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.
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 | IND | AgniKul Cosmos | 100 | -- | -- | -- | Devel. | NET 2023 | Expected launch in 2022 | |||||||
Alpha | USA | Firefly Aerospace | 1,000 | — | — | -- | 5 [a] | 4 | 4 | 2 | Active | 2021 | [1] | |||
Angara | RUS | Khrunichev | 3,800–35,000 | 3,600–12,500 | -- | -- | 7 [b] | 7 | 7 | 6 | Active | 2014 | [2] [3] | |||
Antares | USA | 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 | FRA ESA | ArianeGroup | 21,650 (A64 var.) | 11,500+ (A64 var.) | 8,500 (A64 var.) | 115 | 1 [e] | 1 | 1 | 1 | Active | 2024 | Var.: Ariane 62, Ariane 64. | [7] | ||
Astra Rocket | USA | Astra | 50–150 (to SSO) | — | — | -- | 7 [f] | 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 [g] | 101 | 101 | 101 | Active [h] | 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 [i] | 14 | 14 | 14 | Active | 2020 | Var.: Ceres-1, Ceres-1S | [12] [13] | ||
Chollima-1 | DPRK | NADA | ~300 | -- | -- | -- | 4 [j] | 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 | 55 [k] | 55 | 51 | 51 | Active | 2017 | [17] | |||||
Epsilon | JPN | IHI Corporation | 1,200 | -- | -- | -- | 6 [l] | 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 | 410 [m] [n] | 408 | 408 | 407 | Active | 2010 | Var.: v1.0, v1.1, [o] FT, [p] Block 4, Block 5. Launcher of crewed Dragon capsule. | ||
Falcon Heavy | USA | SpaceX | 63,800 | 26,700 | -- | 90–150 | 11 [q] | 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 [r] | 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 [s] | 9 | 8 | 8 | Active | 2010 | [27] [28] [29] | |||
H-II, IIA & IIB | JPN | Mitsubishi | 19,000 | 8,000 | -- | (190), 90, 112 | 65 [t] | 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 [u] | 4 | 3 | 3 | Active | 2023 | Var.: 30S, 22S, 32L, 24L, heavy [31] [32] | [32] | |||
Hyperbola-1 | CHN | i-Space | 300 | -- | -- | 7 [v] | 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 [w] | 1 | 1 | 1 | Active | 2019 | [35] | ||||
Jielong 3 | CHN | CALT | 1,500 (500 km SSO) | -- | -- | -- | 4 [x] | 4 | 4 | 4 | Active | 2022 | [36] [37] | |||
KAIROS | JPN | Space One | 250 150 (SSO) | -- | -- | 1 [y] | 0 | 0 | 0 | Active | 2024 | [38] | ||||
Kuaizhou ( DF-21 ) | CHN | CASIC | 450(KZ-1A Enhanced) | -- | -- | -- | 33 [z] [aa] | 32 [ab] | 30 | 30 | 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 [ac] | 5 | 4 | 4 | Susp. [ad] | 2020 | [41] | |||
Lijian-1 (Kinetica-1) | CHN | CAS Space | 1,500 (500 km SSO) | -- | -- | -- | 5 [ae] | 5 | 5 | 5 | 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 | 476 [af] [ag] | 470 [ah] | 467 | 459 | Active | 1971 | See notes | Var.: 2A, 2C, 2D, 2E, 2F, [ai] 3, 3A, 3B, 3B/E, 3C, 4A, 4B, 4C. See [aj] for retired var. among those listed here. | [45] | ||
Long March 5 | CHN | CALT | -- | 14,000 (CZ-5) | 8,000 (CZ-5) | -- | 12 [ak] | 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) | -- | -- | -- | 23 [al] | 23 | 23 | 23 | 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 | -- | -- | -- | 17 [am] | 16 | 16 | 16 | Active | 2016 | Var.: 7 | [50] [51] [52] | ||
