(standard) | 21,682[119] | 5,761[119]
(9,000 with upper stage) |
No | 17[118] | 1997 | 2005 | |||
| Tysklon-2
(R-36-O) |
Yuzhmash | 32 m | 3,350 | No | 18 | 1965 | 1971 | ||||
| Tsyklon-2A | Yuzhmash | 39.7 m | 3,350[120] | No | 8[121] | 1967 | 1969 | ||||
| Tsyklon-2M |
|
Yuzhmash | 39.7 m | 2,820[122] | No | 106[123] | 1969 | 2006[123] | |||
| Tsyklon-3 |
|
Yuzhmash | 39.3 m | 1,920[124] | No | 122[125] | 1977 | 2009[125] | |||
| Unha-2 | KCST | 29.5 m | 80 | No | 1 | 2009 | 2009 | ||||
| Unha-3 | KCST | 30 m | 200[126] | No | 4[127] | 2009[lower-alpha 15] | 2016 | ||||
| Vanguard | Martin | 22.1 m | 9[128] | No | 10 (+1) | 1957 | 1959 | ||||
| Vanguard SLV-7 | Martin | 21.6 m | 20 | No | 1 | 1959 | 1959 | ||||
| Vega | ArianeGroupAvio | 31 m | 2,300[129] | N/A | 1,450 to SSO[130] 1,500 to polar[131] | No | 22[132] | 2012 | 2024 | ||
| VLS-1 | AEB, IAE | 19.5 m | 380[133] | No | 2[lower-alpha 16] | 1997 | 2003 | ||||
| Volna-O | Makeyev | 14.2 m | 100[134] | No | 1 (+5)[81] | 1995[lower-alpha 17] | 2005[81] | ||||
| Voskhod | RSC Energia | 44.1 m | 5,680 | No | 299 | 1963 | 1976 | ||||
| Vostok-L (Luna) | RSC Energia | 30.8 m | 4,000 | 400 to TLI | No | 9 | 1958 | 1960 | |||
| Vostok (Korabl) | RSC Energia | 38.4 m | 4,550 | 390 to TLI[135] | No | 4 | 1960 | 1960 | |||
| Vostok-K | RSC Energia | 30.8 m | 2,460[136] | No | 16 | 1960 | 1964 | ||||
| Vostok-2 | RSC Energia | 30.8 m | 4,730[136] | No | 45 | 1962 | 1967 | ||||
| Vostok-2M | RSC Energia | 38.8 m | 1,300[137] | No | 93 | 1964 | 1991 | ||||
| Soyuz/Vostok | RSC Energia | 31 m | 6,000[138] | No | 2 | 1965 | 1966 | ||||
| Zenit-2 |
|
Yuzhnoye | 57 m | 13,740[139] | No | 36[140] | 1985 | 2004[141] | |||
| Zenit-2FG | Yuzhnoye | 57 m | No | 1 | 2011 | 2011 | |||||
| Zenit-2M | Yuzhnoye | 57 m | 13,920[139] | No | 1 | 2007 | 2007 | ||||
| Zenit-3F | Yuzhnoye | 59.6 m | 1,740 to GEO[142] | No | 4[143] | 2011 | 2017 | ||||
| Zenit-3SL | Yuzhmash
RSC Energia |
59.6 m | 7,000[143] | 6,160 | No | 36[143] | 1999 | 2014 | |||
| Zenit-3SLB | Yuzhmash
RSC Energia |
59.5 m | 3,750[143] | No | 6[143] | 2008 | 2013 | ||||
| Zhuque-1 | LandSpace | 19 m | 300[144] | 200 to SSO | No | 1[145] | 2018[145] | 2018 | |||
Retired Atlas rockets
| Vehicle | Origin | Manufacturer | Height | Mass to ... (kg) | Reuse | Launches (+ suborbital) |
Launch Sites | Date of flight | |||
|---|---|---|---|---|---|---|---|---|---|---|---|
| LEO | GTO | Other | First | Last | |||||||
| Atlas-Able | General Dynamics | 28 m | ~175 to TLI | No | 3 | 1959 | 1960 | ||||
| Atlas-Agena | Convair/General Dynamics | 36 m | 1,000 | 390 to TLI | No | 109 | 1960 | 1978 | |||
| Atlas-Centaur | Lockheed | 36.2-38.8 m | 1,134[146] | 2,222[147] | No | 148 | 1962 | 1983 | |||
| Atlas B | Lockheed Martin | 24.9 m | ~4,000 | No | 10 | 1958 | 1959 | ||||
| Atlas-D OV1 | Convair/General Dynamics | 25.9 m | 1,400 | No | 7 | 1965 | 1967 | ||||
| Atlas E/F-Agena | Convair/General Dynamics/Lockheed | 34 m | 1,000 | 390 to TLI | No | 1 | 1978 | 1978 | |||
| Atlas E/F-Altair-3A | Convair/General Dynamics | 27.3 m | 210 | No | 1 | 1990 | 1990 | ||||
| Atlas E/F-Burner-2 | Convair/General Dynamics | 28.9 m | 950 | No | 1 | 1972 | 1972 | ||||
| Atlas E/F-MSD | Convair/General Dynamics | 27.3 m | 800 | No | 4 | 1976 | 1980 | ||||
| Atlas E/F-OIS | Convair/General Dynamics | 28.7 m | 870 | No | 2 | 1979 | 1985 | ||||
| Atlas E/F-OV1 | Convair/General Dynamics | 26.5 m | 363 | No | 4 | 1968 | 1971 | ||||
| Atlas E/F-PTS | Convair/General Dynamics | 26.5 m | 295 | No | 1 | 1974 | 1974 | ||||
| Atlas E/F-SGS-1 | Convair/General Dynamics | 29 m | 450 | No | 8 | 1977 | 1981 | ||||
| Atlas E/F-SGS-2 | Convair/General Dynamics | 29 m | 770 | No | 4 | 1983 | 1985 | ||||
| Atlas E/F-Star-17A | Convair/General Dynamics | 27.4 m | N/A | 800 to MPEO | No | 1 | 1975 | 1975 | |||
| Atlas E/F-Star-37S | Convair/General Dynamics | 29 m | N/A | 1,100 to SSO | No | 19 | 1978 | 1995 | |||
| Atlas-F Agena-D | Convair/General Dynamics | 34 m | N/A | 2,300 to Polar | No | 1 | 1978 | 1978 | |||
