This page contains a list of orbital launchers' families. To see the long complete list of launch systems, see Comparison of orbital launch systems.
This is a comparison of orbital launch systems. The following exposes the full list of conventional orbital launch systems. For the short simple list of conventional launcher families, see: Comparison of orbital launchers families. For the list of predominantly solid-fuelled orbital launch systems, see: Comparison of solid-fuelled orbital launch systems.
A Low Earth Orbit (LEO) is an Earth-centered orbit with an altitude of 2,000 km (1,200 mi) or less, or with at least 11.25 periods per day and an eccentricity less than 0.25. Most of the manmade objects in space are in LEO. A histogram of the mean motion of the cataloged objects shows that the number of objects drops significantly beyond 11.25.
A geosynchronous transfer orbit or geostationary transfer orbit (GTO) is a Hohmann transfer orbit—an elliptical orbit used to transfer between two circular orbits of different radii in the same plane—used to reach geosynchronous or geostationary orbit using high-thrust chemical engines.
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 | |||||||
Angara 1.2 | Khrunichev | 3,800 | -- | -- | 25 | 1 | 1 | 0 | N/A | Active | 2014 | As of 2017, only launch was suborbital [1] | [2] [3] [4] | ||
Angara A5 | Khrunichev | 14,600–35,000 | 3,600–12,500 | -- | -- | 1 | 1 | 1 | 1 | Active | 2014 | [2] [5] | |||
Antares | Orbital ATK | 6,500 | -- | -- | 80 | 7 | 6 | 6 | 6 | Active | 2013 | Cygnus launcher | [6] [7] [8] | ||
Ariane 1-2-3 | Aérospatiale | N/A | 2,650 | N/A | -- | 28 | Retired | 1979 | 1989 | [9] [10] | |||||
Ariane 4 | Aérospatiale | 7,000 | 4,720 | N/A | -- | 116 | Retired | 1988 | 2003 | Var.: 40, 42P, 42L, 44P, 44L, 44LP | [10] | ||||
Ariane 5 | Airbus | 21,000 | 10,735 [11] | N/A | 165–220 | 76 | 74 | 74 | 72 | Active | 1996 | Var.: G, G+, GS, ECA, ES. | [12] [13] [14] | ||
Ariane 6 | Airbus Safran | 21,500 | 11,500 | N/A | 115 | 0 | Devel. | 2020 | Var.: Ariane 62, Ariane 64. | ||||||
ASLV | ISRO | 150 | -- | -- | -- | 4 | Retired | 1987 | 1994 | [15] | |||||
Athena I & II | Lockheed ATK | 2,065 | -- | 295 | -- | 7 | Retired | 1995 | 2001 | Launch Lunar Prospector. [16] | [17] | ||||
Atlas A-B-C-D-E-F-G Atlas I | Lockheed | 5,900 | 2,340 | -- | -- | 514 | Retired | 1957 | 1997 | Launch Mercury. Atlas or Centaur upper stage. | [18] [19] [20] [21] | ||||
Atlas II | Lockheed | 8,618 | 3,833 | -- | -- | 63 | 63 | 63 | Retired | 1991 | 2004 | [22] [23] [24] | |||
Atlas III | Lockheed | 10,759 | 4,609 | -- | -- | 6 | 6 | 6 | Retired | 2003 | 2005 | Var.: IIIA, IIIB | [25] [26] | ||
Atlas V | ULA | 18,850 | 8,900 | 2,807 | 109–153 | 74 | 74 | 74 | 73 | Active | 2002 | Launched Juno & New Horizons | [27] [28] | ||
BFR | SpaceX | 100,000+ | -- | 100,000+ [lower-alpha 1] | -- | 0 | Devel. | 2020 | Fully reusable. Expected as early as 2020, with suborbital spaceship tests beginning in the first half of 2019. | [29] [30] [31] [32] | |||||