-- | 7,000 | -- | Var.: 7A | |||||||||||||
Long March 8 | CHN | CALT | 4,500(SSO) | 2,800 | > 1,200 | -- | 3 [an] | 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 [ao] | 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) | -- | -- | -- | 1 [ap] | 1 | 1 | 1 | Active | 2024 | kerolox LV 3.8 metres diameter | [61] [62] [63] | ||
LVM3 | IND | ISRO | 10,000 | 4,000 | 2,180 | -- | 6 [aq] [ar] | 6 | 6 | 6 | Active | 2014 | Uprated cryo 2nd stage (C32) and semi-cryo 1st stage (SC120) variants expected | [64] [65] | ||
Maia | FRA | MaiaSpace | 500(SSO) | -- | -- | 0 | Devel. | 2025 | Planned first stage reuse | [66] | ||||||
Minotaur I | USA | Orbital ATK | 580 | -- | -- | -- | 12 [as] | 12 | 12 | 12 | Active | 2000 | Derived from the Minuteman II | [67] [68] | ||
Minotaur IV & V | USA | Orbital ATK | 1,735 | 640 | 447 | 50 | 8 [at] | 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 (Soorya) | IND | ISRO | 30,000 [77] | 10,000 | -- | -- | 0 | Devel. | NET 2032 | Program approved in 2024 | [78] | |||||
Nuri | ROK | KARI | 1,500 | -- | -- | 3 [au] | 3 | 2 | 2 | Active | 2021 | [79] [80] | ||||
OS-M | CHN | OneSpace | 205(M1) | -- | -- | -- | 1 [av] | 0 | 0 | 0 | Active | 2019 | Var.: M1, M2, M4. Single M1 failed launch; M2 & M4 in development. | [81] | ||
Pallas-1 | CHN | Galactic Energy | 5,000 3,000 (SSO) | -- | -- | -- | 0 | Devel. | Nov. 2024 | kerolox LV with reusable 1st stage | [82] [43] | |||||
Pegasus | USA | Orbital ATK | 450 | -- | -- | -- | 45 [aw] | 44 | 42 | 40 | Active | 1990 | [83] | |||
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 | [84] [85] | ||||||
Prime | UK | Orbex | 150(SSO) | -- | -- | -- | 0 | Devel. | NET 2023 | [86] [87] | ||||||
Proton (UR-500) | USSR RUS | Khrunichev | 23,000 | 6,920 | 5,680 | 65 (Proton-M) | 430 [ax] | 382 | Active | 1965 | Var.: K, M, Medium in development. | [88] [89] [90] | ||||
PSLV | IND | ISRO | 3,800 | 1,200 | 550 | -- | 61 [ay] | 60 | 59 | 58 | Active | 1993 | Var.: CA, XL, QL, DL Launched moon probe Chandrayaan I, Mars probe Mangalyaan I | [91] [92] | ||
Qaem-100 | IRN | IRGC | 80 | -- | -- | -- | 3 [az] | 3 | 2 | 2 | Active | 2023 | also one successful suborbital launch | [93] | ||
Qased | IRN | IRGC | ~50 | -- | -- | -- | 3 [ba] | 3 | 3 | 3 | Active | 2020 | [94] [95] | |||
RFA One | Germany | Rocket Factory Augsburg | 1,300 | 450 | -- | -- | 0 | Devel. | 2024 | 1st stage combustion in Europe, Orbital Stage. | [ citation needed ] [96] [97] [98] [99] | |||||
Rokot/Strela (UR-100N) | RUS | Eurockot Khrunichev | 2,100 | -- | -- | -- | 37 [bb] | 36 | 35 | 35 | Active | 1994 | 34 Rokot launches (no launches post-2019 due to Ukrainian tech ban); 3 Strela launches. | [100] [101] [102] [103] | ||
RS1 | USA | ABL Space Systems | 1,200 | -- | -- | 12 | 1 [bc] | 0 | 0 | 0 | Active | 2023 | [104] | |||
Shavit | ISR | IAI | 225 | -- | -- | 15 | 12 [bd] | 10 | 10 | 10 | Active | 1988 | Var.: Shavit, -1, -2 | [105] | ||
Simorgh | IRN | ISA | 350 | -- | -- | -- | 7 [be] | 7 | 2 | 2 | Active | 2016 | [106] | |||