| Atlas G | Lockheed | 43.9 m | 5,900[148] | 2,222 | 1,179 to HCO[148] | No | 7[148] | 1984 | 1989 | ||
| Atlas H MSD | Lockheed | 27 m | 3,630[149] | No | 5 | 1983 | 1987 | ||||
| Atlas LV-3B | Convair | 28.7 m | 1,360 | No | 9 | 1960 | 1963 | ||||
| Atlas SLV-3 | Convair | 33.3 m | No | 63 | 1966 | 1983 | |||||
| Atlas SLV-3 Burner-2 | Convair | 30.3 m | ~1,000 | No | 1 | 1968 | 1968 | ||||
| Atlas I | Lockheed Martin | 43.9 m | 5,900[148] | 2,340[148] | No | 11[148] | 1990 | 1997 | |||
| Atlas II | Lockheed Martin | 47.5 m | 6,780[148] | 2,810 | 2,000 to HCO[148] | No | 10[148] | 1991 | 1998 | ||
| Atlas IIA | Lockheed Martin | 47.5 m | 7,316[148] | 3,180 | 2,160 to HCO[148] | No | 23[148] | 1992 | 2002 | ||
| Atlas IIAS | Lockheed Martin | 49 m | 8,618[148] | 3,833 | 2,680 to HCO[148] | No | 30[148] | 1993 | 2004 | ||
| Atlas IIIA | Lockheed Martin | 52.5 m | 8,686[148] | 4,060 | 2,970 to HCO[148] | No | 2[148] | 2000 | 2004 | ||
| Atlas IIIB/DEC | Lockheed Martin | 53.7 m | 10,759[148] | 4,609[148] | No | 1[148] | 2002 | 2002 | |||
| Atlas IIIB/SEC | Lockheed Martin | 54.7 m | 10,218[150] | 4,193[148] | No | 3[148] | 2003 | 2005 | |||
| Atlas V 401 | ULA | 57.3 m | 9,050[151] | 4,950 | 6,670 to SSO | No | 41[151] | 2002 | 2022 | ||
| Atlas V 411 | ULA | 58.2 m | 9,050[151] | 6,075 | 8,495 to SSO | No | 6[151] | 2006 | 2020 | ||
| Atlas V 421 | ULA | 59.1 m | 9,050[151] | 7,000 | 9,050 to SSO | No | 9[151] | 2007 | 2022 | ||
| Atlas V 431 | ULA | 59.1 m | 9,050[151] | 7,800 | 9,050 to SSO | No | 3[151] | 2005 | 2016 | ||
| Atlas V 501 | ULA | 62.5 m | 8,250[151] | 3,970 | 5,945 to SSO 1,500 to GEO |
No | 8[151] | 2010 | 2023 | ||
| Atlas V 511 | ULA | 62.5 m | 11,000[151] | 5,250 | 7,820 to SSO
1,750 to GEO |
No | 1[152] | 2022 | 2022 | ||
| Atlas V 521 | ULA | 59.7 m | 13,300[151] | 6,485 | 9,585 to SSO
2,760 to GEO |
No | 2[151] | 2003 | 2004 | ||
| Atlas V 531 | ULA | 59.7 m | 15,300[151] | 7,425 | 11,160 to SSO
3,250 to GEO |
No | 5[151] | 2010 | 2022 | ||
| Atlas V 541 | ULA | 59.7 m | 17,100[151] | 8,240 | 12,435 to SSO
3,730 to GEO |
No | 9[151] | 2011 | 2022 | ||
Retired Delta rockets
| Vehicle | Origin | Manufacturer | Height | Mass to ... (kg) | Reuse | Launches (+ suborbital) |
Launch Sites | Date of flight | |||
|---|---|---|---|---|---|---|---|---|---|---|---|
| LEO | GTO | Other | First | Last | |||||||
| Delta 0300 | McDonnell Douglas | 34 m | 340[153] | 747 to SSO[154] | No | 3[155] | 1972 | 1973[156] | |||
| Delta 0900 | McDonnell Douglas | 34 m | 1,300[157] | 818 to SSO[155] | No | 2[155] | 1972 | 1972 | |||
| Delta 1410 | McDonnell Douglas | 35.2 m | 340[158] | No | 1[155] | 1975 | 1975 | ||||
| Delta 1604 | McDonnell Douglas | 35.2 m | 390[159] | No | 2[155] | 1972 | 1973 | ||||
| Delta 1900 | McDonnell Douglas | 35.2 m | 1,800[155] | No | 1[155] | 1973 | 1973 | ||||
| Delta 1910 | McDonnell Douglas | 35.2 m | 1,066[160] | No | 1[155] | 1975 | 1975 | ||||
| Delta 1913 | McDonnell Douglas | 35.2 m | 328[161] | No | 1[155] | 1973 | 1973 | ||||
| Delta 1914 | McDonnell Douglas | 35.2 m | 680[162] | No | 2[155] | 1972 | 1973 | ||||
| Delta 2310 | McDonnell Douglas | 35.2 m | 336[163] | No | 3[155] | 1974 | 1981 | ||||
| Delta 2313 | McDonnell Douglas | 35.2 m | 243 to GEO[164] | No | 3[155] | 1974 | 1977 | ||||
| Delta 2910 | McDonnell Douglas | 35.2 m | 1,887[155] | No | 6[155] | 1975 | 1978 | ||||
| Delta 2913 | McDonnell Douglas | 35.2 m | 2,000[165] | 700[165] | No | 6[155] | 1975 | 1976 | |||
| Delta 2914 | McDonnell Douglas | 35.2 m | 724[155] | No | 30[155] | 1974 | 1979 | ||||
| Delta 3910 | McDonnell Douglas | 35.2 m | 2,494[155] | 1,154 with PAM-D | No | 10[155] | 1980 | 1988 | |||
| Delta 3913 | McDonnell Douglas | 35.2 m | 816[166] | No | 1[155] | 1981 | 1981 | ||||
| Delta 3914 | McDonnell Douglas | 35.2 m | 954[155] | No | 13[155] | 1975 | 1987 | ||||
| Delta 3920 | McDonnell Douglas | 35.2 m | 3,452[155] | 1,284 with PAM-D | No | 10[155] | 1982 | 1989 | |||
| Delta 3924 | McDonnell Douglas | 35.2 m | 1,104[155] | No | 4[155] | 1982 | 1984 | ||||
| Delta 4925 | McDonnell Douglas | 35.2 m | 3,400[167] | 1,312[155] | No | 2[155] | 1989 | 1990 | |||
