Agency Instance
API endpoint that allows Agencies to be viewed.
GET:
Return a list of all the existing users.
MODE:
Normal and Detailed
/2.2.0/agencies/?mode=detailed
FILTERS:
Parameters - 'featured', 'agency_type', 'country_code'
Example - /2.2.0/agencies/?featured=true
SEARCH EXAMPLE:
/2.2.0/agencies/?search=nasa
ORDERING:
Fields - 'id', 'name', 'featured'
Example - /2.2.0/agencies/?ordering=featured
The 'country_code' field is a string of comma separated ISO 3166 alpha-3 codes.
GET /2.2.0/agencies/98/?format=api
{ "id": 98, "url": "https://ll.thespacedevs.com/2.2.0/agencies/98/?format=api", "name": "Mitsubishi Heavy Industries", "featured": false, "type": "Commercial", "country_code": "JPN", "abbrev": "MHI", "description": "Mitsubishi Heavy Industries, Ltd. is a Japanese multinational engineering, electrical equipment and electronics company headquartered in Tokyo, Japan. MHI is one of the core companies of the Mitsubishi Group.\r\n\r\nMHI's products include aerospace components, air conditioners, aircraft, automotive components, forklift trucks, hydraulic equipment, machine tools, missiles, power generation equipment, printing machines, ships and space launch vehicles. Through its defense-related activities, it is the world's 23rd-largest defense contractor measured by 2011 defense revenues and the largest based in Japan.", "administrator": "President: Seiji Izumisawa", "founding_year": "1884", "launchers": "H-I, H-II, H-III", "spacecraft": "Kounotori | HTV", "parent": null, "launch_library_url": null, "total_launch_count": 50, "successful_launches": 49, "consecutive_successful_launches": 2, "failed_launches": 1, "pending_launches": 13, "successful_landings": 0, "failed_landings": 0, "attempted_landings": 0, "consecutive_successful_landings": 0, "info_url": "https://www.mhi.com/", "wiki_url": "http://en.wikipedia.org/wiki/Mitsubishi_Heavy_Industries", "logo_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/mitsubishi2520heavy2520industries_logo_20200117065724.png", "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/mitsubishi2520heavy2520industries_image_20200117065724.jpg", "nation_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/mitsubishi2520heavy2520industries_nation_20240112111043.jpg", "launcher_list": [ { "id": 319, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/319/?format=api", "name": "H-1", "description": "The H-1 was a Japanese liquid-fuelled carrier rocket, consisting of a license-produced American First Stage and set of booster rockets and all-Japanese upper stages. It replaced the N-II and was subsequently replaced by the H-2 which has the same upper stages with a Japaense first stage.", "family": "H-I", "full_name": "H-I", "variant": "I", "alias": "", "min_stage": 2, "max_stage": 3, "length": 42.0, "diameter": 2.44, "maiden_flight": "1986-08-12", "launch_mass": 142, "leo_capacity": 3200, "gto_capacity": 1100, "to_thrust": null, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/h-1_image_20240210175424.png", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/H-I", "consecutive_successful_launches": 9, "successful_launches": 9, "failed_launches": 0, "pending_launches": 0 }, { "id": 30, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/30/?format=api", "name": "H3", "description": "The H3 Launch Vehicle is an expendable launch system in development in Japan. H3 rockets are liquid-propellant rockets with strap-on solid rocket boosters and are planned to be launched from the Tanegashima Space Center in Japan. Mitsubishi and the JAXA have been responsible for the design, manufacture, and operation of the H3.", "family": "H3", "full_name": "H3", "variant": "", "alias": "", "min_stage": 2, "max_stage": 2, "length": 63.0, "diameter": 5.27, "maiden_flight": null, "launch_mass": 574, "leo_capacity": null, "gto_capacity": 6500, "to_thrust": null, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/h-iii_image_20221104084531.jpeg", "info_url": "http://global.jaxa.jp/press/2015/07/20150702_h3.html", "wiki_url": "https://en.wikipedia.org/wiki/H3_(rocket)", "consecutive_successful_launches": 0, "successful_launches": 0, "failed_launches": 0, "pending_launches": 1 }, { "id": 486, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/486/?format=api", "name": "H3-22", "description": "The H3 Launch Vehicle is a Japanese expendable launch system.\r\nEach H3 booster configuration has a two-digit and a letter designation that indicates the features of that configuration. The first digit represents the number of LE-9 engines on the main stage, either \"2\" or \"3\". The second digit indicates the number of SRB-3 solid rocket boosters attached to the base of the rocket, and can be \"0\", \"2\" or \"4\". All layouts of solid boosters are symmetrical. The letter in the end shows the length of the payload fairing, either short \"S\" or long \"L\". For example, an H3-24L has two engines, four solid rocket boosters, and a long fairing, whereas an H3-30S has three engines, no solid rocket boosters, and a short fairing.", "family": "H3", "full_name": "H3-22", "variant": "22", "alias": "", "min_stage": 2, "max_stage": 2, "length": 63.0, "diameter": 5.27, "maiden_flight": "2023-03-07", "launch_mass": null, "leo_capacity": null, "gto_capacity": 4000, "to_thrust": 7542, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/h3-22_image_20230307130808.jpeg", "info_url": "http://global.jaxa.jp/press/2015/07/20150702_h3.html", "wiki_url": "https://en.wikipedia.org/wiki/H3_(rocket)", "consecutive_successful_launches": 1, "successful_launches": 1, "failed_launches": 1, "pending_launches": 6 }, { "id": 204, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/204/?format=api", "name": "H3-24", "description": "The H3 Launch Vehicle is an expendable launch system in development in Japan.