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).
Description
edit- Family: Name of the family/model of launcher
- Country: Origin country of launcher
- Manufac.: Main manufacturer
- Payload: Maximum mass of payload, for 3 altitudes
- LEO, low Earth orbit
- GTO, geostationary transfer orbit
- TLI, trans-Lunar injection
- Cost: Price for a launch at this time, in millions of US$
- Launches reaching...
- Total: Flights which lift-off, or where the vehicle is destroyed during the terminal count
Note: only includes orbital launches (flights launched with the intention of reaching orbit). Suborbital tests launches are not included in this listing. - Space (regardless of outcome): Flights which reach approximately 100 km or more above Earth's surface.
- Any orbit (regardless of outcome): Flights which achieve at least one complete orbit even if the orbit differs from the targeted orbit.
- Target orbit (without damage to the payload)
- Total: Flights which lift-off, or where the vehicle is destroyed during the terminal count
- Status: Actual status of launcher (retired, development, active)
- Date of flight
- First: Year of first flight of first family member
- Last (if applicable): Year of Last flight (for vehicles retired from service)
- Refs: citations
Same cores are grouped together (like Ariane 1, 2 & 3, but not V).
List of active and under-development launcher families
edit- Legend
- Active or undergoing orbital test flightsUnder-development
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[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 | EU | 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 | 54[k] | 54 | 50 | 50 | 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 | 397[m][n] | 395 | 395 | 394 | 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 | 400 (KZ-1A) | -- | -- | -- | 32[z][aa] | 31[ab] | 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[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 | 473[af][ag] | 467[ah] | 464 | 456 | 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) |
-- | -- | -- | 22[al] | 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[am] | 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[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) |
-- | -- | -- | 0 | Devel. | 2024 | kerolox LV 3.8 metres diameter |
[61][62][63] | |||||
LVM3 | IND | ISRO | 10,000 | 4,000 | 2,180 | -- | 6[ap] [aq] | 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[ar] | 12 | 12 | 12 | Active | 2000 | Derived from the Minuteman II | [67][68] | ||
Minotaur IV & V | USA | Orbital ATK | 1,735 | 640 | 447 | 50 | 8[as] | 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 | Budgetary allocation of USD 1 Bn approved in 2024, with development program completion expected within 96 months | [78] | |||||
Nuri | ROK | KARI | 1,500 | -- | -- | 3[at] | 3 | 2 | 2 | Active | 2021 | [79][80] | ||||
OS-M | CHN | OneSpace | 205 (M1) | -- | -- | -- | 1[au] | 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[av] | 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[aw] | 382 | Active | 1965 | Var.: K, M, Medium in development. | [88][89][90] | ||||
PSLV | IND | ISRO | 3,800 | 1,200 | 550 | -- | 60[ax] | 59 | 58 | 57 | Active | 1993 | Var.: CA, XL, QL, DL Launched moon probe Chandrayaan I, Mars probe Mangalyaan I |
[91][92] | ||
Qaem-100 | IRN | IRGC | 80 | -- | -- | -- | 3[ay] | 3 | 2 | 2 | Active | 2023 | also one successful suborbital launch | [93] | ||
Qased | IRN | IRGC | ~50 | -- | -- | -- | 3[az] | 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[ba] | 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[bb] | 0 | 0 | 0 | Active | 2023 | [104] | |||
Shavit | ISR | IAI | 225 | -- | -- | 15 | 12[bc] | 10 | 10 | 10 | Active | 1988 | Var.: Shavit, -1, -2 | [105] | ||
Simorgh | IRN | ISA | 350 | -- | -- | -- | 6[bd] | 6 | 1 | 1 | Active | 2016 | [106] | |||