| Delta 5920 | McDonnell Douglas | 35.2 m | 3,848[168] | No | 1[155] | 1989 | 1989 | ||||
| Delta II 6920 | McDonnell Douglas | 38.8 m | 3,983[155] | No | 3[155] | 1990 | 1992 | ||||
| Delta II 6925 | McDonnell Douglas | 39.4 m | 1,447 | 1,447[155] | No | 14[155] | 1989 | 1992 | |||
| Delta II 7320 | Boeing IDS / ULA | 38.9 m | 2,865[155] | 1,651 to SSO | No | 12[155] | 1999 | 2015 | |||
| Delta II 7326 | Boeing IDS | 38.4 m | 934[155] | 636 to TLI
629 to HCO |
No | 3[155] | 1998 | 2001 | |||
| Delta II 7420 | ULA | 39 m | 3,185[155] | 1,966 to SSO | No | 14[155] | 1998 | 2018 | |||
| Delta II 7425 | Boeing IDS | 39 m | 1,100[155] | 804 to HCO | No | 4[155] | 1998 | 2002 | |||
| Delta II 7426 | Boeing IDS | 39 m | 1,058[155] | 734 to TLI
711 to HCO |
No | 1[155] | 1999 | 1999 | |||
| Delta II 7920 | Boeing IDS / ULA | 39.4 m | 5,030[155] | 3,123 to SSO | No | 29[155] | 1998 | 2017 | |||
| Delta II 7925 | Boeing IDS / ULA | 39.4 m | 1,819[155] | 1,177 to TLI
1,265 to HCO |
No | 69[155] | 1990 | 2009 | |||
| Delta II-H 7920H | Boeing IDS / ULA | 39 m | 6,097[155] | No | 3[155] | 2003 | 2011 | ||||
| Delta II-H 7925H | Boeing IDS / ULA | 39.8 m | 2,171 | 1,508 to HCO[155] | No | 3[155] | 2003 | 2007 | |||
| Delta III 8930 | Boeing IDS | 39 m | 8,292[155] | 3,810 | No | 3[155] | 1998 | 2000 | |||
| Delta IV Heavy | ULA | 72 m | 28,370[169] | 14,210[169] | 23,560 to polar[169]
11,290 to TLI 8,000 to TMI |
No | 16[170] | 2004 | 2024 | ||
| Delta IV M | Boeing IDS | 61.3 m | 9,440[169] | 4,440 | 7,690 to polar | No | 3[170] | 2003 | 2006 | ||
| Delta IV M+(4,2) | ULA | 61.3 m | 13,140[169] | 6,390 | 10,250 to polar | No | 14[170] | 2002 | 2019 | ||
| Delta IV M+(5,2) | ULA | 65.5 m | 11,470[169] | 5,490 | 9,600 to polar | No | 3[170] | 2012 | 2018 | ||
| Delta IV M+(5,4) | ULA | 65.5 m | 14,140[169] | 7,300 | 11,600 to polar | No | 8[170] | 2009 | 2019 | ||
Retired Thor rockets
| Vehicle | Origin | Manufacturer | Height | Mass to ... (kg) | Reuse | Launches (+ suborbital) |
Launch Sites | Date of flight | |||
|---|---|---|---|---|---|---|---|---|---|---|---|
| LEO | GTO | Other | First | Last | |||||||
| Thor-Able I | Douglas/Aerojet | 26.9 m | 250 | No | 3 | 1958 | 1958 | ||||
| Thor-Able II | Douglas/Aerojet | 27.3 m | 270 | No | 4 | 1959 | 1960 | ||||
| Thor-Able III | Douglas/Aerojet | 27.4 m | ~64 to HEO | No | 1 | 1959 | 1959 | ||||
| Thor-Able IV | Douglas/Aerojet | 27.2 m | ~43 to Heliocentric | No | 1 | 1960 | 1960 | ||||
| Thor Agena-A | Douglas/Lockheed | 22.7 m | 860 | No | 16 | 1959 | 1960 | ||||
| Thor Agena-B | Douglas/Lockheed | 26.3 m | 1,200 | No | 21 | 1962 | 1965 | ||||
| Thor Agena-D | Douglas/Lockheed | 29.3 m | 1,150 | No | 22 | 1962 | 1967 | ||||
| Thorad SLV-2G Agena D | Douglas/Lockheed | 32.9 m | 2,000 | No | 30 | 1966 | 1971 | ||||
| Thorad SLV-2H Agena D | Douglas/Lockheed | 34 m | 2,000 | No | 13 | 1969 | 1972 | ||||
| Thor-Burner-1 MG-18 | Douglas | 23 m | 770 | 150-300 to MEO | No | 2 | 1965 | 1965 | |||
| Thor-Burner-1 Altair-3 | Douglas | ~24 m | >73 | No | 4 | 1965 | 1966 | ||||
| Thor-Burner-2 | Douglas | 22.4 m | 250 to MEO | No | 12 | 1966 | 1971 | ||||
| Thor-Burner-2A | Douglas | 23.5 m | 300 to MEO | No | 8 | 1971 | 1976 | ||||
| Thor-Delta | Douglas | 31 m | 226 | 45 | No | 12 | 1960 | 1962 | |||
| Thor-Delta A | Douglas | 31 m | 250 | 68 | No | 2 | 1962 | 1962 | |||
| Thor-Delta B | Douglas | 31 m | 370 | 68 | No | 9 | 1962 | 1964 | |||
| Thor-Delta C | Douglas | 27.5 m | 81 | No | 11 | 1963 | 1967 | ||||
| Thor-Delta C1 | Douglas | 27.5 m | 81 | No | 2 | 1966 | 1969 | ||||
| Thor-Delta D | Douglas | 32 m | 450 | 104 | No | 2 | 1964 | 1965 | |||
| Thor-Delta E | Douglas | 31 m | 540 | 150 | No | 6 | 1965 | 1967 | |||
| Thor-Delta E1 | Douglas | 28 m | 540 | 205 | No | 17 | 1966 | 1971 | |||
| Thor-Delta G | Douglas | 30 m | 650 | No | 2 | 1966 | 1967 | ||||
| Thor-Delta J | Douglas | 31 m | 260 | 263 | No | 1 | 1968 | 1968 | |||
| Thor-Delta L | Douglas | 35 m | 356 | 300 | No | 2 | 1969 | 1972 | |||
| Thor-Delta M | Douglas | 34 m | 356 | 355 | No | 12 | 1968 | 1971 | |||
