Loading AI tools
From Wikipedia, the free encyclopedia
This article compares different orbital 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 of currently active and under-development launcher families, while the second contains a list of retired launcher families.
The related article "Comparison of orbital launch systems" lists each individual launcher system within any given launcher family, categorized by its current operational status.
Same cores are grouped together (like Ariane 1, 2 & 3, but not V).
Family | Country | 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 | IND | AgniKul Cosmos | 100 | -- | -- | -- | Devel. | NET 2023 | Expected launch in 2022 | |||||||
Alpha | USA | Firefly Aerospace | 1,000 | — | — | -- | 5[lower-alpha 1] | 4 | 4 | 2 | Active | 2021 | [1] | |||
Angara | RUS | Khrunichev | 3,800–35,000 | 3,600–12,500 | -- | -- | 7[lower-alpha 2] | 7 | 7 | 6 | Active | 2014 | [2][3] | |||
Antares | USA | Orbital ATK | 8,000 | -- | -- | 80[citation needed] | 18[lower-alpha 3] | 17 | 17 | 17 | Active[lower-alpha 4] | 2013 | Cygnus launcher. Var.: 110, 120, 130, 230, 230+, 330 |
[4][5][6] | ||
Ariane 6 | EU | ArianeGroup | 21,650 (A64 var.) |
11,500+ (A64 var.) |
8,500 (A64 var.) |
115 | 1[lower-alpha 5] | 1 | 1 | 1 | Active | 2024 | Var.: Ariane 62, Ariane 64. | [7] | ||
Astra Rocket | USA | Astra | 50–150 (to SSO) |
— | — | -- | 7[lower-alpha 6] | 4 | 2 | 2 | Active | 2020 | 2 suborbital test launches in 2018. | [8] | ||
Atlas V | USA | ULA | 18,850 | 8,900 | 2,807 | 109–153 | 101[lower-alpha 7] | 101 | 101 | 101 | Active[lower-alpha 8] | 2002 | 2029 (planned) |
Launched Juno & New Horizons | [9][10] | |
Blue Whale 1 | ROK | Perigee Aerospace | 170 (to SSO) | -- | -- | -- | 0 | Devel. | NET 2024 | [11] | ||||||
Ceres-1 | CHN | Galactic Energy | 400 (LEO) 300 (SSO) |
-- | -- | -- | 15[lower-alpha 9] | 14 | 14 | 14 | Active | 2020 | Var.: Ceres-1, Ceres-1S | [12][13] | ||
Chollima-1 | DPRK | NADA | ~300 | -- | -- | -- | 4[lower-alpha 10] | 2 | 1 | 1 | Active | 2023 | UDMH/N2O4 fueled carrier | [14] | ||
Cyclone-4M | UKR | Yuzhnoye Yuzhmash |
5,000 | 1,000 | -- | -- | 0 | Devel. | unknown | [15] | ||||||
Darwin-1 | CHN | Rocket Pi | 300 | -- | -- | -- | 0 | Devel. | NET 2024 | methalox launcher | [16] | |||||
Electron | NZ USA |
Rocket Lab | 225 | 6 | 53[lower-alpha 11] | 53 | 49 | 49 | Active | 2017 | [17] | |||||
Epsilon | JPN | IHI Corporation | 1,200 | -- | -- | -- | 6[lower-alpha 12] | 6 | 5 | 5 | Active | 2013 | [18][19] | |||
Eris | AUS | Gilmour Space Technologies | 305 | -- | -- | -- | 0 | Devel. | NET 2023 | [20] | ||||||
Falcon | Falcon 9 | USA | SpaceX | 22,800 | 8,300 | -- | 61.2 | 390[lower-alpha 13][lower-alpha 14] | 388 | 388 | 387 | Active | 2010 | Var.: v1.0, v1.1,[lower-alpha 15] FT,[lower-alpha 16] Block 4, Block 5. Launcher of crewed Dragon capsule. | ||
