
This article compares differentorbital launcher families (launchers which are significantly different from other members of the same 'family' have separate entries). The article is organized into two tables: the first contains a list ofcurrently active and under-development launcher families, while the second contains a list ofretired launcher families.
The related article "Comparison of orbital launch systems" lists each individual launcher system within any given launcher family, categorized by its currentoperational status.
This article does not include suborbital launches (i.e. flights which were not intended to reach LEO or VLEO).
Same cores are grouped together (like Ariane 1, 2 & 3, but not V).
| Family | Country/Org. | Manufac. | Payload (kg) | Cost (US$, millions) | Launches reaching... | Status | Date of flight | Notes | Refs | |||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| LEO | GTO | TLI | Total | Space | Any orbit | Target orbit | First | Last | ||||||||
| Agnibaan | AgniKul Cosmos | 100 | -- | -- | -- | Devel. | NET 2023 | Expected launch in 2022 | ||||||||
| Alpha | Firefly Aerospace | 1,000 | — | — | -- | 6[a] | 5 | 4 | 2 | Active | 2021 | [1] | ||||
| Angara | Khrunichev | 3,800–35,000 | 3,600–12,500 | -- | -- | 11[b] | 11 | 11 | 9 | Active | 2014 | [2][3] | ||||
| Antares | Orbital ATK | 8,000 | -- | -- | 80[citation needed] | 18[c] | 17 | 17 | 17 | Active[d] | 2013 | Cygnus launcher. Var.: 110, 120, 130, 230, 230+, 330 | [4][5][6] | |||
| Ariane 6 | ArianeGroup | 21,650 (A64var.) | 11,500+ (A64var.) | 8,500 (A64var.) | 115 | 4[e] | 4 | 4 | 4 | Active | 2024 | Var.: Ariane 62, Ariane 64. | [7] | |||
| Astra Rocket | Astra | 50–150 (to SSO) | — | — | -- | 7[f] | 4 | 2 | 2 | Active | 2020 | 2 suborbital test launches in 2018. | [8] | |||
| Atlas V | ULA | 18,850 | 8,900 | 2,807 | 109–153 | 105[g] | 105 | 105 | 105 | Active[h] | 2002 | 2029 (planned) | LaunchedJuno &New Horizons | [9][10] | ||
| Blue Whale 1 | Perigee Aerospace | 170(to SSO) | -- | -- | -- | 0 | Devel. | NET 2024 | [11] | |||||||
| Ceres | Galactic Energy | 400 (LEO) 300 (SSO) | -- | -- | -- | 22[i] | 21 | 20 | 20 | Active | 2020 | Var.: Ceres-1, Ceres-1S | [12][13][14] | |||
| 1,600[14] (LEO) 1,300 (500 km SSO) | -- | -- | -- | Var.: Ceres-2 | ||||||||||||
| Chollima-1 | NADA | ~300 | -- | -- | -- | 4[j] | 2 | 1 | 1 | Active | 2023 | UDMH/N2O4 fueled carrier | [15] | |||
| Cyclone-4M | Yuzhnoye Yuzhmash | 5,000 | 1,000 | -- | -- | 0 | Devel. | unknown | [16] | |||||||
| Electron | Rocket Lab | 225 | 6 | 71[k] | 71 | 67 | 67 | Active | 2017 | [17][18] | ||||||
| Epsilon | IHI Corporation | 1,200 | -- | -- | -- | 6[l] | 6 | 5 | 5 | Active | 2013 | [19][20] | ||||
| Eris | Gilmour Space Technologies | 305 | -- | -- | -- | 1[m] | 0 | 0 | 0 | Active | 2025 | [21] | ||||
| Falcon | Falcon 9 | SpaceX | 22,800 | 8,300 | -- | 61.2 | 568[n][o] | 566 | 566 | 565 | Active | 2010 | Var.: v1.0, v1.1,[p] FT,[q] Block 4, Block 5. Launcher of crewedDragon capsule. | |||