| Thor-Delta M6 | Douglas | 32.4 m | 454 | 450 | No | 1 | 1971 | 1971 | |||
| Thor-Delta N | Douglas | 33 m | 900 | No | 6 | 1968 | 1972 | ||||
| Thor-Delta N6 | Douglas | 33 m | 1,600 | No | 3 | 1970 | 1971 | ||||
| Thor-DM21 Able-Star | Douglas/Aerojet | 29 m | 150 | No | 11 | 1960 | 1962 | ||||
| Thor-DSV2A Able-Star | Douglas/Aerojet | 29 m | 150 | No | 8 | 1963 | 1965 | ||||
| Thor-ISS | Douglas/Thiokol | 23 m | 500 to MEO | No | 5 | 1976 | 1980 | ||||
| Thor-SLV2A Agena-B | Douglas/Lockheed | 31 m | 400 | No | 2 | 1963 | 1966 | ||||
| Thor-SLV2A Agena-D | Douglas/Lockheed | 29.3 m | 1,500 | No | 60 | 1963 | 1968 | ||||
Notes
- ↑ Reference altitude 500 km
- ↑ First suborbital test in 1969, first orbital launch attempt in 1970
- ↑ 3.0 3.1 Despite not being officially acknowledged by the manufacturer, significant changes between different iterations of the rocket lead to the identification of different variants.[citation needed]
- ↑ Without Buran, and assuming payload providing orbital insertion
- ↑ 5.0 5.1 The U.S. Space Shuttle Transportation System and the Soviet Energia-Buran system consist of launch vehicle rockets and returnable spaceplane orbiter. Payload values listed here are for the mass of the payload in cargo bay of the spaceplanes, excluding the mass of the spaceplanes themselves.
- ↑ The SpaceX website lists the F9 payload to LEO as 13,150kg. The payload to GTO is listed as 4,850kg. However, SpaceX has stated that these numbers include a 30% margin to accommodate re-usability.
- ↑ 5,100 kg to a 500-km Sun-synchronous orbit; 3,300 kg to 800 km[36]: 64–65
- ↑ Despite not being officially acknowledged by the manufacturer, significant changes between different iterations of the rocket lead to the identification of different variants.[citation needed]
- ↑ Suborbital test flights in 1995, 1997 and 2002, no orbital launches attempted
- ↑ The N1 rocket was initially designed for 75 t LEO capacity and launch attempts were made with this version, but there were studies to increase the payload capacity to 90–95 t, if a liquid-hydrogen upper stage engine could be developed.
- ↑ A suborbital test flight was conducted in May 2018.[64]
- ↑ The Saturn V made 13 launches, 12 of which reached the correct orbits, and the other (Apollo 6) reached a different orbit than the one which had been planned; however, some mission objectives could still be completed; NASA, Saturn V News Reference, Appendix: Saturn V Flight History (1968) . For more information, see the Saturn V article. The Saturn V launch record is usually quoted as having never failed, e.g. "The rocket was masterminded by Wernher Von Braun and did not fail in any of its flights", Alan Lawrie and Robert Godwin; Saturn, but the Apollo 6 launch should be considered a partial mission failure. The 13th launch of Saturn V was in special configuration (SA-513) with the Skylab.
- ↑ A prior version of the SS-520 flew twice as a suborbital sounding rocket in 1998 and 2000. In 2017, the addition of a small third stage enabled orbital launches of ultra-light nano- or picosatellites.[103]
- ↑ Reference altitude 400 km
- ↑ A suborbital test flight failed in 2006. The first two orbital missions failed in 2009 and 2012, and the rocket finally reached orbit in late 2012.[127]
- ↑ A third rocket exploded before launch.
- ↑ First orbital launch attempt in 2005
References
- ↑ 1.0 1.1 1.2 Krebs, Gunter. "Antares (Taurus-2)". Gunter's Space Page. https://space.skyrocket.de/doc_lau/antares_osc.htm.
- ↑ 2.00 2.01 2.02 2.03 2.04 2.05 2.06 2.07 2.08 2.09 2.10 2.11 2.12 2.13 2.14 2.15 2.16 2.17 Krebs, Gunter. "Ariane-1, -2, -3, -4". http://space.skyrocket.de/doc_lau/ariane.htm.
- ↑ 3.0 3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 Krebs, Gunter. "Ariane-5". Gunter's Space Page. https://space.skyrocket.de/doc_lau/ariane-5.htm.
- ↑ "Ariane 5". http://andegraf.com/rockets/ariane5.htm.
- ↑ "Final launch of Ariane 5 GS completes busy year / Launchers / Our Activities / ESA". European Space Agency. 2009-12-19. http://www.esa.int/esaCP/SEM5TFAK73G_index_0.html.