\r\nEach H3 booster configuration has a two-digit and a letter designation that indicates the features of that configuration. The first digit represents the number of LE-9 engines on the main stage, either \"2\" or \"3\". The second digit indicates the number of SRB-3 solid rocket boosters attached to the base of the rocket, and can be \"0\", \"2\" or \"4\". All layouts of solid boosters are symmetrical. The letter in the end shows the length of the payload fairing, either short \"S\" or long \"L\". For example, an H3-24L has two engines, four solid rocket boosters, and a long fairing, whereas an H3-30S has three engines, no solid rocket boosters, and a short fairing.", "family": "H3", "full_name": "H3-24", "variant": "24", "alias": "", "min_stage": 2, "max_stage": 2, "length": 63.0, "diameter": 5.27, "maiden_flight": null, "launch_mass": null, "leo_capacity": null, "gto_capacity": 6500, "to_thrust": 12142, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/h-iii_image_20221104084531.jpeg", "info_url": "http://global.jaxa.jp/press/2015/07/20150702_h3.html", "wiki_url": "https://en.wikipedia.org/wiki/H3_(rocket)", "consecutive_successful_launches": 0, "successful_launches": 0, "failed_launches": 0, "pending_launches": 5 }, { "id": 203, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/203/?format=api", "name": "H3-30", "description": "The H3 Launch Vehicle is an expendable launch system in development in Japan. H3 rockets are liquid-propellant rockets with strap-on solid rocket boosters and are planned to be launched from the Tanegashima Space Center in Japan. Mitsubishi and the JAXA have been responsible for the design, manufacture, and operation of the H3.", "family": "H3", "full_name": "H3-30", "variant": "30", "alias": "", "min_stage": 2, "max_stage": 2, "length": 63.0, "diameter": 5.27, "maiden_flight": null, "launch_mass": 274, "leo_capacity": null, "gto_capacity": 2100, "to_thrust": 4413, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/h-iii_image_20221104084531.jpeg", "info_url": "http://global.jaxa.jp/press/2015/07/20150702_h3.html", "wiki_url": "https://en.wikipedia.org/wiki/H3_(rocket)", "consecutive_successful_launches": 0, "successful_launches": 0, "failed_launches": 0, "pending_launches": 0 }, { "id": 320, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/320/?format=api", "name": "H-II", "description": "The H-II rocket was a Japanese satellite launch system which flew seven times between 1994 and 1999 with 5 successes. It was developed by NASDA in order to give Japan a capability to launch larger satellites in the 1990s. It was the first two stage liquid fuelled rocket Japan made using only domestic technologies.", "family": "H-II", "full_name": "H-II", "variant": "", "alias": "", "min_stage": 2, "max_stage": 2, "length": 49.0, "diameter": 4.0, "maiden_flight": "1994-02-03", "launch_mass": 260, "leo_capacity": 10060, "gto_capacity": 3930, "to_thrust": null, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/H-II", "consecutive_successful_launches": 0, "successful_launches": 6, "failed_launches": 1, "pending_launches": 0 }, { "id": 32, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/32/?format=api", "name": "H-IIA", "description": "H-IIA (H2A) is an active expendable launch system operated by Mitsubishi Heavy Industries (MHI) for the Japan Aerospace Exploration Agency. The liquid-fueled H-IIA rockets have been used to launch satellites into geostationary orbit, to launch a lunar orbiting spacecraft, and to launch Akatsuki, which studied the planet Venus. Launches occur at the Tanegashima Space Center.", "family": "H-II", "full_name": "H-IIA 202", "variant": "202", "alias": "", "min_stage": 2, "max_stage": 2, "length": 53.0, "diameter": 4.0, "maiden_flight": "2001-08-29", "launch_mass": 285, "leo_capacity": 10000, "gto_capacity": 4100, "to_thrust": 2260, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/h-iia_202_lifto_image_20240325123250.jpg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/H-IIA", "consecutive_successful_launches": 33, "successful_launches": 33, "failed_launches": 0, "pending_launches": 2 }, { "id": 321, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/321/?format=api", "name": "H-IIA", "description": "The H-IIA rocket family is an expendable launch system operated by Mitsubishi Heavy Industries for the Japan Aerospace Exploration Agency. The liquid fuelled rocket has been used to launch satellites, lunar spacecraft and planetary science craft.", "family": "H-II", "full_name": "H-IIA 2022", "variant": "2022", "alias": "", "min_stage": 2, "max_stage": 2, "length": 53.0, "diameter": 