| Falcon Heavy | SpaceX | 63,800 | 26,700 | -- | 90–150 | 11[r] | 11 | 11 | 11 | Active | 2018 | First test launch 2018-02-06 | [24][25][26] | |||
| Gravity-1 | Orienspace | 6,500(LEO) 3,700(700 km SSO) | -- | -- | -- | 2[s] | 2 | 2 | 2 | Active | 2024 | largest solid launcher (3rd stage can be solid/kerolox) | [27][28] | |||
| Gravity-2 | Orienspace | 25,600(LEO) 19,100(SSO) | 7,700 | -- | -- | 0 | Devel. | 2025 | kerolox (core), solid (boosters); reusable 1st stage | [28] | ||||||
| GSLV Mark II | ISRO | 5,000 | 2,700 | -- | -- | 12[t] | 11 | 10 | 10 | Active | 2010 | [29][30][31] | ||||
| H3 | Mitsubishi | 4,000–28,300(base-heavy) | 7,900–14,800(base-heavy) | 11,900(heavy) | 6[u] | 6 | 5 | 5 | Active | 2023 | Var.: 30S, 22S, 32L, 24L, heavy[32][33] | [33] | ||||
| Hyperbola-1 | i-Space | 300 | -- | -- | 8[v] | 6 | 4 | 4 | Active | 2019 | [34] | |||||
| Hyperbola-3 | i-Space | 8,500–13,400 | -- | -- | 0 | Devel. | 2025 | VTVL | [35] | |||||||
| Jielong 1 | CALT | 200(SSO) | -- | -- | 1[w] | 1 | 1 | 1 | Active | 2019 | [36] | |||||
| Jielong 3 | CALT | 1,600 (500 km SSO)[37] | -- | -- | -- | 8[x] | 8 | 8 | 8 | Active | 2022 | [37][38][39] | ||||
| KAIROS | Space One | 250 150 (SSO) | -- | -- | 2[y] | 0 | 0 | 0 | Active | 2024 | [40] | |||||
| Kuaizhou (DF-21) | CASIC | 450(KZ-1A Enhanced) | -- | -- | -- | 34[z][aa] | 33[ab] | 31 | 31 | Active | 2013 | Var.: KZ-1, KZ-1A, KZ-11; (KZ-21 under development) | [41][42] | |||
| 1,500(KZ-11) | -- | -- | ||||||||||||||
| LauncherOne | Virgin Orbit | 300(SSO) | -- | -- | -- | 6[ac] | 5 | 4 | 4 | Susp.[ad] | 2020 | [43] | ||||
| Lijian-1 (Kinetica-1) | CAS Space | 1,500 (500 km SSO) | -- | -- | -- | 10[ae] | 10 | 9 | 9 | Active | 2022 | solid fueled carrier | [38][27] | |||
| Lijian-2 (Kinetica-2) | CAS Space | 12,000 (LEO) 7800 (SSO) | -- | -- | -- | 0 | Devel. | 2025 | kerolox LV. reusable 1st stage | [44][45] | ||||||
| Long March 2–3–4 (DF-5) | CALT+SAST | 12,000 | 5,500 | 3,300 | 507[af][ag] | 501[ah] | 498 | 490 | Active | 1971 | See notes | Var.: 2A, 2C, 2D, 2E, 2F,[ai] 3, 3A, 3B, 3B/E, 3C, 4A, 4B, 4C. See[aj] for retiredvar. among those listed here. | [47] | |||
| Long March 5 | CALT | -- | 14,000 | 8,000 | -- | 16[ak] | 16 | 15 | 15 | Active | 2016 | Var.: CZ-5 | [48][49] | |||
| 25,000 | -- | -- | Var.: CZ-5B | |||||||||||||
| CZ 6–7–8 family | Long March 6 | SAST | 1,500(LEO) 1,080(700 lm SSO) | -- | -- | -- | 33[al] | 33 | 33 | 33 | Active | 2015 | Var.: 6 | [50][51] | ||
| 4,500(700 km SSO) | -- | -- | Var.: 6A | |||||||||||||
| 2,400 (500 km SSO) | -- | -- | Var.: 6C | |||||||||||||
| Long March 7 | CALT | 14,000 | -- | -- | -- | 22[am] | 21 | 21 | 21 | Active | 2016 | Var.: 7 | [52][53][54] | |||
| -- | 7,000 | -- | Var.: 7A | |||||||||||||
| Long March 8 | CALT | 4,500(SSO) | 2,800 | >1,200 | -- | 8[an] | 8 | 8 | 8 | Active | 2020 | Var.: 8 | [53][55][56][57] | |||
| 7,000(700 km SSO) | -- | -- | Var.: 8A | |||||||||||||