- ↑ 6.0 6.1 "Ariane 5 Users Manual". Arianespace. p. 39 (ISS orbit). http://www.arianespace.com/site/documents/Ariane5_users_manual_Issue4.pdf.
- ↑ "Ariane 5 sets new record on latest launch". 24 October 2021. https://www.esa.int/Enabling_Support/Space_Transportation/Ariane/Ariane_5_sets_new_record_on_latest_launch.
- ↑ "Welcome To ISRO :: Launch Vehicles". ISRO. http://www.isro.org/Launchvehicles/launchvehicles.aspx#ASLV.
- ↑ 9.0 9.1 Krebs, Gunter. "SLV-3 / ASLV". http://space.skyrocket.de/doc_lau/slv_aslv.htm.
- ↑ "Athena-1 (LLV-1 / LMLV-1)". http://space.skyrocket.de/doc_lau_det/athena-1.htm.
- ↑ "NASA, Athena Mission Planner's Guide 26 August 2012". https://www.nasa.gov/sites/default/files/files/Athena_MPG_01-23-12.pdf.
- ↑ "Athena-2". Astronautix.com. http://www.astronautix.com/lvs/athena2.htm.
- ↑ "Athena-2 (LLV-2 / LMLV-2)". http://space.skyrocket.de/doc_lau_det/athena-2.htm.
- ↑ Encyclopedia Astronautica, Black Arrow
- ↑ astronautix.com, Titan III
- ↑ 16.0 16.1 Krebs, Gunter. "Dnepr". http://space.skyrocket.de/doc_lau_det/dnepr-1.htm.
- ↑ Clark, Stephen (30 December 2016). "Iridium satellites closed up for launch on Falcon 9 rocket". http://spaceflightnow.com/2016/12/30/iridium-satellites-closed-up-for-launch-on-falcon-9-rocket/. "Russian officials have said they plan to discontinue Dnepr launches."
- ↑ 18.0 18.1 18.2 "S. P. Korolev RSC Energia – LAUNCHERS". Energia. http://www.energia.ru/english/energia/launchers/vehicle_energia.html.
- ↑ 19.0 19.1 19.2 "Projects&Products". IHI Aerospace. http://www.ihi.co.jp/ia/en/product/rocket.html.
- ↑ 20.0 20.1 20.2 Krebs, Gunter. "Epsilon". Gunter's Space Page. https://space.skyrocket.de/doc_lau/epsilon.htm.
- ↑ 21.0 21.1 Krebs, Gunter. "Falcon-1". http://space.skyrocket.de/doc_lau/falcon-1.htm.
- ↑ 22.0 22.1 "Falcon 9". SpaceX. 2012-11-16. http://www.spacex.com/falcon9.
- ↑ Krebs, Gunter. "Falcon-9". http://space.skyrocket.de/doc_lau_fam/falcon-9.htm.
- ↑ 24.0 24.1 24.2 24.3 "Capabilities & Services". SpaceX. http://www.spacex.com/about/capabilities.
- ↑ de Selding, Peter B. (June 15, 2016). "Iridium's SpaceX launch slowed by Vandenberg bottleneck". SpaceNews. http://spacenews.com/iridiums-spacex-launch-slowed-by-vandenberg-bottleneck/.
- ↑ Feng Bao 1, part of CZ family
- ↑ Krebs, Gunter. "FB-1 (Feng Bao-1)". https://space.skyrocket.de/doc_lau/fb-1.htm.
- ↑ 28.0 28.1 "Alpha Launch Vehicle" (in en-US). https://fireflyspace.com/alpha/.
- ↑ "Missions Archive" (in en-US). https://fireflyspace.com/missions/.
- ↑ 30.0 30.1 30.2 "Indian Space Research Organisation - Geosynchronous Satellite Launch Vehicle Mark II". https://www.isro.gov.in/GSLV_CON.html.
- ↑ 31.0 31.1 31.2 31.3 31.4 Krebs, Gunter. "GSLV". http://space.skyrocket.de/doc_lau/gslv.htm.
- ↑ "JERS (Fuyo)". http://space.skyrocket.de/doc_sdat/jers.htm.
- ↑ astronautix.com, H-2
- ↑ 34.0 34.1 Krebs, Gunter. "H-2". http://space.skyrocket.de/doc_lau/h-2.htm.
- ↑ 35.0 35.1 "H-IIA Launch Vehicle". JAXA. https://global.jaxa.jp/activity/pr/brochure/files/rocket01.pdf.
- ↑ "H-IIA – User's Manual". Mitsubishi Heavy Industries, MHI Launch Services. February 2015. https://www.mhi.com/jp/products/pdf/manual.pdf.
- ↑ Krebs, Gunter. "H-2A-202" (in en). https://space.skyrocket.de/doc_lau_det/h-2a-202.htm.
- ↑ "H-IIA – User's Manual". Mitsubishi Heavy Industries, MHI Launch Services. February 2015. https://www.mhi.com/jp/products/pdf/manual.pdf.
- ↑ 39.0 39.1 39.2 39.3 39.4 Krebs, Gunter. "H-2A". http://space.skyrocket.de/doc_lau/h-2a.htm.
- ↑ astronautix.com H-IIA 2024
- ↑ "MHI Launch Services: Launch Vehicles". Mitsubishi Heavy Industries, MHI Launch Services. https://www.mhi.com/products/space/launch_srv_lineup.html.
- ↑ Krebs, Gunter. "H-2B". http://space.skyrocket.de/doc_lau/h-2b.htm.
- ↑ 43.0 43.1 Krebs, Gunter. "Kaituozhe-2 (KT-2)". https://space.skyrocket.de/doc_lau/kaituozhe-2.htm.
- ↑ "Cosmos-1, 3, 3M and 3MU – SL-8 – C-1". http://www.russianspaceweb.com/cosmos3.html.
- ↑ 45.0 45.1 45.2 45.3 45.4 45.5 45.6 "Nissan Heritage Collection online【その他】プリンス自動車工業小史". Nissan Motors. http://nissan-heritage-collection.com/NEWS/publicContents/index.php?procType=CATEGORY&catID=14.