Black Arrow | RAE Westland | 132 | -- | -- | -- | 4 | 3 | Retired | 1969 | 1971 | [33] | ||||
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 | [34] [35] | ||||
Delta II | 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. | [34] [36] [37] | |
Delta III | Boeing | 8,290 | 3,810 | -- | -- | 3 | 2 | 2 | Retired | 1998 | 2000 | [38] [39] | |||
Delta IV | ULA | 23,040 | 13,130 | 9,000 | -- | 35 | 35 | 35 | 34 | Active | 2002 | Var.: M, M+, and Heavy. | [40] | ||
Diamant | SEREB | -- | -- | -- | 12 | 9 | Retired | 1965 | 1975 | [ citation needed ] | |||||
R-36M Dnepr | Yuzhmash | 3,600 | -- | 750 | 14 | 17 | Retired | 1999 | 2015 | [41] [42] [ full citation needed ] [43] | |||||
Electron | Rocket Lab | 225 | 6 | 2 | 2 | 1 | 1 | Active | 2017 | [44] | |||||
Energia | NPO Energia | 100,000 | 240 | 2 | 2 | 1 | 1 | Retired | 1987 | 1988 | 1 partial failure with Polyus spacecraft, 1 successful flight with Buran shuttle. | [45] [ citation needed ] | |||
Epsilon | IHI Corporation | 1,200 | -- | -- | -- | 1 | 1 | 1 | 1 | Active | 2013 | [46] [47] | |||
Falcon 1 | SpaceX | 420 [48] | -- | -- | 7.9 [48] | 5 [49] | 4 [48] | 2 [48] | 2 [49] | Retired [48] | 2006 | 2009 | |||
Falcon 9 v1.0, v1.1, FT, B5 | SpaceX | 22,800 | 8,300 | -- | 61.2 | 66 | 65 | 65 | 65 | Active | 2010 | Upgrade to version 1.1 in 2013; upgrade to version FT in 2015 Launcher of Dragon capsule. One flight put primary but not secondary payload into correct orbit, [50] one rocket and payload were destroyed before launch in preparation for static fire [51] and thus is not counted. Falcon 9 Block 5 first launched 11th May 2018 with Bangabandhu 1, the first fully sized Bangladesh satellite. | [52] [53] | ||
Falcon Heavy | SpaceX | 63,800 | 26,700 | -- | 90–150 | 1 | 1 | 1 | 1 | Active | 2018 | First test launch 2018-02-06 | [54] [55] [56] | ||
GSLV Mk.I | ISRO | 5,000 | 2,500 | -- | -- | 6 | 4 | 2 | 2 | Retired | 2001 | 2010 | [57] [58] [59] | ||
GSLV Mk.II | ISRO | 5,000 | 2,700 | -- | -- | 7 | 6 | 6 | 6 | Active | 2010 | [57] [60] [59] | |||
GSLV Mk.III (LVM3) | ISRO | 10,000 | 4,000 | -- | -- | 3 | 3 | 3 | 3 | Active | 2014 | [61] [62] | |||
H-I | Mitsubishi | 3,200 | -- | -- | 9 | 9 | Retired | 1986 | 1992 | License-built version of the Thor-ELT | [63] | ||||
H-II, IIA & IIB | Mitsubishi | 19,000 | 8,000 | -- | (190), 90, 112 | 28 | 26 | Active | 1994 | Var.: A202, A2022, A2024, A204, B | [64] | ||||
Haas | ARCA | 400 | -- | -- | 0 | Devel. | 2018 | Launch from balloon | [65] [66] | ||||||
J-I | IHI Corporation Nissan Motors | 880 | -- | -- | -- | 1 | Retired | 1996 | 1996 | Partial demonstration flight only | [ citation needed ] | ||||
R-12 & R-14 Kosmos | Yuzhnoye Polyot | 1,500 | -- | -- | 12 | 610 | 559 | Retired | 1967 | 2010 | Var.: 1, 2, 3, 3M | [13] [67] [68] | |||
Kaituozhe | CALT | -- | -- | -- | 3 | 0 | Active | 2002 | Var.: 1, 2 | [ citation needed ] | |||||
Lambda 4S | Nissan ISAS | -- | -- | -- | 5 | 1 | Retired | 1966 | 1970 | [ citation needed ] | |||||