SK solid fueled TV2 | ROK | MND | > 100 | -- | -- | -- | 1 [bf] | 1 | 1 | 1 | Active | 2023 | solid fueled launch vehicle | [107] | ||
SLS | USA | Orbital ATK Boeing United Launch Alliance Aerojet Rocketdyne | 95,000–130,000 | -- | 27,000–46,000 | -- | 1 [bg] | 1 | 1 | 1 | Active | 2022 | Var.: Block 1, Block 1B, Block 2 | [108] [109] | ||
Soyuz | USSR RUS | RSC Energia TsSKB-Progress | 8,200 | 2,400 | 1,200 | -- | 1,995 [bh] | [bi] | 1,870 [bj] | 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 | [110] [111] | |||
SS-520 | JPN | IHI Aerospace | 4 | -- | -- | -- | 2 [bk] | 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. | [112] | ||
SSLV | IND | ISRO | 500 | 300 | -- | -- | 3 [bl] | 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 ] | -- | 6 [bm] [bn] | 5 | 0 | 0 | test flights | 2023 | 1st flight intended a TAO orbit; 3rd flight suborbital | [113] [114] [115] [116] [117] | ||
150,000 (reusable) [ better source needed ] | ||||||||||||||||
Start-1 ( RT-2PM ) | RUS | MITT | 532 | -- | -- | -- | 7 [bo] | 6 | 6 | 6 | Active | 1993 | [118] | |||
Taurus / Minotaur-C | USA | Orbital Sciences | 1,450 | -- | -- | -- | 9 [bp] | 9 | 6 | 6 | Active | 1989 | Var.: 2110, 3110, 3210 | [119] | ||
Tianlong 2 | CHN | Space Pioneer | 2,000(LEO) 1,500 (500 km SSO) | -- | -- | 1 [bq] | 1 | 1 | 1 | Active | 2023 | liquid fueled (kerolox) carrier | [120] [121] | |||
Tianlong 3 | CHN | Space Pioneer | 17,000(LEO) 14,000 (500 km SSO) | -- | -- | 0 | Devel. | 2024 | kerolox with reusable 1st stage | [121] [122] | ||||||
Tronador | ARG | CONAE | 500 | Devel. | 2030 | |||||||||||
Unha | DPRK | KCST | 200 | -- | -- | -- | 4 [br] | 3 | 2 | Active | 2006 | Var.: Paektusan based on Taepodong-1 missile; Unha based on Taepodong-2 missile. | [123] [124] | |||
Vega | ITA FRA ESA | Avio | 2,300 | -- | -- | 23 | 25 [bs] | 24 | 22 | 22 | Active | 2012 | Vega, Vega-C, Vega-E in-development. | [125] | ||
Vikram | IND | Skyroot Aerospace | 720 | -- | -- | 0 | Devel. | NET 2023 | Var.: Vikram 1, Vikram II, Vikram III | [126] | ||||||
VLM | BRA | CTA | 150 | -- | -- | -- | 0 | Devel. | NET 2025 | [127] [128] [129] | ||||||
Vulcan | USA | ULA | 17,800–34,900 | 7,400–16,300 | -- | 99 | 2 [bt] | 2 | 2 | 2 | Active | 2024 | [130] [ non-primary source needed ] [131] [132] [133] | |||
Yenisei | RUS | TsSKB-Progress RSC Energia | 88,000–115,000 | 20,000-27,000 | 0 | Devel. | NET 2032 | [134] [135] [136] [137] | ||||||||
Zenit | USSR UKR RUS | Yuzhnoye | 13,740 | 6,160 | 4,098 | -- | 84 [bu] | 74 | 72 | Active | 1985 | Var.: 2, 2M (2SB, 2SLB), 3SL, 3SLB, 3SLBF | [138] | |||
Zephyr | FRA | Latitude | 100 | -- | -- | 0 | Devel. | 2025 | [139] | |||||||
Zero | JPN | Interstellar Technologies | 100(SSO) | -- | -- | 0 | Devel. | 2023 | [140] | |||||||
Zhuque-2 | CHN | LandSpace | 4,000(LEO) 1,500 (500 km SSO) [141] | -- | -- | 4 [bv] | 4 | 3 | 3 | Active | 2022 | Var.: ZQ-2 | 1st methalox LV to reach: space (2022), orbit (2023), orbit with payload (12/2023) | [36] [141] [142] | ||
6,000(LEO) 4,000 (500 km SSO) [142] | -- | -- | Var.: ZQ-2E | |||||||||||||
Zhuque-3 | CHN | LandSpace | 21,000(expendable) | -- | -- | 0 | Devel. | 2025 | methalox LV with reusable 1st stage; stainless steel body | [143] | ||||||