Falcon Heavy | USA | SpaceX | 63,800 | 26,700 | -- | 90–150 | 11[lower-alpha 17] | 11 | 11 | 11 | Active | 2018 | First test launch 2018-02-06 | [23][24][25] | ||
Gravity-1 | CHN | Orienspace | 6,500 (LEO) 3,700 (700 km SSO) |
-- | -- | -- | 1[lower-alpha 18] | 1 | 1 | 1 | Active | 2024 | largest solid launcher (3rd stage can be solid/kerolox) | [16][26] | ||
Gravity-2 | CHN | Orienspace | 25,600 (LEO) 19,100 (SSO) |
7,700 | -- | -- | 0 | Devel. | 2025 | kerolox (core), solid (boosters); reusable 1st stage | [26] | |||||
GSLV Mark II | IND | ISRO | 5,000 | 2,700 | -- | -- | 10[lower-alpha 19] | 9 | 8 | 8 | Active | 2010 | [27][28][29] | |||
H-II, IIA & IIB | JPN | Mitsubishi | 19,000 | 8,000 | -- | (190), 90, 112 | 65[lower-alpha 20] | 64 | 63 | 62 | Active | 1994 | Var.: A202, A2022, A2024, A204, B | [30] | ||
H3 | JPN | Mitsubishi | 4,000–28,300 (base-heavy) | 7,900–14,800 (base-heavy) | 11,900 (heavy) | 4[lower-alpha 21] | 4 | 3 | 3 | Active | 2023 | Var.: 30S, 22S, 32L, 24L, heavy[31][32] | [32] | |||
Hyperbola-1 | CHN | i-Space | 300 | -- | -- | 7[lower-alpha 22] | 5 | 3 | 3 | Active | 2019 | [33] | ||||
Hyperbola-3 | CHN | i-Space | 8,500–13,400 | -- | -- | 0 | Devel. | 2025 | VTVL | [34] | ||||||
Jielong 1 | CHN | CALT | 200 (SSO) | -- | -- | 1[lower-alpha 23] | 1 | 1 | 1 | Active | 2019 | [35] | ||||
Jielong 3 | CHN | CALT | 1,500 (500 km SSO) | -- | -- | -- | 4[lower-alpha 24] | 4 | 4 | 4 | Active | 2022 | [36][37] | |||
KAIROS | JPN | Space One | 250 150 (SSO) |
-- | -- | 1[lower-alpha 25] | 0 | 0 | 0 | Active | 2024 | [38] | ||||
Kuaizhou (DF-21) |
CHN | CASIC | 400 (KZ-1A) | -- | -- | -- | 32[lower-alpha 26][lower-alpha 27] | 31[lower-alpha 28] | 29 | 29 | Active | 2013 | Var.: KZ-1, KZ-1A, KZ-11; (KZ-21 under development) | [39][40] | ||
1,500 (KZ-11) | -- | -- | ||||||||||||||
LauncherOne | USA | Virgin Orbit | 300 (SSO) | -- | -- | -- | 6[lower-alpha 29] | 5 | 4 | 4 | Susp.[lower-alpha 30] | 2020 | [41] | |||
Lijian-1 (Kinetica-1) |
CHN | CAS Space | 1,500 (500 km SSO) |
-- | -- | -- | 4[lower-alpha 31] | 4 | 4 | 4 | Active | 2022 | solid fueled carrier | [36][16] | ||
Lijian-2 (Kinetica-2) |
CHN | CAS Space | 12,000 (LEO) 7800 (SSO) |
-- | -- | -- | 0 | Devel. | 2025 | kerolox LV. reusable 1st stage | [42][43] | |||||
Long March 2–3–4 (DF-5) |
CHN | CALT+SAST | 12,000 | 5,500 | 3,300 | 471[lower-alpha 32][lower-alpha 33] | 465[lower-alpha 34] | 462 | 454 | Active | 1971 | See notes | Var.: 2A, 2C, 2D, 2E, 2F,[lower-alpha 35] 3, 3A, 3B, 3B/E, 3C, 4A, 4B, 4C. See [lower-alpha 36] for retired var. among those listed here. | [45] | ||
Long March 5 | CHN | CALT | -- | 14,000 (CZ-5) |
8,000 (CZ-5) |
-- | 12[lower-alpha 37] | 12 | 11 | 11 | Active | 2016 | Var.: CZ-5 | [46][47] | ||
25,000 (CZ-5B) |
-- | -- | Var.: CZ-5B | |||||||||||||
CZ 6–7–8 family | Long March 6 | CHN | SAST | 1,500 (LEO) 1,080 (700 lm SSO) |
-- | -- | -- | 22[lower-alpha 38] | 22 | 22 | 22 | Active | 2015 | Var.: 6 | [48][49] | |