- ↑ 46.0 46.1 46.2 46.3 46.4 46.5 46.6 "Satellite Launch Vehicles". Institute of Space and Astronautical Science (ISAS). http://www.isas.jaxa.jp/e/enterp/rockets/vehicles/index.shtml.
- ↑ astronautix.com, Long March 1, also called CZ-1
- ↑ 48.0 48.1 Krebs, Gunter. "CZ-1 (Chang Zheng-1)". http://space.skyrocket.de/doc_lau/cz-1.htm.
- ↑ astronautix.com, Long March 1D (CZ-1D)
- ↑ astronautix.com Long March 2A – CZ-2A
- ↑ 51.0 51.1 51.2 Krebs, Gunter. "CZ-2 (Chang Zheng-2)". http://space.skyrocket.de/doc_lau/cz-2.htm.
- ↑ 52.0 52.1 52.2 Krebs, Gunter. "CZ-3 (Chang Zheng-3)". http://space.skyrocket.de/doc_lau/cz-3.htm.
- ↑ "LM-3A Series Launch Vehicles User's Manual Issue 2011". 2011. http://www.cgwic.com/LaunchServices/Download/manual/LM-3A%20Series%20Launch%20Vehicles%20User's%20Manual%20Issue%202011.pdf.
- ↑ "CZ-4B (Chang Zheng-4B)" (in en). https://space.skyrocket.de/doc_lau_det/cz-4b.htm.
- ↑ astronautix.com, Encyclopedia Astronautica, Molniya 8K78M
- ↑ Krebs, Gunter. "Molniya (8K78)". http://space.skyrocket.de/doc_lau_det/molniya.htm.
- ↑ "US-K (73D6)". http://space.skyrocket.de/doc_sdat/us-k.htm.
- ↑ Krebs, Gunter. "Molniya and Soyuz with upper stages". http://space.skyrocket.de/doc_lau/molniya.htm.
- ↑ astronautix.com, N-I- Delta
- ↑ astronautix.com, Encyclopedia Astronautica, N-2
- ↑ "STSAT 2C". http://space.skyrocket.de/doc_sdat/stsat-2c.htm.
- ↑ Goh, Deyana (5 July 2018). "Chinese startup One Space successfully tests first stage engine for orbital rocket". Spacetech Asia. http://www.spacetechasia.com/chinese-startup-one-space-successfully-tests-first-stage-engine-for-orbital-rocket/.
- ↑ Krebs, Gunter. "OS-M (Chongqing SQX)". https://space.skyrocket.de/doc_lau/os-m.htm.
- ↑ Jones, Andrew (17 May 2018). "Chinese company OneSpace sends OS-X rocket to 40 km in maiden flight". GBTimes. https://gbtimes.com/chinese-company-onespace-sends-os-x-rocket-to-40-km-in-maiden-flight.
- ↑ Encyclopedia Astronautica, Proton-K
- ↑ "Launch Vehicles". http://abyss.uoregon.edu/~js/space/lectures/lec17.html.
- ↑ "Proton". Astronautix.com. http://www.astronautix.com/lvs/proton.htm.
- ↑ "Proton-M | Khrunichev | Next Spaceflight" (in en). https://nextspaceflight.com/rockets/40/.
- ↑ Krebs, Gunter. "Proton (UR-500) Family" (in en). https://space.skyrocket.de/doc_lau_fam/proton.htm.
- ↑ Krebs, Gunter. "Proton-M Blok-DM-03" (in en). https://space.skyrocket.de/doc_lau_det/proton-m_blok-dm-03.htm.
- ↑ 71.0 71.1 "PSLV-CA (2)" (in en). https://space.skyrocket.de/doc_lau_det/pslv-ca_2.htm.
- ↑ "Outcome Budget 2016–2017". Government of India, Department of Space. 2016. https://www.isro.gov.in/sites/default/files/article-files/node/7064/outcomebudget2016-2017.pdf. "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)."
- ↑ Krebs, Gunter. "Rokot (Rockot)". https://space.skyrocket.de/doc_lau/rokot.htm.
- ↑ "ABL Space Systems". https://www.ablspacesystems.com.
- ↑ "ABL Space Systems maiden flight fails after liftoff". 10 February 2023. https://www.nasaspaceflight.com/2023/01/abl-rs1-demo-1/.
- ↑ astronautix.com, Saturn I
- ↑ 77.0 77.1 "Saturn-1 & Saturn-1B". Space.skyrocket.de. http://space.skyrocket.de/doc_lau/saturn-1.htm.
- ↑ Encyclopedia Astronautica, Saturn IB
- ↑ Bilstein, Roger E.. "Appendix C: Saturn Family/Mission Data". NASA History Office. https://history.nasa.gov/SP-4206/app-c.htm.
- ↑ "Vysota / Volna / Shtil". http://space.skyrocket.de/doc_lau/shtil_volna.htm.
- ↑ 81.0 81.1 81.2 "Vysota / Volna / Shtil". http://space.skyrocket.de/doc_lau/shtil_volna.htm.
- ↑ 82.0 82.1 82.2 "SLV-3". https://b14643.eu/Spacerockets_1/India/SLV/Description/Frame.htm.
- ↑ Krebs, Gunter. "Soyuz (11A511)". http://space.skyrocket.de/doc_lau_det/soyuz.htm.
- ↑ "Soyuz-FG Launch Vehicle". Progress Rocket Space Centre. http://en.samspace.ru/products/launch_vehicles/rn_soyuz_fg/.
- ↑ 85.0 85.1 85.2 85.3 Krebs, Gunter. "Soyuz with Fregat upper stage". http://space.skyrocket.de/doc_lau/soyuz_fregat.htm.
- ↑ Krebs, Gunter. "Soyuz-FG (11A511U-FG)". http://space.skyrocket.de/doc_lau_det/soyuz-fg.htm.