Long March 1 | CALT | 740 | 440 | -- | -- | 6 | Retired | 1970 | 2002 | Var.: 1, 1D | [69] [70] [71] | ||||
DF-5 Long March 2-3-4 | CALT | 12,000 | 5,500 | 3,300 | -- | 167 | 158 | Active | 1971 | Var.: 2A, 2C, 2D, 2E, 3, 3A, 3B, 3C, 4, 4B Launcher of Shenzhou | [72] | ||||
Long March 5 | CALT | 25,000 | 14,000 | 8,000 | -- | 2 | 2 | 1 | 1 | Active | 2016 | Var.: 5, 5B | [73] [74] | ||
Long March 6 | CALT | 1,500 | -- | -- | -- | 1 | 1 | 1 | 1 | Active | 2015 | [75] | |||
Long March 7 | CALT | 20,000 | -- | -- | -- | 1 | 1 | 1 | 1 | Active | 2016 | [76] | |||
Minotaur I | Orbital ATK | 580 | -- | -- | -- | 11 | 11 | 11 | 11 | Active | 2000 | Derived from the Minuteman II | [77] [78] | ||
Minotaur IV & V | Orbital ATK | 1,735 | 640 | 447 | 50 | 4 | 4 | 4 | 4 | Active | 2010 | Also 2 suborbital launches (HTV-2a). Var.: IV, IV Lite, IV HAPS, V. Derived from Peacekeeper missile | [77] [79] | ||
Mu 1-3-4 | Nissan Motor IHI | 770 | -- | -- | -- | 27 | Retired | 1966 | 1995 | Var.: 1, 3D, 4S, 3C, 3H, 3S, 3SII | [80] | ||||
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 | [81] | |
N-I & II | Mitsubishi | 2,000 | 730 | -- | -- | 15 | Retired | 1975 | 1987 | Derived from the American Delta rocket | [82] | ||||
Naro | Khrunichev KARI | 100 | -- | -- | -- | 3 | 2 | 1 | 1 | Retired | 2009 | 2013 | First stage uses the Russian RD-151 engine | [83] | |
Pegasus | Orbital ATK | 450 | -- | -- | -- | 43 | 42 | 41 | 38 | Active | 1990 | [84] | |||
UR-500 Proton | Khrunichev | 23,000 | 6,920 | 5,680 | 65 (Proton-M) | 399 | 353 | Active | 1965 | Var.: K, M, Medium in development. | [85] [86] [87] | ||||
PSLV | ISRO | 3,800 | 1,300 | -- | -- | 45 | 44 | 43 | 42 | Active | 1993 | Var.: CA, XL, HP, 3S Launched moon probe Chandrayaan I, Mars probe Mangalyaan I | [88] [89] | ||
UR-100N Rokot Strela | Eurockot Khrunichev | 2,100 | -- | -- | -- | 25 | 23 | 23 | Active | 1994 | 23 launches of Rokot; 2 launches of Strela | [90] [91] [92] [93] | |||
Safir | ISA | 50 | -- | -- | -- | 7 | 5 | 4 | 4 | Active | 2007 | [94] | |||
Saturn I & IB | Chrysler Douglas | 18,600 | -- | -- | 19 | 13 | 13 | 13 | 13 | Retired | 1961 | 1975 | Saturn 1 family also included 6 suborbital test launches | [95] [96] | |
Saturn V | Boeing North American Douglas | 118,000 | -- | 47,000 | 185 | 13 | 13 | 13 | Retired | 1967 | 1973 | Var.: Apollo, Skylab | [95] [97] [98] | ||
Scout | US Air Force NASA | 210 | -- | -- | -- | 125 | 104 | Retired | 1960 | 1994 | Var.: X1, X2, A, D, G | [99] | |||
Shavit | IAI | 225 | -- | -- | 15 | 10 | 8 | 8 | 8 | Active | 1988 | Var.: Shavit, -1, -2 | [100] | ||
R-29 Shtil Volna | Makeyev | 430 | -- | -- | -- | 8 | Retired | 1995 | 2006 | Var.: Volna, Shtil, 2.1, 2R, 3 | [101] | ||||
R-7 Semyorka Soyuz | RSC Energia TsSKB-Progress | 8,200 | 2,400 | 1,200 | -- | 1,854 | 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 | [102] [103] | |||||
Simorgh | ISA | 350 | -- | -- | -- | 2 | 0 | 0 | 0 | Active | 2016 | [104] | |||
SLS | Orbital ATK Boeing United Launch Alliance Aerojet Rocketdyne | 70,000 to 130,000 | -- | -- | -- | 0 | Devel. | 2020 | Expected 2020 | [105] [106] | |||||