12,500–18,300 (1st stage recovered) | ||||||||||||||||
Zuljanah | IRN | ISA | 220 [144] | 0 | Devel. | NET 2023 | Two successful suborbital flights | [145] [144] |
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 | FRA ESA | Aérospatiale | — | 2,650 | — | -- | 28 | Retired | 1979 | 1989 | [146] [147] | ||||
Ariane 4 | FRA ESA | Aérospatiale | 7,000 | 4,720 | — | -- | 116 | Retired | 1988 | 2003 | Var.: 40, 42P, 42L, 44P, 44L, 44LP | [147] | |||
Ariane 5 | FRA ESA | Airbus | 21,000 | 10,735 [148] | — | 165–220 | 117 | 115 | 115 | 112 | Retired | 1996 | 2023 | Var.: G, G+, GS, ECA, ES. | [149] [150] [151] |
ASLV | IND | ISRO | 150 | -- | -- | -- | 4 | Retired | 1987 | 1994 | [152] | ||||
Athena I & II | USA | Lockheed ATK | 2,065 | -- | 295 | -- | 7 | Retired | 1995 | 2001 | Launch Lunar Prospector. [153] | [154] | |||
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. | [155] [156] [157] [158] | |||
Atlas II | USA | Lockheed | 8,618 | 3,833 | -- | -- | 63 | 63 | 63 | Retired | 1991 | 2004 | [159] [160] [161] | ||
Atlas III | USA | Lockheed | 10,759 | 4,609 | -- | -- | 6 | 6 | 6 | Retired | 2003 | 2005 | Var.: IIIA, IIIB | [162] [163] | |
Black Arrow | UK | RAE Westland | 132 | -- | -- | -- | 4 | 3 | Retired | 1969 | 1971 | [164] | |||
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 | [165] | |||
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. | [165] [166] [167] |
Delta III | USA | Boeing | 8,290 | 3,810 | -- | -- | 3 | 2 | 2 | Retired | 1998 | 2000 | [168] [169] | ||
Delta IV | USA | ULA | 23,040 | 13,130 | 9,000 | -- | 45 | 45 | 45 | 44 | Retired | 2002 | 2024 | Var.: M, M+, and Heavy. | [170] |
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 | [171] [172] [173] | ||||
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. | [174] [ citation needed ] |
Falcon 1 | USA | SpaceX | 420 [175] | -- | -- | 7.9 [175] | 5 [176] | 4 [175] | 2 [175] | 2 [176] | Retired [175] | 2006 | 2009 | ||
Feng Bao 1 ( DF-5 ) | CHN | SAST | 2,500 | -- | -- | -- | 8 | 4 | Retired | 1972 | 1981 | 3 successful suborbital flights | [177] | ||
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 | [178] | |||
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 | [150] [179] [180] | ||
Kaituozhe ( DF-31 ) | CHN | CALT | 800 | -- | -- | -- | 3 | 1 | 1 | 1 | Retired (likely) | 2002 | 2017 | Var.: KT-1, KT-2, KT2-A | [181] |
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 | [182] [183] [184] | |
Long March 1D | CHN | CALT | 740 | -- | -- | -- | 0 | Retired | 1995 | 2002 | 3 suborbital launches only (2 successful.) | [182] [183] [184] | |||
Mu 1-3-4 | JPN | Nissan Motor IHI | 770 | -- | -- | -- | 27 | Retired | 1966 | 1995 | Var.: 1, 3D, 4S, 3C, 3H, 3S, 3SII | [185] | |||
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 | [186] |
N-I & II | JPN | Mitsubishi | 2,000 | 730 | -- | -- | 15 | 15 | 15 | 14 [bw] | Retired | 1975 | 1987 | Derived from the American Delta rocket | [187] |
Naro | ROK | Khrunichev KARI | 100 | -- | -- | -- | 3 | 2 | 1 | 1 | Retired | 2009 | 2013 | First stage uses the Russian RD-151 engine | [188] |