SK solid fueled TV2 | ROK | MND | > 100 | -- | -- | -- | 1[be] | 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[bf] | 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 | -- | 1,992[bg] | [bh] | 1,867[bi] | 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[bj] | 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[bk] | 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[bl][bm] | 4 | 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[bn] | 6 | 6 | 6 | Active | 1993 | [118] | |||
Taurus / Minotaur-C | USA | Orbital Sciences | 1,450 | -- | -- | -- | 9[bo] | 9 | 6 | 6 | Active | 1989 | Var.: 2110, 3110, 3210 | [119] | ||
Tianlong 2 | CHN | Space Pioneer | 2,000 (LEO) 1,500 (500 km SSO) |
-- | -- | 1[bp] | 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[bq] | 3 | 2 | Active | 2006 | Var.: Paektusan based on Taepodong-1 missile; Unha based on Taepodong-2 missile. | [123][124] | |||
Vega | EU | Avio | 2,300 | -- | -- | 23 | 24[br] | 23 | 21 | 21 | 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[bs] | 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[bt] | 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 | 6,000 (LEO) 4000 (500 km SSO)[141] |
-- | -- | 3[bu] | 3 | 2 | 2 | Active | 2022 | 1st methalox LV to reach: space (2022), orbit (2023), orbit with payload (12/2023) |
[36][141] | |||
Zhuque-3 | CHN | LandSpace | 21,000 (expendable) | -- | -- | 0 | Devel. | 2025 | methalox LV with reusable 1st stage; stainless steel body | [142] | ||||||
12,500–18,300 (1st stage recovered) | ||||||||||||||||
Zuljanah | IRN | ISA | 220[143] | 0 | Devel. | NET 2023 | Two successful suborbital flights | [144][143] |
List of retired launcher families
edit- Legend
- Retired
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 | [145][146] | ||||
Ariane 4 | EU | Aérospatiale | 7,000 | 4,720 | — | -- | 116 | Retired | 1988 | 2003 | Var.: 40, 42P, 42L, 44P, 44L, 44LP | [146] | |||
Ariane 5 | EU | Airbus | 21,000 | 10,735[147] | — | 165–220 | 117 | 115 | 115 | 112 | Retired | 1996 | 2023 | Var.: G, G+, GS, ECA, ES. | [148][149][150] |
ASLV | IND | ISRO | 150 | -- | -- | -- | 4 | Retired | 1987 | 1994 | [151] | ||||
Athena I & II | USA | Lockheed ATK | 2,065 | -- | 295 | -- | 7 | Retired | 1995 | 2001 | Launch Lunar Prospector.[152] | [153] | |||
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. |
[154][155][156][157] | |||
Atlas II | USA | Lockheed | 8,618 | 3,833 | -- | -- | 63 | 63 | 63 | Retired | 1991 | 2004 | [158][159][160] | ||
Atlas III | USA | Lockheed | 10,759 | 4,609 | -- | -- | 6 | 6 | 6 | Retired | 2003 | 2005 | Var.: IIIA, IIIB | [161][162] | |
Black Arrow | UK | RAE Westland | 132 | -- | -- | -- | 4 | 3 | Retired | 1969 | 1971 | [163] | |||
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 |
[164] | |||
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. |
[164][165][166] |
Delta III | USA | Boeing | 8,290 | 3,810 | -- | -- | 3 | 2 | 2 | Retired | 1998 | 2000 | [167][168] | ||
Delta IV | USA | ULA | 23,040 | 13,130 | 9,000 | -- | 45 | 45 | 45 | 44 | Retired | 2002 | 2024 | Var.: M, M+, and Heavy. | [169] |
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 | [170][171][172] | ||||
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. | [173][citation needed] |
Falcon 1 | USA | SpaceX | 420[174] | -- | -- | 7.9[174] | 5[175] | 4[174] | 2[174] | 2[175] | Retired[174] | 2006 | 2009 | ||
Feng Bao 1 (DF-5) |
CHN | SAST | 2,500 | -- | -- | -- | 8 | 4 | Retired | 1972 | 1981 | 3 successful suborbital flights | [176] | ||
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 | [177] | |||
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 | [149][178][179] | ||
Kaituozhe (DF-31) |
CHN | CALT | 800 | -- | -- | -- | 3 | 1 | 1 | 1 | Retired (likely) | 2002 | 2017 | Var.: KT-1, KT-2, KT2-A | [180] |
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 | [181][182][183] | |
Long March 1D | CHN | CALT | 740 | -- | -- | -- | 0 | Retired | 1995 | 2002 | 3 suborbital launches only (2 successful.) | [181][182][183] | |||