4,500 (700 km SSO) | -- | -- | Var.: 6A | |||||||||||||
2,400 (500 km SSO) | -- | -- | Var.: 6C | |||||||||||||
Long March 7 | CHN | CALT | 14,000 | -- | -- | -- | 16[lower-alpha 39] | 15 | 15 | 15 | Active | 2016 | Var.: 7 | [50][51][52] | ||
-- | 7,000 | -- | Var.: 7A | |||||||||||||
Long March 8 | CHN | CALT | 4,500 (SSO) | 2,800 | > 1,200 | -- | 3[lower-alpha 40] | 3 | 3 | 3 | Active | 2020 | Var.: 8, 8A | [51][53][54] | ||
Long March 9 | CHN | CALT | 150,000 | -- | 50,000 | -- | 0 | Devel. | 2033 | partly-reusable Super-Heavy carrier | [53][55] | |||||
Long March 10 | CHN | CALT | 70,000 (CZ-10)[56] | -- | 27,000 (CZ-10)[55] |
-- | 0 | Devel. | 2026 | Human-rated Var.: 10 (3-core, TLI) |
[57][58][56][55][59] | |||||
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 | CHN | CALT | 1,000 | -- | -- | -- | 17[lower-alpha 41] | 17 | 17 | 17 | Active | 2015 | Likely based on DF-31 missile | [60] | ||
Long March 12 | CHN | SAST | 12,000 (LEO); 6,000 (700 km SSO) |
-- | -- | -- | 0 | Devel. | 2024 | kerolox LV 3.8 metres diameter |
[61][62][63] | |||||
LVM 3 | IND | ISRO | 10,000 | 4,000 | 2,180 | -- | 6[lower-alpha 42] [lower-alpha 43] | 6 | 6 | 6 | Active | 2014 | [64][65] | |||
Maia | FRA | MaiaSpace | 500 (SSO) | -- | -- | 0 | Devel. | 2025 | Planned first stage reuse | [66] | ||||||
Minotaur I | USA | Orbital ATK | 580 | -- | -- | -- | 12[lower-alpha 44] | 12 | 12 | 12 | Active | 2000 | Derived from the Minuteman II | [67][68] | ||
Minotaur IV & V | USA | Orbital ATK | 1,735 | 640 | 447 | 50 | 8[lower-alpha 45] | 8 | 8 | 8 | Active | 2010 | Also 2 suborbital launches (HTV-2a). Var.: IV, IV Lite, IV HAPS, V. Derived from Peacekeeper missile | [67][69] | ||
Miura 5 | ESP | PLD Space | 900 | -- | -- | 0 | Devel. | NET 2024 | [70] | |||||||
MLV | USA | Firefly Aerospace | 14,000 | -- | -- | -- | 0 | Devel. | 2025 | [71] | ||||||
Nebula-1 | CHN | Deep Blue Aerospace | 1,000 | -- | -- | 0 | Devel. | 2024 | VTVL (first stage) | [72] | ||||||
Nebula-2 | CHN | Deep Blue Aerospace | 20,000 | -- | -- | 0 | Devel. | 2025 | kerolox; VTVL (first stage) | [73] | ||||||
Neutron | NZ USA |
Rocket Lab | 15,000 | -- | 2,000 | 50 | 0 | Devel. | 2024 | [74] | ||||||
New Glenn | USA | Blue Origin | 45,000 | 13,000 | -- | 0 | Devel. | NET 2024 | [75] | |||||||
New Line 1 | CHN | LinkSpace | 200 (SSO) | -- | -- | 0 | Devel. | unknown | [76] | |||||||
NGLV | IND | ISRO | 20,000 | 10,000 | -- | -- | 0 | Devel. | unknown | [77] | ||||||
Nuri | ROK | KARI | 1,500 | -- | -- | 3[lower-alpha 46] | 3 | 2 | 2 | Active | 2021 | [78][79] | ||||
OS-M | CHN | OneSpace | 205 (M1) | -- | -- | -- | 1[lower-alpha 47] | 0 | 0 | 0 | Active | 2019 | Var.: M1, M2, M4. Single M1 failed launch; M2 & M4 in development. | [80] | ||
Pallas-1 | CHN | Galactic Energy | 5,000 3,000 (SSO) |
-- | -- | -- | 0 | Devel. | Nov. 2024 | kerolox LV with reusable 1st stage | [81][43] | |||||