Safir | IRN | ISA | 50 | -- | -- | -- | 8 [bx] | 5 | 4 | 4 | Retired | 2007 | 2019 | Numbers given here may be in dispute | [189] |
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 | [190] [191] |
Saturn V | USA | Boeing North American Douglas | 118,000 | -- | 47,000 | 185 | 13 | 13 | 13 | Retired | 1967 | 1973 | Var.: Apollo, Skylab | [190] [192] [193] | |
Scout | USA | US Air Force NASA | 210 | -- | -- | -- | 125 | 104 | Retired | 1960 | 1994 | Var.: X1, X2, A, D, G | [194] | ||
Shtil'/Volna-O ( R-29 ) | RUS | Makeyev | 430 | -- | -- | -- | 8 [by] | 7 | 2 | 2 | Retired (as commercial launchers) [195] | 1995 | 2006 | Var.: Volna, Shtil, 2.1, 2R, 3 | [195] |
SLV | IND | ISRO | 40 | -- | -- | -- | 4 | 3 | 3 | 2 | Retired | 1979 | 1983 | Launched Rohini satellite series | [196] |
STS (Space Shuttle) | USA | Alliant Martin Marietta Rockwell | 24,400 | 3,810 | -- | 450 | 135 | 134 | 134 | 133 | Retired | 1981 | 2011 | Orbiter mass: 68585 kg. | [197] |
Terran 1 | USA | Relativity Space | 1,250 | -- | -- | 1 | 1 | 0 | 0 | Retired | 2023 | 2023 | anticipates 3-D printing most rocket parts | [198] | |
Thor | USA | Douglas | 1,270 | -- | 38 | -- | 357 | Retired | 1957 | 1980 | Launched Pioneer & Explorer probes | [165] | |||
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 | [199] [200] | |||
Tsyklon ( R-36 ) | USSR UKR | Yuzhmash | 4,100 | -- | -- | -- | 259 | Retired | 1967 | 2009 | Var.: 1, 2, 3. | [201] | |||
Vanguard | USA | Martin | 23 | -- | -- | -- | 12 | 3 | Retired | 1957 | 1959 | [202] | |||
Zhuque-1 | CHN | LandSpace | 300 | -- | -- | 1 | 1 | 0 | 0 | Retired | 2018 | 2018 | [203] [204] |
The Kosmos rockets were a series of Soviet and subsequently Russian rockets, derived from the R-12 and R-14 missiles, the best known of which is the Kosmos-3M, which has made over 440 launches. The Kosmos family contained a number of rockets, both carrier rockets and sounding rockets, for orbital and sub-orbital spaceflight respectively. The first variant, the Kosmos, first flew on 27 October 1961. Over 700 Kosmos rockets have been launched overall.
The Minotaur is a family of United States solid-fuel launch vehicles repurposed from retired Minuteman and Peacekeeper model intercontinental ballistic missiles. Built by Northrop Grumman under the Space Force's Rocket Systems Launch Program, these vehicles are used for various space and test launch missions.
ChinaSat is the brand name of communications satellites operated by China Satellite Communications.
This comparison of orbital launch systems lists the attributes of all current and future individual rocket configurations designed to reach orbit. A first list contains rockets that are operational or have attempted an orbital flight attempt as of 2024; a second list includes all upcoming rockets. For the simple list of all conventional launcher families, see: Comparison of orbital launchers families. For the list of predominantly solid-fueled orbital launch systems, see: Comparison of solid-fueled orbital launch systems.