Mu 1-3-4 | JPN | Nissan Motor IHI | 770 | -- | -- | -- | 27 | Retired | 1966 | 1995 | Var.: 1, 3D, 4S, 3C, 3H, 3S, 3SII | [184] | |||
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 | [185] |
N-I & II | JPN | Mitsubishi | 2,000 | 730 | -- | -- | 15 | 15 | 15 | 14[bv] | Retired | 1975 | 1987 | Derived from the American Delta rocket | [186] |
Naro | ROK | Khrunichev KARI | 100 | -- | -- | -- | 3 | 2 | 1 | 1 | Retired | 2009 | 2013 | First stage uses the Russian RD-151 engine | [187] |
Safir | IRN | ISA | 50 | -- | -- | -- | 8[bw] | 5 | 4 | 4 | Retired | 2007 | 2019 | Numbers given here may be in dispute | [188] |
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 | [189][190] |
Saturn V | USA | Boeing North American Douglas | 118,000 | -- | 47,000 | 185 | 13 | 13 | 13 | Retired | 1967 | 1973 | Var.: Apollo, Skylab | [189][191][192] | |
Scout | USA | US Air Force NASA | 210 | -- | -- | -- | 125 | 104 | Retired | 1960 | 1994 | Var.: X1, X2, A, D, G | [193] | ||
Shtil'/Volna-O (R-29) |
RUS | Makeyev | 430 | -- | -- | -- | 8[bx] | 7 | 2 | 2 | Retired (as commercial launchers)[194] | 1995 | 2006 | Var.: Volna, Shtil, 2.1, 2R, 3 | [194] |
SLV | IND | ISRO | 40 | -- | -- | -- | 4 | 3 | 3 | 2 | Retired | 1979 | 1983 | Launched Rohini satellite series | [195] |
STS (Space Shuttle) |
USA | Alliant Martin Marietta Rockwell | 24,400 | 3,810 | -- | 450 | 135 | 134 | 134 | 133 | Retired | 1981 | 2011 | Orbiter mass: 68585 kg. | [196] |
Terran 1 | USA | Relativity Space | 1,250 | -- | -- | 1 | 1 | 0 | 0 | Retired | 2023 | 2023 | anticipates 3-D printing most rocket parts | [197] | |
Thor | USA | Douglas | 1,270 | -- | 38 | -- | 357 | Retired | 1957 | 1980 | Launched Pioneer & Explorer probes | [164] | |||
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 |
[198][199] | |||
Tsyklon (R-36) |
USSR UKR |
Yuzhmash | 4,100 | -- | -- | -- | 259 | Retired | 1967 | 2009 | Var.: 1, 2, 3. | [200] | |||
Vanguard | USA | Martin | 23 | -- | -- | -- | 12 | 3 | Retired | 1957 | 1959 | [201] | |||
Zhuque-1 | CHN | LandSpace | 300 | -- | -- | 1 | 1 | 0 | 0 | Retired | 2018 | 2018 | [202][203] |
See also
editNotes
edit- ^ Number of Alpha launches current as of 04 July 2024.
- ^ Number of Angara 1.2 + A5 launches current as of 17 September 2024.
- ^ Number of Antares launches current as of 02 August 2023.
- ^ The only currently available version, Antares 230+, has only one launch planned, in July 2023. After that, the development period will follow.
- ^ Number of Ariane 6 launches current as of 09 July 2024.
- ^ Number of Astra launches current as of 12 June 2022.
- ^ Number of Atlas V launches current as of 30 July 2024.
- ^ All remaining planned launches are sold.
- ^ Number of Ceres-1 launches current as of 29 August 2024.
- ^ Number of Chollima-1 launches current as of 27 May 2024.
- ^ Number of Electron launches current as of 05 November 2024.
- ^ Number of Epsilon launches current as of 12 October 2022.
- ^ Number of Falcon 9 launches are updated via manual input into "Template:Falcon rocket statistics". Said page was last updated on 14 November 2024.
- ^ One flight put primary but not secondary payload into correct orbit,[21] one rocket and payload were destroyed before launch in preparation for static fire[22][non-primary source needed] and thus is not counted.
- ^ Upgraded to version 1.1 in 2013.
- ^ Upgraded to version FT in 2015.
- ^ Falcon rocket statistics template page last updated on 14 November 2024.
- ^ Number of Gravity-1 launches current as of 11 January 2024.
- ^ Number of GSLV Mark II launches current as of 17 February 2024.
- ^ Number of H-II (all versions) launches current as of 26 September 2024.
- ^ Number of H3 launches current as of 04 November 2024.
- ^ Number of Hyperbola-1 launches current as of 10 July 2024.
- ^ Jielong 1 launch numbers current as of 17 August 2019.
- ^ Jielong 3 launch numbers current as of 24 September 2024.
- ^ Number of KAIROS launches current as of 13 March 2024.
- ^ Number of Kuaizhou launches current as of 20 September 2024.