SLV | ISRO | 40 | -- | -- | -- | 4 | 3 | 3 | 2 | Retired | 1979 | 1983 | Launched Rohini satellite series | [107] | |
SS-520 | IHI Aerospace | 4 | -- | -- | -- | 4 | 3 | 1 | 1 | 2017 | Two successful suborbital flights, one failed and one successful attempt to reach orbit. A test how small orbital rockets can be. The rocket has a mass of only 2.6 tonnes. | [108] | |||
Small Satellite Launch Vehicle | ISRO | 500 | 300 | -- | -- | 0 | Devel. | 2019 | As of December 2018, design of the rocket has been completed and first developmental flight is to take place before May 2019. | [109] [110] | |||||
STS Space Shuttle | Alliant Martin Marietta Rockwell | 24,400 | 3,810 | -- | 450 | 135 | 134 | 134 | 133 | Retired | 1981 | 2011 | Orbiter mass: 68585 kg. | [111] | |
RT-2PM Start-1 | MITT | 532 | -- | -- | -- | 7 | 6 | Active | 1993 | [112] | |||||
Taurus / Minotaur-C | Orbital Sciences | 1,450 | -- | -- | -- | 9 | 9 | 6 | 6 | Active | 1989 | Var.: 2110, 3110, 3210 | [113] | ||
Thor | Douglas | 1,270 | -- | 38 | -- | 357 | Retired | 1957 | 1980 | Launched Pioneer & Explorer probes | [35] | ||||
LGM-25C Titan I-II-III-IV | 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 | [114] [115] | ||||
R-36 Tsyklon | Yuzhmash | 4,100 | -- | -- | -- | 259 | Retired | 1967 | 2009 | Var.: 1, 2, 3. | [116] | ||||
Unified Launch Vehicle | ISRO | 41,300 | 16,300 | -- | -- | 0 | Devel. | Var.: 6S12, 2S60, 2S138, 2S200 | [117] | ||||||
Unha-3 | KCST | 200 | -- | -- | -- | 4 | 3 | 2 | Active | 2006 | Var.: Paektusan based on Taepodong-1 missile; Unha based on Taepodong-2 missile. | [118] [119] | |||
Vanguard | Martin | 23 | -- | -- | -- | 12 | 3 | Retired | 1957 | 1959 | [120] | ||||
Vega | Avio | 2,300 | -- | -- | 23 | 13 | 13 | 13 | 13 | Revis. | 2012 | Vega-C and Vega-E in development. | [121] | ||
VLM | CTA | 380 | -- | -- | -- | 0 | Devel. | 2019 | [122] | ||||||
Vulcan | ULA | 17,800–34,900 | 7,400–16,300 | -- | 99 | 0 | Devel. | 2021 | [123] [124] [125] [126] | ||||||
Zenit | Yuzhnoye | 13,740 | 6,160 | 4,098 | -- | 82 | 71 | 69 | Active | 1985 | Var.: 2, 2M (2SB, 2SLB), 3SL, 3SLB, 3SLBF | [127] |
This page is an incomplete list of orbital rocket engine data.
A number of different spacecraft have been used to carry cargo to and from space stations.
Delta IV is an expendable launch system in the Delta rocket family. The rocket's main components are designed by Boeing's Defense, Space & Security division and built in the United Launch Alliance (ULA) facility in Decatur, Alabama. Final assembly is completed at the launch site by ULA. The rocket was designed to launch payloads into orbit for the United States Air Force Evolved Expendable Launch Vehicle (EELV) program and for the commercial satellite business. The Delta IV is available in five versions: Medium, Medium+ (4,2), Medium+ (5,2), Medium+ (5,4), and Heavy, to cover a range of payload size and weight. The Delta IV was primarily designed to satisfy the needs of the U.S. military.