| Long March 9 | CALT | 150,000 | -- | 50,000 | -- | 0 | Devel. | 2033 | partly-reusable Super-Heavy carrier | [55][58] | ||||||
| Long March 10 | CALT | 70,000(CZ-10)[59] | -- | 27,000 (CZ-10)[58] | -- | 0 | Devel. | 2026 | Human-rated Var.: 10 (3-core, TLI) | [60][61][59][58][62] | ||||||
| 14,000(CZ-10A, reusable) | -- | -- | Human-rated Var.: 10A (1-core, LEO, partly reusable) | |||||||||||||
| 18,000(CZ-10A, expendable) | -- | -- | Human-rated Var.: 10A (1-core, LEO, expendable) | |||||||||||||
| Long March 11 | CALT | 1,000 | -- | -- | -- | 18[ao] | 18 | 18 | 18 | Active | 2015 | Likely based onDF-31 missile | [63] | |||
| Long March 12 | SAST | 12,000(LEO); 6,000(700 km SSO) | -- | -- | -- | 3[ap] | 3 | 3 | 3 | Active | 2024 | kerolox LV 3.8 metres diameter | [64][65][66] | |||
| LVM3 | ISRO | 10,000 | 4,000 | 2,180 | -- | 7[aq][ar] | 7 | 7 | 7 | Active | 2014 | Uprated cryo 2nd stage (C32) and semi-cryo 1st stage (SC120) variants expected | [67][68] | |||
| Maia | MaiaSpace | 500(SSO) | -- | -- | 0 | Devel. | 2025 | Planned first stage reuse | [69] | |||||||
| Minotaur I | Orbital ATK | 580 | -- | -- | -- | 12[as] | 12 | 12 | 12 | Active | 2000 | Derived from the Minuteman II | [70][71] | |||
| Minotaur IV &V | Orbital ATK | 1,735 | 640 | 447 | 50 | 9[at] | 9 | 9 | 9 | Active | 2010 | Also 2 suborbital launches (HTV-2a).Var.: IV, IV Lite, IV HAPS, V. Derived from Peacekeeper missile | [70][72] | |||
| Miura 5 | PLD Space | 900 | -- | -- | 0 | Devel. | NET 2024 | [73] | ||||||||
| MLV | Firefly Aerospace | 14,000 | -- | -- | -- | 0 | Devel. | 2025 | [74] | |||||||
| Nebula-1 | Deep Blue Aerospace | 1,000 | -- | -- | 0 | Devel. | 2024 | VTVL (first stage) | [75] | |||||||
| Nebula-2 | Deep Blue Aerospace | 20,000 | -- | -- | 0 | Devel. | 2025 | kerolox; VTVL (first stage) | [76] | |||||||
| Neutron | Rocket Lab | 15,000 | -- | 2,000 | 50 | 0 | Devel. | 2024 | [77] | |||||||
| New Glenn | Blue Origin | 45,000 | 13,000 | -- | 2[au] | 2 | 2 | 2 | Active | 2025 | [78] | |||||
| New Line 1 | LinkSpace | 200(SSO) | -- | -- | 0 | Devel. | unknown | [79] | ||||||||
| NGLV (Soorya) | ISRO | 30,000[80] | 10,000 | -- | -- | 0 | Devel. | NET 2032 | Program approved in 2024 | [81] | ||||||
| Nuri | KARI | 1,500 | -- | -- | 3[av] | 3 | 2 | 2 | Active | 2021 | [82][83] | |||||
| OS-M | OneSpace | 205(M1) | -- | -- | -- | 1[aw] | 0 | 0 | 0 | Active | 2019 | Var.: M1, M2, M4. Single M1 failed launch; M2 & M4 in development. | [84] | |||
| Pallas-1 | Galactic Energy | 5,000 3,000(SSO) | -- | -- | -- | 0 | Devel. | 4th Qt 2025 | kerolox LV with reusable 1st stage | [85][45] | ||||||
| Pallas-2 | Galactic Energy | 20,000 | 7,500 | -- | -- | 0 | Devel. | NET 4th Qt 2026 | Var.: 1-core | [86] | ||||||
| 58,000 | -- | -- | Var.: 3-core | |||||||||||||
| Pegasus | Orbital ATK | 450 | -- | -- | -- | 45[ax] | 44 | 42 | 40 | Active | 1990 | [87] | ||||
| Pioneer-1 (akaYuanxingzhe-1 orXZY-1) | Arrowhead Technology/Space Epoch | 6,500(1,100 km LEO) | -- | -- | 0 | Devel. | 2025 | first stage recovery via ocean landing | [88][89] | |||||||