- ↑ Krebs, Gunter. "Soyuz-L (11A511L)". http://space.skyrocket.de/doc_lau_det/soyuz-l.htm.
- ↑ Krebs, Gunter. "Soyuz-M (11A511M)". http://space.skyrocket.de/doc_lau_det/soyuz-m.htm.
- ↑ "Soyuz-ST". Encyclopedia Astronautica. http://www.astronautix.com/lvs/soyuzst.htm. Retrieved 17 May 2015.
- ↑ 90.0 90.1 "Soyuz-ST Launch Vehicle". Progress Rocket Space Centre. http://en.samspace.ru/products/launch_vehicles/rn_soyuz_st/.
- ↑ "Soyuz 2 Launch Vehicle". http://www.russianspaceweb.com/soyuz2_lv.html.
- ↑ "Soyuz overview". Arianespace. http://www.arianespace.com/vehicle/soyuz/.
- ↑ 93.0 93.1 "Soyuz-U Launch Vehicle". http://en.samspace.ru/products/launch_vehicles/rn_soyuz_u/.
- ↑ Krebs, Gunter. "Soyuz with Ikar and Volga upper stages". http://space.skyrocket.de/doc_lau/soyuz_ikar-volga.htm.
- ↑ Krebs, Gunter. "Soyuz-U (11A511U)". http://space.skyrocket.de/doc_lau_det/soyuz-u.htm.
- ↑ Krebs, Gunter. "Soyuz-U2 (11A511U2)". http://space.skyrocket.de/doc_lau_det/soyuz-u2.htm.
- ↑ 97.0 97.1 97.2 Krebs, Gunter. "Soyuz-2-1v (Soyuz-1)" (in en). https://space.skyrocket.de/doc_lau_det/soyuz-2-1v.htm.
- ↑ 98.0 98.1 Krebs, Gunter. "Soyuz-2-1v Volga (Soyuz-1 Volga)" (in en). https://space.skyrocket.de/doc_lau_det/soyuz-2-1v_volga.htm.
- ↑ Krebs, Gunter. "Shuttle (STS)". http://space.skyrocket.de/doc_lau/sts.htm.
- ↑ "SPACE TRANSPORTATION SYSTEM PAYLOADS". Kennedy Space Center. 2000. http://science.ksc.nasa.gov/shuttle/technology/sts-newsref/carriers.html.
- ↑ "NASA – Space Shuttle". NASA. http://www.nasa.gov/mission_pages/shuttle/main/index.html.
- ↑ "Sputnik 2 (PS-2 #1)". http://space.skyrocket.de/doc_sdat/sputnik-2.htm.
- ↑ 103.0 103.1 Krebs, Gunter. "SS-520". http://space.skyrocket.de/doc_lau/ss-520.htm.
- ↑ Graham, William (3 February 2018). "Japanese sounding rocket claims record-breaking orbital launch". NASASpaceFlight. https://www.nasaspaceflight.com/2018/02/japanese-rocket-record-borbital-launch/.
- ↑ "Experimental Launch of World's Smallest Orbital Space Rocket ends in Failure". Spaceflight 101. 14 January 2017. http://spaceflight101.com/ss-520-4-rocket-launches-on-experimental-mission/.
- ↑ "Start-1". http://space.skyrocket.de/doc_lau_det/start-1.htm.
- ↑ "Strela launcher". http://www.russianspaceweb.com/strela.html.
- ↑ "Strela". Gunter's Space Page. http://space.skyrocket.de/doc_lau/strela.htm.
- ↑ "Taurus". Orbital Sciences Corporation. 2012. http://www.orbital.com/spacelaunch/taurus/.
- ↑ "Taurus / Minotaur-C" (in en). https://space.skyrocket.de/doc_lau/taurus.htm.
- ↑ "Terran". https://www.relativityspace.com/rockets.
- ↑ astronautix.com, Titan II GLV
- ↑ astronautix.com, Titan 23G
- ↑ astronautix.com, Titan IIIC
- ↑ astronautix.com, Titan IIID
- ↑ astronautix.com, Titan IIIE
- ↑ 117.0 117.1 "Titan-4". http://space.skyrocket.de/doc_lau/titan-4.htm.
- ↑ 118.0 118.1 "Titan-4". Space.skyrocket.de. http://space.skyrocket.de/doc_lau/titan-4.htm.
- ↑ 119.0 119.1 "Fact Sheet – Titan IVB". United States Air Force. https://www.maxwell.af.mil/au/awc/space/factsheets/titan_ivb.htm.
- ↑ astronautix.com, Tsyklon-2A
- ↑ "Tsiklon-2A (11K67)". Space.skyrocket.de. http://space.skyrocket.de/doc_lau_det/tsiklon-2a.htm.
- ↑ astronautix.com, Tsyklon-2
- ↑ 123.0 123.1 "Tsiklon-2 (11K69)". Space.skyrocket.de. http://space.skyrocket.de/doc_lau_det/tsiklon-2.htm.
- ↑ nasaspaceflight.com, Tsyklon-3
- ↑ 125.0 125.1 "Tsiklon-3 (11K68)". Space.skyrocket.de. http://space.skyrocket.de/doc_lau_det/tsiklon-3.htm.
- ↑ https://web.archive.org/web/20191112061955/http://spaceflight101.com/status-of-north-korean-satellite-unknown-after-prolonged-radio-silence-reports-of-tumbling/
- ↑ 127.0 127.1 Krebs, Gunter. "Unha ("Taepodong-2")". http://space.skyrocket.de/doc_lau/unha.htm.
- ↑ astronautix.com, vanguard
- ↑ Krebs, Gunter. "Vega (P80 based)" (in en). https://space.skyrocket.de/doc_lau/vega_p80.htm.
- ↑ "Vega User's Manual, Issue 4, Revision 0". Arianespace. April 2014. p. 38. https://www.arianespace.com/wp-content/uploads/2018/05/Vega-Users-Manual_Issue-04_April-2014.pdf.
- ↑ "Vega". Arianespace. https://www.arianespace.com/vehicle/vega/.