The Zenit 3SLB or Zenit-3M was a Ukrainian expendable carrier rocket derived from the Zenit-2SB. It was a member of the Zenit family of rockets, which were designed by the Yuzhnoye Design Office. Produced at Yuzhmash, the rocket was a modified version of the Zenit-3SL, designed to be launched from a conventional launch pad rather than the Sea Launch Ocean Odyssey platform. Most of components of the rocket were produced in Russia. The Ukrainian space industry was highly integrated with that of Russia due to its Soviet heritage, but that cooperation was interrupted by the Russo-Ukrainian War beginning in 2014, which effectively led to a hiatus in the Zenit program. The subsequent Russian invasion of Ukraine in 2022 saw damage to its manufacturing facilities due to Russian missile strikes, and what survived those strikes pivoted to producing military weapons.
The Long March 6 or Chang Zheng 6 as in pinyin, abbreviated LM 6 for export or CZ 6 within China, is a Chinese liquid-fuelled launch vehicle of the Long March family, which was developed by the China Aerospace Science and Technology Corporation (CASC) and the Shanghai Academy of Spaceflight Technology (SAST). The rocket was developed in the 2000s, and made its maiden flight in 2015. As one of the new generation rocket family, the Long March 6 was designed to be a light capacity, "high-speed response" rocket, complementing the heavy lift Long March 5 and the mid-heavy lift Long March 7 rocket families. It is capable of placing at least 1,000 kg (2,200 lb) of payload into a Sun-synchronous orbit. The first stage of the Long March 6 was derived from the booster rockets being developed for the Long March 5 rocket. It is powered by a YF-100 engine, which generates 1,340 kN (300,000 lbf) of thrust from burning kerosene and LOX as rocket fuel and oxidiser. This was the first flight of the new engine design.
A heavy-lift launch vehicle (HLV) is an orbital launch vehicle capable of generating a large amount of lift to reach its intended orbit. Heavy-lift launch vehicles generally are capable of lifting payloads between 20,000 to 50,000 kg or between 20,000 to 100,000 kilograms into low Earth orbit (LEO). As of 2024, operational heavy-lift launch vehicles include the Long March 5 and the Proton-M.
This article documents notable spaceflight events during the year 2019.
Notable spaceflight activities in 2017 included the maiden orbital flight of India's Geosynchronous Satellite Launch Vehicle Mark III on 5 June and the first suborbital test of Rocket Lab's Electron rocket, inaugurating the Mahia spaceport in New Zealand. The rocket is named for its innovative Rutherford engine which feeds propellants via battery-powered electric motors instead of the usual gas generator and turbopumps.
This article documents notable spaceflight events during the year 2018. For the first time since 1990, more than 100 orbital launches were performed globally.
Kuaizhou is a family of Chinese "quick-reaction" orbital launch vehicles. Flying since 2013, Kuaizhou 1 and 1A consist of three solid-fueled rocket stages, with a liquid-fueled fourth stage as part of the satellite system. Kuaizhou 11, which flew an unsuccessful maiden flight in July 2020, is a larger model able to launch a 1,500 kg (3,300 lb) payload into low Earth orbit. Heavy-lift models KZ-21 and KZ-31 are in development. The Kuaizhou series of rockets is manufactured by ExPace, a subsidiary of China Aerospace Science and Industry Corporation (CASIC), as their commercial launch vehicles.
A medium-lift launch vehicle (MLV) is a rocket launch vehicle that is capable of lifting between 2,000 to 20,000 kg by NASA classification or between 5,000 to 20,000 kilograms by Russian classification of payload into low Earth orbit (LEO). An MLV is between small-lift launch vehicles and heavy-lift launch vehicles.
A small-lift launch vehicle is a rocket orbital launch vehicle that is capable of lifting 2,000 kilograms (4,400 lb) or less or under 5,000 kilograms (11,000 lb) of payload into low Earth orbit (LEO). The next larger category consists of medium-lift launch vehicles.
LandSpace Technology Corporation is a Chinese commercial space launch provider based in Beijing. It was founded in 2015 by Zhang Changwu.
This article documents notable spaceflight events during the year 2020.
Spaceflight in 2025 promises to follow the 2020s trend of record breaking orbital launches and increased developments in lunar, Mars and low-earth orbit exploration.
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.
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.