| Prime | Orbex | 150(SSO) | -- | -- | -- | 0 | Devel. | NET 2023 | [90][91] | |||||||
| Proton (UR-500) | Khrunichev | 23,000 | 6,920 | 5,680 | 65 (Proton-M) | 430[ay] | 382 | Active | 1965 | Var.: K, M, Medium in development. | [92][93][94] | |||||
| PSLV | ISRO | 3,800 | 1,200 | 550 | -- | 63[az] | 62 | 60 | 59 | Active | 1993 | Var.: CA, XL, QL, DL Launched moon probe Chandrayaan I, Mars probe Mangalyaan I | [95][96] | |||
| Qaem-100 | IRGC | 80 | -- | -- | -- | 3[ba] | 3 | 2 | 2 | Active | 2023 | also one successful suborbital launch | [97] | |||
| Qased | IRGC | ~50 | -- | -- | -- | 3[bb] | 3 | 3 | 3 | Active | 2020 | [98][99] | ||||
| RFA One | Rocket Factory Augsburg | 1,300 | 450 | -- | -- | 0 | Devel. | 2024 | 1st stage combustion in Europe, Orbital Stage. | [citation needed][100][101][102][103] | ||||||
| Rokot/Strela (UR-100N) | EurockotKhrunichev | 2,100 | -- | -- | -- | 37[bc] | 36 | 35 | 35 | Active | 1994 | 34 Rokot launches (no launches post-2019 due to Ukrainian tech ban); 3 Strela launches. | [104][105][106][107] | |||
| RS1 | ABL Space Systems | 1,200 | -- | -- | 12 | 1[bd] | 0 | 0 | 0 | Active | 2023 | [108] | ||||
| Shavit | IAI | 225 | -- | -- | 15 | 13[be] | 11 | 11 | 11 | Active | 1988 | Var.: Shavit, -1, -2 | [109] | |||
| Simorgh | ISA | 350 | -- | -- | -- | 7[bf] | 7 | 2 | 2 | Active | 2016 | [110] | ||||
| SK solid fueled TV2 | MND | > 100 | -- | -- | -- | 1[bg] | 1 | 1 | 1 | Active | 2023 | solid fueled launch vehicle | [111] | |||
| SLS | Orbital ATKBoeingUnited Launch AllianceAerojet Rocketdyne | 95,000–130,000 | -- | 27,000–46,000 | -- | 1[bh] | 1 | 1 | 1 | Active | 2022 | Var.: Block 1, Block 1B, Block 2 | [112][113] | |||
| Soyuz | RSC EnergiaTsSKB-Progress | 8,200 | 2,400 | 1,200 | -- | 2,006[bi] | [bj] | 1,881[bk] | Active | 1957 | Var.: Sputnik, Luna, Vostok-L, Vostok-K, Voskhod, Molniya, Molniya-L, Molniya-M, Polyot, Soyuz, Soyuz-L, Soyuz-M, Soyuz-U, Soyuz-FG,Soyuz-2, Soyuz-2-1v | [114][115] | ||||
| Spectrum | Isar Aerospace | 1,000 (LEO)[116] 700 (SSO) | -- | -- | -- | 1[bl] | 0 | 0 | 0 | Active | 2025 | [116] | ||||
| SS-520 | IHI Aerospace | 4 | -- | -- | -- | 2[bm] | 2 | 1 | 1 | Active | 2017 | 2 successful suborbital flights and 2 orbital flights (one success). A test of how small orbital rockets can be. The rocket has a mass of only 2.6 tonnes. | [117] | |||
| SSLV | ISRO | 500 | 300 | -- | -- | 3[bn] | 3 | 2 | 2 | Active | 2022 | |||||
| Starship | SpaceX | 250,000 (expendable)[better source needed] | 40,000[better source needed] | 100,000+ (With in-orbit refueling) [better source needed] | -- | 11[bo][bp] | 10 | 0 | 0 | test flights | 2023 | 1st flight intended aTAO orbit; 3rd flight suborbital | [118][119][120][121][122] | |||
| 150,000 (reusable)[better source needed] | ||||||||||||||||
| Start-1 (RT-2PM) | MITT | 532 | -- | -- | -- | 7[bq] | 6 | 6 | 6 | Active | 1993 | [123] | ||||