The Angara rocket family is a family of space-launch vehicles being developed by the Moscow-based Khrunichev State Research and Production Space Center. The rockets are to put between 3,800 and 24,500 kg into low Earth orbit and are intended, along with Soyuz-2 variants, to replace several existing launch vehicles.
Geosynchronous Satellite Launch Vehicle abbreviated as GSLV, is an expendable launch system operated by the Indian Space Research Organisation (ISRO). GSLV has been used in thirteen launches to date, since its first launch in 2001 to the most recent on December 19, 2018 carrying the GSAT-7A military communications satellite. Even though Geosynchronous Satellite Launch Vehicle Mark III shares the name it is an entirely different launcher.
The Indian Space Research Organisation is the space agency of the Government of India headquartered in the city of Bengaluru. Its vision is to "harness space technology for national development while pursuing space science research and planetary exploration."
The GSAT satellites are India's indigenously developed communications satellites, used for digital audio, data and video broadcasting. As of 5 December 2018, 20 GSAT satellites of ISRO have been launched out of which 14 satellites are currently in service.
Satish Dhawan Space Centre (SDSC) or Sriharikota Range (SHAR) is a rocket launch centre operated by Indian Space Research Organisation (ISRO). It is located in Sriharikota in Andhra Pradesh. Sriharikota Range was renamed in 2002 after ISRO's former chairman Satish Dhawan.
The Geosynchronous Satellite Launch Vehicle Mark III (GSLV-III), also referred to as the Launch Vehicle Mark 3 (LVM3) is a three-stage medium-lift launch vehicle developed by the Indian Space Research Organisation (ISRO). It is designed to launch satellites into geostationary orbit, and is intended as a launch vehicle for crewed missions under the Indian Human Spaceflight Programme. The GSLV-III has a higher payload capacity than the similarly named GSLV.
INSAT-4C was an Indian communications satellite which was lost in a launch failure in 2006. Had it reached orbit, it would have formed part of the Indian National Satellite System. Launched in 2007, it was intended to have operated in geostationary orbit at a longitude of 73.97° east. The INSAT-4CR satellite, launched in September 2007, replaced it.
A space tug is a type of spacecraft used to transfer spaceborne cargo from one orbit to another orbit with different energy characteristics. An example would be moving a spacecraft from a low Earth orbit (LEO) to a higher-energy orbit like a geostationary transfer orbit, a lunar transfer, or an escape trajectory.
GSAT-14 is an Indian communications satellite launched in January 2014. It replaced the GSAT-3 satellite, which was launched in 2004. GSAT-14 was launched by a Geosynchronous Satellite Launch Vehicle Mk.II, which incorporated an Indian-built cryogenic engine on the third stage.
IRNSS-1B is the second out of seven in the Indian Regional Navigation Satellite System (IRNSS) series of satellites after IRNSS-1A. The IRNSS constellation of satellites is slated to be launched to provide navigational services to the region. It was placed in geosynchronous orbit on 4 April 2014.
KVD-1 was an upper stage LOX/LH2 cryogenic engine developed by the Isayev Design Bureau of Russia in the early 1960s. It is a modified version of the RD-56, developed for a never-completed cryogenic upper stage of the N-1 super-heavy lift rocket, with the goal of enabling manned lunar missions by the USSR. The KVD-1 produces a thrust of 7.5 tonnes.
The Unified Launch Vehicle (ULV) is a development project by the Indian Space Research Organisation (ISRO) whose core objective is to design a modular architecture that could eventually replace the PSLV, GSLV Mk I/II and GSLV Mk III with a single family of launchers. The design may include a heavy-lift variant dubbed HLV, as well as super heavy-lift variant called SHLV with a cluster stage of five SCE-200 engines each replacing the main core stage SC-160 and as well as the two solid boosters.
A small-lift launch vehicle is a rocket orbital launch vehicle that is capable of lifting up to 2,000 kg (4,400 lb) of payload into low Earth orbit (LEO). The next larger category consists of medium-lift launch vehicles.
Russian officials have said they plan to discontinue Dnepr launches.
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 '
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