- ↑ Parsonson, Andrew (2024-09-05). "First-Gen Vega Rocket Retired After Successful Sentinel-2C Launch" (in en-US). https://europeanspaceflight.com/first-gen-vega-rocket-retired-after-successful-sentinel-2c-launch/.
- ↑ "VLS". http://space.skyrocket.de/doc_lau/vls.htm.
- ↑ "IRDT 1, 2, 2R". http://space.skyrocket.de/doc_sdat/irdt-1.htm.
- ↑ "NASA – NSSDCA – Spacecraft – Details". https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=1959-014A.
- ↑ 136.0 136.1 "Spacecraft – Vostok". http://www.braeunig.us/space/specs/vostok.htm.
- ↑ "Meteor-2 (11F632)". http://space.skyrocket.de/doc_sdat/meteor-2.htm.
- ↑ astronautix.com, Soyuz/Vostok
- ↑ 139.0 139.1 Kyle, Ed. "Zenit Data Sheet". Spacelaunchreport.com. http://www.spacelaunchreport.com/zenit.html.
- ↑ Krebs, Gunter. "Zenit-2". http://space.skyrocket.de/doc_lau/zenit-2.htm.
- ↑ "Zenit launch vehicle". Russianspaceweb.com. http://www.russianspaceweb.com/zenit.html.
- ↑ "Elektro-L 1, 2, 3". http://space.skyrocket.de/doc_sdat/elektro-l.htm.
- ↑ 143.0 143.1 143.2 143.3 143.4 Krebs, Gunter. "Zenit-3". http://space.skyrocket.de/doc_lau/zenit-3.htm.
- ↑ Jones, Andrew (2 August 2018). "Landspace of China to launch first rocket in Q4 2018". SpaceNews. https://spacenews.com/landspace-of-china-to-launch-first-rocket-in-q4-2018.
- ↑ 145.0 145.1 Barbosa, Rui C. (27 October 2018). "Chinese commercial provider LandSpace launches Weilai-1 on a Zhuque-1 rockets – fails to make orbit". NASASpaceFlight.com. https://www.nasaspaceflight.com/2018/10/chinese-landspace-launches-weilai-1-zhuque-1-rocket/.
- ↑ "Atlas Centaur LV-3C Development". 25 March 2023. http://www.spacelaunchreport.com/aclv3cb.html.
- ↑ "Atlas Centaur". http://space.skyrocket.de/doc_lau/atlas_centaur.htm.
- ↑ 148.00 148.01 148.02 148.03 148.04 148.05 148.06 148.07 148.08 148.09 148.10 148.11 148.12 148.13 148.14 148.15 148.16 148.17 148.18 148.19 148.20 148.21 148.22 Krebs, Gunter. "Atlas Centaur". http://space.skyrocket.de/doc_lau/atlas_centaur.htm.
- ↑ astronautix.com, Atlas H
- ↑ astronautix.com, Atlas IIIB
- ↑ 151.00 151.01 151.02 151.03 151.04 151.05 151.06 151.07 151.08 151.09 151.10 151.11 151.12 151.13 151.14 151.15 151.16 "Atlas V". https://www.ulalaunch.com/rockets/atlas-v.
- ↑ "ULA launches two space surveillance satellites for U.S. Space Force" (in en-US). 2022-01-21. https://spacenews.com/ula-launches-two-space-surveillance-satellites-for-u-s-space-force/.
- ↑ "WMO OSCAR – Satellite: NOAA-3". http://www.wmo-sat.info/oscar/satellites/view/325.
- ↑ "NASA – NSSDCA – Spacecraft – Details". https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=ITOS-E1.
- ↑ 155.00 155.01 155.02 155.03 155.04 155.05 155.06 155.07 155.08 155.09 155.10 155.11 155.12 155.13 155.14 155.15 155.16 155.17 155.18 155.19 155.20 155.21 155.22 155.23 155.24 155.25 155.26 155.27 155.28 155.29 155.30 155.31 155.32 155.33 155.34 155.35 155.36 155.37 155.38 155.39 155.40 155.41 155.42 155.43 155.44 155.45 155.46 155.47 155.48 155.49 155.50 155.51 155.52 Krebs, Gunter. "Delta". http://space.skyrocket.de/doc_lau/delta.htm.
- ↑ Wade, Mark. "Delta 0300". http://www.astronautix.com/lvs/dela0300.htm.
- ↑ Wade, Mark. "Delta 0900". http://www.astronautix.com/lvs/dela0900.htm.
- ↑ "GEOS 3". http://space.skyrocket.de/doc_sdat/geos-3.htm.
- ↑ "1972 – 2616 – Flight Archive". https://www.flightglobal.com/pdfarchive/view/1972/1972%20-%202616.html.
- ↑ "OSO 8". http://space.skyrocket.de/doc_sdat/oso-8.htm.
- ↑ "Explorer: RAE B". http://space.skyrocket.de/doc_sdat/explorer_rae-b.htm.
- ↑ "Delta-1914". http://space.skyrocket.de/doc_lau_det/delta-1914.htm.
- ↑ "NASA – NSSDCA – Spacecraft – Details". https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=1976-077A.
- ↑ "Skynet 2A, 2B". http://space.skyrocket.de/doc_sdat/skynet-2.htm.
- ↑ 165.0 165.1 Wade, Mark. "Delta 2913". http://www.astronautix.com/lvs/dela2913.htm.
- ↑ "Explorer: DE 1, 2". http://space.skyrocket.de/doc_sdat/explorer_de.htm.
- ↑ Wade, Mark. "Delta 4000". http://www.astronautix.com/lvs/dela4000.htm.
- ↑ Wade, Mark. "Delta 5000". http://www.astronautix.com/lvs/dela5000.htm.
- ↑ 169.0 169.1 169.2 169.3 169.4 169.5 169.6 "Delta IV". https://www.ulalaunch.com/rockets/delta-iv.
- ↑ 170.0 170.1 170.2 170.3 170.4 Krebs, Gunter. "Delta-4". http://space.skyrocket.de/doc_lau/delta-4.htm.