| Taurus / Minotaur-C | Orbital Sciences | 1,450 | -- | -- | -- | 9[br] | 9 | 6 | 6 | Active | 1989 | Var.: 2110, 3110, 3210 | [124] | |||
| Tianlong 2 | Space Pioneer | 2,000(LEO) 1,500(500 km SSO) | -- | -- | 1[bs] | 1 | 1 | 1 | Active | 2023 | liquid fueled (kerolox) carrier | [125][126] | ||||
| Tianlong 3 | Space Pioneer | 17,000(LEO) 14,000(500 km SSO) | -- | -- | 0 | Devel. | 2024 | kerolox with reusable 1st stage | [126][127] | |||||||
| Tronador | CONAE | 500 | Devel. | 2030 | ||||||||||||
| Unha | KCST | 200 | -- | -- | -- | 4[bt] | 3 | 2 | Active | 2006 | Var.:Paektusan based onTaepodong-1 missile; Unha based onTaepodong-2 missile. | [128][129] | ||||
| Vega | Avio | 2,300 | -- | -- | 23 | 27[bu] | 26 | 24 | 24 | Active | 2012 | Vega, Vega-C, Vega-E in-development. | [130] | |||
| Vikram | Skyroot Aerospace | 720 | -- | -- | 0 | Devel. | NET 2023 | Var.: Vikram 1, Vikram II, Vikram III | [131] | |||||||
| VLM | CTA | 150 | -- | -- | -- | 0 | Devel. | NET 2025 | [132][133][134] | |||||||
| Vulcan | ULA | 17,800–34,900 | 7,400–16,300 | -- | 99 | 3[bv] | 3 | 3 | 3 | Active | 2024 | [135][non-primary source needed][136][137][138] | ||||
| Yenisei | TsSKB-Progress RSC Energia | 88,000–115,000 | 20,000-27,000 | 0 | Devel. | NET 2032 | [139][140][141][142] | |||||||||
| Zenit | Yuzhnoye | 13,740 | 6,160 | 4,098 | -- | 84[bw] | 74 | 72 | Active | 1985 | Var.: 2, 2M (2SB, 2SLB), 3SL, 3SLB, 3SLBF | [143] | ||||
| Zephyr | Latitude | 100 | -- | -- | 0 | Devel. | 2025 | [144] | ||||||||
| Zero | Interstellar Technologies | 100(SSO) | -- | -- | 0 | Devel. | 2023 | [145] | ||||||||
| Zhuque-2 | LandSpace | 4,000(LEO) 1,500(500 km SSO)[146] | -- | -- | 6[bx] | 6 | 4 | 4 | Active | 2022 | Var.: ZQ-2 | 1st methalox LV to reach: space (2022), orbit (2023), orbit with payload (12/2023) | [38][146][147] | |||
| 6,000(LEO) 4,000(500 km SSO)[147] | -- | -- | Var.: ZQ-2E | |||||||||||||
| Zhuque-3 | LandSpace | 21,000(expendable) | -- | -- | 0 | Devel. | 2025 | methalox LV with reusable 1st stage; stainless steel body | [148] | |||||||
| 12,500–18,300(1st stage recovered) | ||||||||||||||||
| Zuljanah | ISA | 220[149] | 0 | Devel. | NET 2023 | Two successful suborbital flights | [150][149] | |||||||||
| Family | Country/Orgs. | Manufac. | Payload (kg) | Cost (US$, millions) | Launches reaching... | Status | Date of flight | Notes | Refs | ||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| LEO | GTO | TLI | Total | Space | Any orbit | Target orbit | First | Last | |||||||
| Ariane 1-2-3 | Aérospatiale | — | 2,650 | — | -- | 28 | Retired | 1979 | 1989 | [151][152] | |||||
| Ariane 4 | Aérospatiale | 7,000 | 4,720 | — | -- | 116 | Retired | 1988 | 2003 | Var.: 40, 42P, 42L, 44P, 44L, 44LP | [152] | ||||
| Ariane 5 | Airbus | 21,000 | 10,735[153] | — | 165–220 | 117 | 115 | 115 | 112 | Retired | 1996 | 2023 | Var.: G, G+, GS, ECA, ES. | [154][155][156] | |
| ASLV | ISRO | 150 | -- | -- | -- | 4 | 2 | 2 | 1 | Retired | 1987 | 1994 | [157] | ||