4.0, "maiden_flight": "2005-02-26", "launch_mass": 316, "leo_capacity": null, "gto_capacity": 4500, "to_thrust": null, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/h-ii_2022_lifto_image_20240411175401.png", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/H-IIA", "consecutive_successful_launches": 3, "successful_launches": 3, "failed_launches": 0, "pending_launches": 0 }, { "id": 48, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/48/?format=api", "name": "H-IIA", "description": "H-IIA (H2A) was an expendable launch system operated by Mitsubishi Heavy Industries (MHI) for the Japan Aerospace Exploration Agency. The liquid-fueled H-IIA rockets have been used to launch satellites into geostationary orbit, to launch a lunar orbiting spacecraft, and to launch Akatsuki, which studied the planet Venus. Launches occur at the Tanegashima Space Center.", "family": "H-II", "full_name": "H-IIA 204", "variant": "204", "alias": "", "min_stage": 2, "max_stage": 2, "length": 53.0, "diameter": 4.0, "maiden_flight": "2006-12-18", "launch_mass": 445, "leo_capacity": null, "gto_capacity": 6000, "to_thrust": 2260, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/h-iia_204_lifto_image_20240325124231.jpg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/H-IIA", "consecutive_successful_launches": 5, "successful_launches": 5, "failed_launches": 0, "pending_launches": 0 }, { "id": 322, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/322/?format=api", "name": "H-IIA", "description": "The H-IIA rocket family is an expendable launch system operated by Mitsubishi Heavy Industries for the Japan Aerospace Exploration Agency. The liquid fuelled rocket has been used to launch satellites, lunar spacecraft and planetary science craft.", "family": "H-II", "full_name": "H-IIA 2024", "variant": "2024", "alias": "", "min_stage": 2, "max_stage": 2, "length": 53.0, "diameter": 4.0, "maiden_flight": "2002-02-04", "launch_mass": 347, "leo_capacity": null, "gto_capacity": 5000, "to_thrust": null, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/h-iia_2024_lift_image_20240411181830.png", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/H-IIA", "consecutive_successful_launches": 3, "successful_launches": 6, "failed_launches": 1, "pending_launches": 0 }, { "id": 77, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/77/?format=api", "name": "H-IIB", "description": "H-IIB (H2B) is an expendable launch system used to launch H-II Transfer Vehicles (HTV, or Kounotori) towards the International Space Station. H-IIB rockets are liquid-fuelled with solid-fuel strap-on boosters and are launched from the Tanegashima Space Center in Japan. Mitsubishi and JAXA have been primarily responsible for design, manufacture, and operation of H-IIB.", "family": "H2B", "full_name": "H-IIB 304", "variant": "304", "alias": "", "min_stage": 0, "max_stage": 2, "length": 56.6, "diameter": 5.2, "maiden_flight": "2009-09-10", "launch_mass": 551, "leo_capacity": 16500, "gto_capacity": 8000, "to_thrust": 9000, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/h-iib_304_lifto_image_20240325125154.jpg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/H-IIB", "consecutive_successful_launches": 9, "successful_launches": 9, "failed_launches": 0, "pending_launches": 0 }, { "id": 341, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/341/?format=api", "name": "N-2", "description": "The N-II or N-2 was a derivative of the American Delta rocket, produced under licence in Japan. It replaced the N-I-rocket in Japanese use. It used a Thor-ELT first stage, a Delta-F second stage, nine Castor SRMs, and on most flights either a Star-37E or Burner-2 upper stage, identical to the US Delta 0100 series configurations. Eight were launched between 1981 and 1987, before it was replaced by the H-I, which featured Japanese-produced upper stages. All eight launches were successful.", "family": "", "full_name": "N-2", "variant": "2", "alias": "", "min_stage": 2, "max_stage": 3, "length": 35.0, "diameter": 2.44, "maiden_flight": "1981-02-11", "launch_mass": 132, "leo_capacity": 2000, "gto_capacity": 730, "to_thrust": 2278, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": "", "wiki_url": "https://en.wikipedia.org/wiki/N-II_(rocket)", "consecutive_successful_launches": 8, "successful_launches": 8, "failed_launches": 0, "pending_launches": 0 }, { "id": 459, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/459/?format=api", "name": "N-I", "description": "The N-I or N-1 was a derivative of the American Thor-Delta rocket, produced under licence in Japan. It used a Thor-ELT first stage, a Mitsubishi Heavy Industries-designed LE-3 engine was used as a second stage, and three Castor SRMs. Seven were launched between 1975 and 1982, before it was replaced by the N-II.", "family": "", "full_name": "N-I", "variant": "", "alias": "", "min_stage": 2, "max_stage": 3, "length": 34.0, "diameter": 2.44, "maiden_flight": "1975-09-09", "launch_mass": 131, "leo_capacity": 1200, "gto_capacity": 360, "to_thrust": null, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/N-I_(rocket)", "consecutive_successful_launches": 2, "successful_launches": 6, "failed_launches": 1, "pending_launches": 0 } ], "spacecraft_list": [] }