Pegasus | USA | Orbital ATK | 450 | -- | -- | -- | 45[lower-alpha 48] | 44 | 42 | 40 | Active | 1990 | [82] | |||
Pioneer-1 (aka Yuanxingzhe-1 or XZY-1) |
CHN | Arrowhead Technology/Space Epoch | 6,500 (1,100 km LEO) | -- | -- | 0 | Devel. | 2025 | first stage recovery via ocean landing | [83][84] | ||||||
Prime | UK | Orbex | 150 (SSO) | -- | -- | -- | 0 | Devel. | NET 2023 | [85][86] | ||||||
Proton (UR-500) |
USSR RUS |
Khrunichev | 23,000 | 6,920 | 5,680 | 65 (Proton-M) | 430[lower-alpha 49] | 382 | Active | 1965 | Var.: K, M, Medium in development. | [87][88][89] | ||||
PSLV | IND | ISRO | 3,800 | 1,200 | 550 | -- | 60[lower-alpha 50] | 59 | 58 | 57 | Active | 1993 | Var.: CA, XL, QL, DL Launched moon probe Chandrayaan I, Mars probe Mangalyaan I |
[90][91] | ||
Qaem-100 | IRN | IRGC | 80 | -- | -- | -- | 3[lower-alpha 51] | 3 | 2 | 2 | Active | 2023 | also one successful suborbital launch | [92] | ||
Qased | IRN | IRGC | ~50 | -- | -- | -- | 3[lower-alpha 52] | 3 | 3 | 3 | Active | 2020 | [93][94] | |||
RFA One | Germany | Rocket Factory Augsburg | 1,300 | 450 | -- | -- | 0 | Devel. | 2024 | 1st stage combustion in Europe, Orbital Stage. | [citation needed][95][96][97][98] | |||||
Rokot/Strela (UR-100N) |
RUS | Eurockot Khrunichev | 2,100 | -- | -- | -- | 37[lower-alpha 53] | 36 | 35 | 35 | Active | 1994 | 34 Rokot launches (no launches post-2019 due to Ukrainian tech ban); 3 Strela launches. | [99][100][101][102] | ||
RS1 | USA | ABL Space Systems | 1,200 | -- | -- | 12 | 1[lower-alpha 54] | 0 | 0 | 0 | Active | 2023 | [103] | |||
Shavit | ISR | IAI | 225 | -- | -- | 15 | 12[lower-alpha 55] | 10 | 10 | 10 | Active | 1988 | Var.: Shavit, -1, -2 | [104] | ||
Simorgh | IRN | ISA | 350 | -- | -- | -- | 6[lower-alpha 56] | 6 | 1 | 1 | Active | 2016 | [105] | |||
SK solid fueled TV2 | ROK | MND | > 100 | -- | -- | -- | 1[lower-alpha 57] | 1 | 1 | 1 | Active | 2023 | solid fueled launch vehicle | [106] | ||
SLS | USA | Orbital ATK Boeing United Launch Alliance Aerojet Rocketdyne | 95,000–130,000 | -- | 27,000–46,000 | -- | 1[lower-alpha 58] | 1 | 1 | 1 | Active | 2022 | Var.: Block 1, Block 1B, Block 2 | [107][108] | ||
Soyuz |
USSR RUS |
RSC Energia TsSKB-Progress | 8,200 | 2,400 | 1,200 | -- | 1,992[lower-alpha 59] | [lower-alpha 60] | 1,867[lower-alpha 61] | 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 | [109][110] | |||
SS-520 | JPN | IHI Aerospace | 4 | -- | -- | -- | 2[lower-alpha 62] | 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. | [111] | ||
SSLV | IND | ISRO | 500 | 300 | -- | -- | 3[lower-alpha 63] | 3 | 2 | 2 | Active | 2022 | ||||
Starship | USA | SpaceX | 250,000 (expendable) [better source needed] | 40,000 [better source needed] | 100,000+ (With in-orbit refueling) [better source needed] | -- | 5[lower-alpha 64][lower-alpha 65] | 4 | 0 | 0 | test flights | 2023 | 1st flight intended a TAO orbit; 3rd flight suborbital | [112][113][114][115][116] | ||