- ^ Number of Kuaizhou launches excludes a successful suborbital test launch on 17 March 2012.
- ^ According to cited reference, a KZ-11 3rd stage failed to ignite during the launch on 10 July 2020; also, the KZ-1A launch on 12 September 2020 experienced a 4th-stage failure. Both launches likely reached space.
- ^ LauncherOne launch numbers current as of 9 January 2023.
- ^ The parent company suspended operations and declared bankruptcy
- ^ Lijian-1 launch numbers current as of 11 November 2024.
- ^ Number of Long March 2-3-4 launches current as of 13 November 2024.
- ^ The total number of launches in the CZ-2,3,4 series listed here does not include 6 possible launches [5 possilbe successes and 1 possible failure] of the CZ-2C (3) var. noted in reference.[44]
- ^ Sources from List of Long March launches are unclear regarding whether 3 failed launches in the CZ-2,3,4 series reached space; thus the number quoted here is the minimum number of launches that reached space while the actual possible number could be greater than the quoted number by up to three.
- ^ CZ-2F is the crew-rated launcher for the Shenzhou spacecraft.
- ^ As of 21 February 2020, the following var. in the Long March 2-3-4 family of launchers have been retired: 2A, 2E, 3, 3B, and 4A.
- ^ Number of Long March 5 launches current as of 3 May 2024.
- ^ Number of Long March 6 launches current as of 22 October 2024.
- ^ Number of Long March 7 launches current as of 22 August 2024.
- ^ Number of Long March 8 launches current as of 20 March 2024.
- ^ Number of Long March 11 launches current as of 25 December 2023.
- ^ Number of GSLV LVM-3 launches current as of 14 July 2023.
- ^ LVM-3 launch numbers do not include one successful suborbital flight.
- ^ Number of Minotaur I launches current as of 15 June 2021.
- ^ Number of Minotaur IV and V launches current as of 15 July 2020.
- ^ Number of Nuri launches current as of 25 May 2023.
- ^ Number of OS-M launches current as of 27 March 2019.
- ^ Number of Pegasus launches current as of 13 June 2021.
- ^ Number of Proton launches current as of 12 March 2023.
- ^ Number of PSLV launches current as of 01 January 2024.
- ^ Number of Qaem-100 launches current as of 14 September 2024.
- ^ Number of Qased launches current as of 27 September 2023.
- ^ Number of Rokot+Strela launches current as of 26 December 2019.
- ^ Number of RS1 launches current as of 20 January 2023.
- ^ Number of Shavit launches current as of 28 March 2023
- ^ Number of Simorgh launches current as of 28 January 2024.
- ^ Number of TV2 launches current as of 04 December 2023.
- ^ Number of SLS launches current as of 16 November 2022.
- ^ Number of R-7 Semyorka/Soyuz launches current as of 04 November 2024.
- ^ Due to the existence of ICBM variants, suborbital flights, and the large total number of flights, the number of launches reaching space and those reaching any orbit are not given here in order to lessen the possible dissemination of inaccurate information.
- ^ The total number of launches and launch successes are taken from the R-7 Semyorka Wikipedia page.
- ^ Number of SS-520 launches current as of 3 February 2018.
- ^ Number of SSLV launches current as of 16 August 2024.
- ^ Number of Starship launches current as of 12 October 2024.
- ^ Starship test launches are intended as pseudo-orbital flights (may be considered as suborbital) and so are included in this list for now.
- ^ Number of Start-1/Start launches current as of 25 April 2006.
- ^ Number of Taurus/Minotaur-C launches current as of 31 October 2017.
- ^ Number of Tianlong-2 launches current as of 02 April 2023.
- ^ Number of Unha-2/Unha-3 launches current as of 7 February 2016.
- ^ Number of Vega (all versions) launches current as of 5 September 2024.
- ^ Number of Vulcan launches current as of 04 October 2024.
- ^ Number of Zenit launches current as of 26 December 2017.
- ^ Number of Zhuque-2 launches current as of 08 December 2023.
- ^ One N-I launch partially failed due to recontact between satellite and upper stage.
- ^ Number of Safir launches current as of 29 August 2019. Number of launches and possible outcomes are in dispute. See main page at Safir.
- ^ 5 of the 8 launches were suborbital (of which 2 failed); 3 of the 8 launches were intended for LEO (2 successes).[194]
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Russian officials have said they plan to discontinue Dnepr launches.
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