| Athena I & II | LockheedATK | 2,065 | -- | 295 | -- | 7 | Retired | 1995 | 2001 | Launch Lunar Prospector.[158] | [159] | ||||
| Atlas I (Atlas A-B-C-D-E-F-G) | Lockheed | 5,900 | 2,340 | -- | -- | 514 | Retired | 1957 | 1997 | LaunchMercury. Atlas or Centaur upper stage. | [160][161][162][163] | ||||
| Atlas II | Lockheed | 8,618 | 3,833 | -- | -- | 63 | 63 | 63 | Retired | 1991 | 2004 | [164][165][166] | |||
| Atlas III | Lockheed | 10,759 | 4,609 | -- | -- | 6 | 6 | 6 | Retired | 2003 | 2005 | Var.: IIIA, IIIB | [167][168] | ||
| Black Arrow | RAEWestland | 132 | -- | -- | -- | 4 | 3 | Retired | 1969 | 1971 | [169] | ||||
| Delta | Douglas | 3,848 | 1,312 | -- | -- | 186 | Retired | 1960 | 1989 | Launched Pioneer & Explorer probes. Var. A, B, C, D, E, G, J, L, M, N, 300, 900, 1X00, 4X00, 2X00, 3X00, 5X00 | [170] | ||||
| Delta II | ULA | 6,000 | 2,171 | 1,508 | 51 | 153 | 152 | 152 | 151 | Retired | 1989 | 2018 | Launched Mars probesMGS toPhoenix Var.: 6000, 7000, and Heavy. | [170][171][172] | |
| Delta III | Boeing | 8,290 | 3,810 | -- | -- | 3 | 2 | 2 | Retired | 1998 | 2000 | [173][174] | |||
| Delta IV | ULA | 23,040 | 13,130 | 9,000 | -- | 45 | 45 | 45 | 44 | Retired | 2002 | 2024 | Var.: M, M+, and Heavy. | [175] | |
| Diamant | SEREB | 160 | -- | -- | -- | 12 | 9 | Retired | 1965 | 1975 | [citation needed] | ||||
| Dnepr (R-36M) | Yuzhmash | 3,600 | -- | 750 | 14 | 17 | Retired | 1999 | 2015 | [176][177][178] | |||||
| Energia | NPO Energia | 100,000 | 20,000 | 32,000 | 240 (Energia−Buran) | 2 | 2 | 1 | 1 | Retired | 1987 | 1988 | 1 partial failure withPolyus spacecraft, 1 successful flight withBuran shuttle. | [179][citation needed] | |
| Falcon 1 | SpaceX | 420[180] | -- | -- | 7.9[180] | 5[181] | 4[180] | 2[180] | 2[181] | Retired[180] | 2006 | 2009 | |||
| Feng Bao 1 (DF-5) | SAST | 2,500 | -- | -- | -- | 8 | 4 | Retired | 1972 | 1981 | 3 successful suborbital flights | [182] | |||
| GSLV Mark I | ISRO | 5,000 | 2,500 | -- | -- | 6 | 4 | 2 | 2 | Retired | 2001 | 2010 | [29][30][31] | ||
| H-I | Mitsubishi | 3,200 | -- | -- | 9 | 9 | Retired | 1986 | 1992 | License-built version of the Thor-ELT | [183] | ||||
| H-II,IIA &IIB | Mitsubishi | 19,000 | 8,000 | -- | (190), 90, 112 | 66[by] | 65 | 64 | 63 | Retired | 1994 | 2025 | Var.: A202, A2022, A2024, A204, B | [184] | |
| J-I | IHI CorporationNissan Motors | 880 | -- | -- | -- | 1 | Retired | 1996 | 1996 | Partial demonstration flight only | [citation needed] | ||||
| Kosmos (R-12 &R-14) | YuzhnoyePolyot | 1,500 | -- | -- | 12 | 610 | 559 | Retired | 1967 | 2010 | Var.: 1, 2, 3, 3M | [155][185][186] | |||
| Kaituozhe (DF-31) | CALT | 800 | -- | -- | -- | 3 | 1 | 1 | 1 | Retired(likely) | 2002 | 2017 | Var.: KT-1, KT-2, KT2-A | [187] | |
| Lambda 4S | NissanISAS | 26 | -- | -- | -- | 5 | 1 | Retired | 1966 | 1970 | [citation needed] | ||||
| Long March 1 | CALT | 300 | -- | -- | -- | 2 | 2 | 2 | 2 | Retired | 1970 | 1971 | [188][189][190] | ||