150,000 (reusable) [better source needed] | ||||||||||||||||
Start-1 (RT-2PM) |
RUS | MITT | 532 | -- | -- | -- | 7[lower-alpha 66] | 6 | 6 | 6 | Active | 1993 | [117] | |||
Taurus / Minotaur-C | USA | Orbital Sciences | 1,450 | -- | -- | -- | 9[lower-alpha 67] | 9 | 6 | 6 | Active | 1989 | Var.: 2110, 3110, 3210 | [118] | ||
Tianlong 2 | CHN | Space Pioneer | 2,000 (LEO) 1,500 (500 km SSO) |
-- | -- | 1[lower-alpha 68] | 1 | 1 | 1 | Active | 2023 | liquid fueled (kerolox) carrier | [119][120] | |||
Tianlong 3 | CHN | Space Pioneer | 17,000 (LEO) 14,000 (500 km SSO) |
-- | -- | 0 | Devel. | 2024 | kerolox with reusable 1st stage | [120][121] | ||||||
Tronador | ARG | CONAE | 500 | Devel. | 2030 | |||||||||||
Unha | DPRK | KCST | 200 | -- | -- | -- | 4[lower-alpha 69] | 3 | 2 | Active | 2006 | Var.: Paektusan based on Taepodong-1 missile; Unha based on Taepodong-2 missile. | [122][123] | |||
Vega | EU | Avio | 2,300 | -- | -- | 23 | 24[lower-alpha 70] | 23 | 21 | 21 | Active | 2012 | Vega, Vega-C, Vega-E in-development. |
[124] | ||
Vikram | IND | Skyroot Aerospace | 720 | -- | -- | 0 | Devel. | NET 2023 | Var.: Vikram 1, Vikram II, Vikram III | [125] | ||||||
VLM | BRA | CTA | 150 | -- | -- | -- | 0 | Devel. | NET 2025 | [126][127][128] | ||||||
Vulcan | USA | ULA | 17,800–34,900 | 7,400–16,300 | -- | 99 | 2[lower-alpha 71] | 2 | 2 | 2 | Active | 2024 | [129][non-primary source needed][130][131][132] | |||
Yenisei | RUS | TsSKB-Progress RSC Energia |
88,000–115,000 | 20,000-27,000 | 0 | Devel. | NET 2032 | [133][134][135][136] | ||||||||
Zenit | USSR UKR RUS |
Yuzhnoye | 13,740 | 6,160 | 4,098 | -- | 84[lower-alpha 72] | 74 | 72 | Active | 1985 | Var.: 2, 2M (2SB, 2SLB), 3SL, 3SLB, 3SLBF | [137] | |||
Zephyr | FRA | Latitude | 100 | -- | -- | 0 | Devel. | 2025 | [138] | |||||||
Zero | JPN | Interstellar Technologies | 100 (SSO) | -- | -- | 0 | Devel. | 2023 | [139] | |||||||
Zhuque-2 | CHN | LandSpace | 6,000 (LEO) 4000 (500 km SSO)[140] |
-- | -- | 3[lower-alpha 73] | 3 | 2 | 2 | Active | 2022 | 1st methalox LV to reach: space (2022), orbit (2023), orbit with payload (12/2023) |
[36][140] | |||
Zhuque-3 | CHN | LandSpace | 21,000 (expendable) | -- | -- | 0 | Devel. | 2025 | methalox LV with reusable 1st stage; stainless steel body | [141] | ||||||
12,500–18,300 (1st stage recovered) | ||||||||||||||||
Zuljanah | IRN | ISA | 220[142] | 0 | Devel. | NET 2023 | Two successful suborbital flights | [143][142] |
Family | Country | 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 | EU | Aérospatiale | — | 2,650 | — | -- | 28 | Retired | 1979 | 1989 | [144][145] | ||||
Ariane 4 | EU | Aérospatiale | 7,000 | 4,720 | — | -- | 116 | Retired | 1988 | 2003 | Var.: 40, 42P, 42L, 44P, 44L, 44LP | [145] | |||
Ariane 5 | EU | Airbus | 21,000 | 10,735[146] | — | 165–220 | 117 | 115 | 115 | 112 | Retired | 1996 | 2023 | Var.: G, G+, GS, ECA, ES. | [147][148][149] |
ASLV | IND | ISRO | 150 | -- | -- | -- | 4 | Retired | 1987 | 1994 | [150] | ||||
Athena I & II | USA | Lockheed ATK | 2,065 | -- | 295 | -- | 7 | Retired | 1995 | 2001 | Launch Lunar Prospector.[151] | [152] | |||
Atlas I (Atlas A-B-C-D-E-F-G) |
USA | Lockheed | 5,900 | 2,340 | -- | -- | 514 | Retired | 1957 | 1997 | Launch Mercury. Atlas or Centaur upper stage. |
[153][154][155][156] | |||
Atlas II | USA | Lockheed | 8,618 | 3,833 | -- | -- | 63 | 63 | 63 | Retired | 1991 | 2004 | [157][158][159] | ||
Atlas III | USA | Lockheed | 10,759 | 4,609 | -- | -- | 6 | 6 | 6 | Retired | 2003 | 2005 | Var.: IIIA, IIIB | [160][161] | |
Black Arrow | UK | RAE Westland | 132 | -- | -- | -- | 4 | 3 | Retired | 1969 | 1971 | [162] | |||
Delta | USA | 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 |
[163] | |||
Delta II | USA | ULA | 6,000 | 2,171 | 1,508 | 51 | 153 | 152 | 152 | 151 | Retired | 1989 | 2018 | Launched Mars probes MGS to Phoenix Var.: 6000, 7000, and Heavy. |
[163][164][165] |
Delta III | USA | Boeing | 8,290 | 3,810 | -- | -- | 3 | 2 | 2 | Retired | 1998 | 2000 | [166][167] | ||
Delta IV | USA | ULA | 23,040 | 13,130 | 9,000 | -- | 45 | 45 | 45 | 44 | Retired | 2002 | 2024 | Var.: M, M+, and Heavy. | [168] |
Diamant | FRA | SEREB | 160 | -- | -- | -- | 12 | 9 | Retired | 1965 | 1975 | [citation needed] | |||
Dnepr (R-36M) |
UKR RUS |
Yuzhmash | 3,600 | -- | 750 | 14 | 17 | Retired | 1999 | 2015 | [169][170][171] | ||||
Energia | USSR | NPO Energia | 100,000 | 20,000 | 32,000 | 240 (Energia−Buran) | 2 | 2 | 1 | 1 | Retired | 1987 | 1988 | 1 partial failure with Polyus spacecraft, 1 successful flight with Buran shuttle. | [172][citation needed] |
Falcon 1 | USA | SpaceX | 420[173] | -- | -- | 7.9[173] | 5[174] | 4[173] | 2[173] | 2[174] | Retired[173] | 2006 | 2009 | ||
Feng Bao 1 (DF-5) |
CHN | SAST | 2,500 | -- | -- | -- | 8 | 4 | Retired | 1972 | 1981 | 3 successful suborbital flights | [175] | ||
GSLV Mark I | IND | ISRO | 5,000 | 2,500 | -- | -- | 6 | 4 | 2 | 2 | Retired | 2001 | 2010 | [27][28][29] | |
H-I | JPN | Mitsubishi | 3,200 | -- | -- | 9 | 9 | Retired | 1986 | 1992 | License-built version of the Thor-ELT | [176] | |||
J-I | JPN | IHI Corporation Nissan Motors | 880 | -- | -- | -- | 1 | Retired | 1996 | 1996 | Partial demonstration flight only | [citation needed] | |||
Kosmos (R-12 & R-14) |
USSR | Yuzhnoye Polyot | 1,500 | -- | -- | 12 | 610 | 559 | Retired | 1967 | 2010 | Var.: 1, 2, 3, 3M | [148][177][178] | ||
Kaituozhe (DF-31) |
CHN | CALT | 800 | -- | -- | -- | 3 | 1 | 1 | 1 | Retired (likely) | 2002 | 2017 | Var.: KT-1, KT-2, KT2-A | [179] |
Lambda 4S | JPN | Nissan ISAS | 26 | -- | -- | -- | 5 | 1 | Retired | 1966 | 1970 | [citation needed] | |||
Long March 1 | CHN | CALT | 300 | -- | -- | -- | 2 | 2 | 2 | 2 | Retired | 1970 | 1971 | [180][181][182] | |