| Long March 1D | CALT | 740 | -- | -- | -- | 0 | Retired | 1995 | 2002 | 3 suborbital launches only (2 successful.) | [188][189][190] | ||||
| Mu 1-3-4 | Nissan Motor IHI | 770 | -- | -- | -- | 27 | Retired | 1966 | 1995 | Var.: 1, 3D, 4S, 3C, 3H, 3S, 3SII | [191] | ||||
| Mu 5 | Nissan Motor IHI | 1,800 | -- | -- | -- | 7 | 6 | Retired | 1997 | 2006 | Var.: M-V, M-V KM | [citation needed] | |||
| N1 | NPO Energia | 90,000 | -- | 23,500 | -- | 4 | 0 | 0 | 0 | Retired | 1969 | 1972 | Designed for Soviet Manned Lunar Mission | [192] | |
| N-I &II | Mitsubishi | 2,000 | 730 | -- | -- | 15 | 15 | 15 | 14[bz] | Retired | 1975 | 1987 | Derived from the American Delta rocket | [193] | |
| Naro | KhrunichevKARI | 100 | -- | -- | -- | 3 | 2 | 1 | 1 | Retired | 2009 | 2013 | First stage uses the Russian RD-151 engine | [194] | |
| Safir | ISA | 50 | -- | -- | -- | 8[ca] | 5 | 4 | 4 | Retired | 2007 | 2019 | Numbers given here may be in dispute | [195] | |
| Saturn I &IB | ChryslerDouglas | 18,600 | -- | -- | 19 | 13 | 13 | 13 | 13 | Retired | 1961 | 1975 | Saturn 1 family also included 6 suborbital test launches | [196][197] | |
| Saturn V | BoeingNorth AmericanDouglas | 118,000 | -- | 47,000 | 185 | 13 | 13 | 13 | Retired | 1967 | 1973 | Var.: Apollo, Skylab | [196][198][199] | ||
| Scout | US Air ForceNASA | 210 | -- | -- | -- | 125 | 104 | Retired | 1960 | 1994 | Var.: X1, X2, A, D, G | [200] | |||
| Shtil'/Volna-O (R-29) | Makeyev | 430 | -- | -- | -- | 8[cb] | 7 | 2 | 2 | Retired(as commercial launchers)[201] | 1995 | 2006 | Var.: Volna, Shtil, 2.1, 2R, 3 | [201] | |
| SLV | ISRO | 40 | -- | -- | -- | 4 | 3 | 3 | 2 | Retired | 1979 | 1983 | LaunchedRohini satellite series | [202] | |
| STS (Space Shuttle) | AlliantMartin MariettaRockwell | 24,400 | 3,810 | -- | 450 | 135 | 134 | 134 | 133 | Retired | 1981 | 2011 | Orbiter mass: 68585 kg. | [203] | |
| Terran 1 | Relativity Space | 1,250 | -- | -- | 1 | 1 | 0 | 0 | Retired | 2023 | 2023 | anticipates 3-D printing most rocket parts | [204] | ||
| Thor | Douglas | 1,270 | -- | 38 | -- | 357 | Retired | 1957 | 1980 | Launched Pioneer & Explorer probes | [170] | ||||
| Titan II-(II GLV)-III-IV (LGM-25C) | Martin Marietta | 21,900 | 5,773 | 8,600 | 350 | 369 | Retired | 1959 | 2005 | Var.: I, II, IIIA, IIIB, IIIC, IIID, IIIE, 34D, IVA, IVB Gemini launcher | [205][206] | ||||
| Tsyklon (R-36) | Yuzhmash | 4,100 | -- | -- | -- | 259 | Retired | 1967 | 2009 | Var.: 1, 2, 3. | [207] | ||||
| Vanguard | Martin | 23 | -- | -- | -- | 12 | 3 | Retired | 1957 | 1959 | [208] | ||||
| Zhuque-1 | LandSpace | 300 | -- | -- | 1 | 1 | 0 | 0 | Retired | 2018 | 2018 | [209][210] | |||

The more capable Long March 5 rocket is expected to help the country achieve its goal of constructing a space station in orbit by the year 2020, as well as play a key role in China's future space exploration aims beyond low-Earth orbit. The rocket's maiden launch is expected to occur in 2014
Russian officials have said they plan to discontinue Dnepr launches.