Long March 1D | CHN | CALT | 740 | -- | -- | -- | 0 | Retired | 1995 | 2002 | 3 suborbital launches only (2 successful.) | [180][181][182] | |||
Mu 1-3-4 | JPN | Nissan Motor IHI | 770 | -- | -- | -- | 27 | Retired | 1966 | 1995 | Var.: 1, 3D, 4S, 3C, 3H, 3S, 3SII | [183] | |||
Mu 5 | JPN | Nissan Motor IHI | 1,800 | -- | -- | -- | 7 | 6 | Retired | 1997 | 2006 | Var.: M-V, M-V KM | [citation needed] | ||
N1 | USSR | NPO Energia | 90,000 | -- | 23,500 | -- | 4 | 0 | 0 | 0 | Retired | 1969 | 1972 | Designed for Soviet Manned Lunar Mission | [184] |
N-I & II | JPN | Mitsubishi | 2,000 | 730 | -- | -- | 15 | 15 | 15 | 14[lower-alpha 74] | Retired | 1975 | 1987 | Derived from the American Delta rocket | [185] |
Naro | ROK | Khrunichev KARI | 100 | -- | -- | -- | 3 | 2 | 1 | 1 | Retired | 2009 | 2013 | First stage uses the Russian RD-151 engine | [186] |
Safir | IRN | ISA | 50 | -- | -- | -- | 8[lower-alpha 75] | 5 | 4 | 4 | Retired | 2007 | 2019 | Numbers given here may be in dispute | [187] |
Saturn I & IB | USA | Chrysler Douglas | 18,600 | -- | -- | 19 | 13 | 13 | 13 | 13 | Retired | 1961 | 1975 | Saturn 1 family also included 6 suborbital test launches | [188][189] |
Saturn V | USA | Boeing North American Douglas | 118,000 | -- | 47,000 | 185 | 13 | 13 | 13 | Retired | 1967 | 1973 | Var.: Apollo, Skylab | [188][190][191] | |
Scout | USA | US Air Force NASA | 210 | -- | -- | -- | 125 | 104 | Retired | 1960 | 1994 | Var.: X1, X2, A, D, G | [192] | ||
Shtil'/Volna-O (R-29) |
RUS | Makeyev | 430 | -- | -- | -- | 8[lower-alpha 76] | 7 | 2 | 2 | Retired (as commercial launchers)[193] | 1995 | 2006 | Var.: Volna, Shtil, 2.1, 2R, 3 | [193] |
SLV | IND | ISRO | 40 | -- | -- | -- | 4 | 3 | 3 | 2 | Retired | 1979 | 1983 | Launched Rohini satellite series | [194] |
STS (Space Shuttle) |
USA | Alliant Martin Marietta Rockwell | 24,400 | 3,810 | -- | 450 | 135 | 134 | 134 | 133 | Retired | 1981 | 2011 | Orbiter mass: 68585 kg. | [195] |
Terran 1 | USA | Relativity Space | 1,250 | -- | -- | 1 | 1 | 0 | 0 | Retired | 2023 | 2023 | anticipates 3-D printing most rocket parts | [196] | |
Thor | USA | Douglas | 1,270 | -- | 38 | -- | 357 | Retired | 1957 | 1980 | Launched Pioneer & Explorer probes | [163] | |||
Titan II-(II GLV)-III-IV (LGM-25C) |
USA | 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 |
[197][198] | |||
Tsyklon (R-36) |
USSR UKR |
Yuzhmash | 4,100 | -- | -- | -- | 259 | Retired | 1967 | 2009 | Var.: 1, 2, 3. | [199] | |||
Vanguard | USA | Martin | 23 | -- | -- | -- | 12 | 3 | Retired | 1957 | 1959 | [200] | |||
Zhuque-1 | CHN | LandSpace | 300 | -- | -- | 1 | 1 | 0 | 0 | Retired | 2018 | 2018 | [201][202] |
Seamless Wikipedia browsing. On steroids.
Every time you click a link to Wikipedia, Wiktionary or Wikiquote in your browser's search results, it will show the modern Wikiwand interface.
Wikiwand extension is a five stars, simple, with minimum permission required to keep your browsing private, safe and transparent.