Agency Instance
API endpoint that allows Agencies to be viewed.
GET:
Return a list of all the existing users.
MODE:
Normal and Detailed
/2.0.0/agencies/?mode=detailed
FILTERS:
Parameters - 'featured', 'agency_type', 'country_code'
Example - /2.0.0/agencies/?featured=true
SEARCH EXAMPLE:
/2.0.0/agencies/?search=nasa
ORDERING:
Fields - 'id', 'name', 'featured'
Example - /2.0.0/agencies/?ordering=featured
GET /2.0.0/agencies/111/?format=api
{ "id": 111, "url": "https://ll.thespacedevs.com/2.0.0/agencies/111/?format=api", "name": "Progress Rocket Space Center", "featured": false, "type": "Commercial", "country_code": "RUS", "abbrev": "PRSC", "description": "Progress Rocket Space Centre, formerly known as TsSKB-Progress, is a space science and aerospace research company which is known for manufacturing launch vehicles and satellites. Most notably, Progress Rocket Space Centre is the manufacturer of Soyuz launch vehicles.", "administrator": "Dmitry Baranov", "founding_year": "1996", "launchers": "", "spacecraft": "", "parent": null, "launch_library_url": null, "total_launch_count": 45, "successful_launches": 44, "consecutive_successful_launches": 3, "failed_launches": 1, "pending_launches": 0, "successful_landings": 0, "failed_landings": 0, "attempted_landings": 0, "consecutive_successful_landings": 0, "info_url": "https://en.samspace.ru/", "wiki_url": "https://en.wikipedia.org/wiki/Progress_Rocket_Space_Centre", "logo_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/progress2520rocket2520space2520center_logo_20210313175054.png", "image_url": null, "nation_url": null, "launcher_list": [ { "id": 335, "launch_library_id": null, "url": "https://ll.thespacedevs.com/2.0.0/config/launcher/335/?format=api", "name": "Molniya 8K78M-PVB", "description": "A Russian orbital launch vehicle. Version of Molniya 8k78M with safety modifications to prevent and resist fires in all stages and the avionics compartment.", "family": "R-7", "full_name": "Molniya 8K78M-PVB", "variant": "8K78M-PVB", "alias": "", "min_stage": 3, "max_stage": 3, "length": null, "diameter": null, "maiden_flight": "1990-04-28", "launch_mass": null, "leo_capacity": null, "gto_capacity": null, "to_thrust": null, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": "", "wiki_url": "https://en.wikipedia.org/wiki/Molniya-M", "consecutive_successful_launches": 8, "successful_launches": 8, "failed_launches": 0, "pending_launches": 0 }, { "id": 34, "launch_library_id": 36, "url": "https://ll.thespacedevs.com/2.0.0/config/launcher/34/?format=api", "name": "Soyuz", "description": "The Soyuz FG rocket is an expendable launch vehicle most commonly known for carrying humans to the International Space Station today.", "family": "", "full_name": "Soyuz FG", "variant": "FG", "alias": "", "min_stage": 2, "max_stage": 2, "length": 49.5, "diameter": 3.0, "maiden_flight": "2001-05-20", "launch_mass": 305, "leo_capacity": 6450, "gto_capacity": null, "to_thrust": null, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/soyuz_image_20190717035537.jpg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Soyuz-FG", "consecutive_successful_launches": 5, "successful_launches": 59, "failed_launches": 1, "pending_launches": 0 }, { "id": 24, "launch_library_id": 49, "url": "https://ll.thespacedevs.com/2.0.0/config/launcher/24/?format=api", "name": "Soyuz 2.1a", "description": "The Soyuz 2.1A converted the flight control system from analog to digital, which allowed launch from fixed platforms. It also allowed big fairings and payloads.\r\nIt is currently used for crewed Soyuz and Progress flights to the ISS.", "family": "Soyuz", "full_name": "Soyuz 2.1a", "variant": "", "alias": "", "min_stage": 2, "max_stage": 3, "length": 46.3, "diameter": 2.95, "maiden_flight": "2004-11-04", "launch_mass": 312, "leo_capacity": 7020, "gto_capacity": 2810, "to_thrust": 4149, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/soyuz_2.1a_image_20230805184309.jpg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Soyuz-2#Soyuz-2.1a", "consecutive_successful_launches": 37, "successful_launches": 43, "failed_launches": 1, "pending_launches": 5 }, { "id": 212, "launch_library_id": 235, "url": "https://ll.thespacedevs.com/2.0.0/config/launcher/212/?format=api", "name": "Soyuz 2.1a/Fregat", "description": "", "family": "Soyuz", "full_name": "Soyuz 2.1a Fregat", "variant": "Fregat", "alias": "", "min_stage": null, "max_stage": null, "length": null, "diameter": null, "maiden_flight": "2006-10-19", "launch_mass": null, "leo_capacity": null, "gto_capacity": null, "to_thrust": null, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": null, "consecutive_successful_launches": 0, "successful_launches": 2, "failed_launches": 1, "pending_launches": 0 }, { "id": 45, "launch_library_id": 83, "url": "https://ll.thespacedevs.com/2.0.0/config/launcher/45/?format=api", "name": "Soyuz 2.1a/Fregat-M", "description": "The 2.1a version includes conversion from analog to digital flight control system and uprated engines on the booster and the first stage with improved injection systems. The new digital flight control and telemetry systems allow the rocket to launch from a fixed rather than angled launch platform and adjust its heading in flight. A digital control system also enables the launch of larger commercial satellites with wider and longer payload fairings such as the ST-type fairing. These fairings introduce too much aerodynamic instability for the old analog system to handle.", "family": "Soyuz", "full_name": "Soyuz 2.1a Fregat-M", "variant": "Fregat-M", "alias": "", "min_stage": 3, "max_stage": 3, "length": 46.3, "diameter": 2.95, "maiden_flight": "2010-10-19", "launch_mass": 312, "leo_capacity": 7020, "gto_capacity": null, "to_thrust": 4149, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/soyuz25202.1a_image_20190726062341.png", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Soyuz-2", "consecutive_successful_launches": 8, "successful_launches": 17, "failed_launches": 1, "pending_launches": 1 }, { "id": 57, "launch_library_id": 66, "url": "https://ll.thespacedevs.com/2.0.0/config/launcher/57/?format=api", "name": "Soyuz 2.1a/Volga", "description": "In addition to the switch to digital flight control systems as part of the Soyuz 2.1A, this version utilizes the Volga upper stage.", "family": "Soyuz", "full_name": "Soyuz 2.1a Volga", "variant": "Volga", "alias": "", "min_stage": 2, "max_stage": 3, "length": 19.6, "diameter": 2.68, "maiden_flight": "2004-11-08", "launch_mass": null, "leo_capacity": null, "gto_capacity": null, "to_thrust": 4149, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Soyuz-2", "consecutive_successful_launches": 1, "successful_launches": 1, "failed_launches": 0, "pending_launches": 0 }, { "id": 15, "launch_library_id": 3, "url": "https://ll.thespacedevs.com/2.0.0/config/launcher/15/?format=api", "name": "Soyuz 2.1b", "description": "Soyuz-2 is the 21st-century version of the Russian Soyuz rocket. In its basic form, it is a three-stage carrier rocket for placing payloads into low Earth orbit. The 2.1b version adds an upgraded engine (RD-0124) with improved performance to the second stage.", "family": "Soyuz", "full_name": "Soyuz 2.1b", "variant": "", "alias": "", "min_stage": 2, "max_stage": 3, "length": 46.3, "diameter": 2.95, "maiden_flight": "2008-07-26", "launch_mass": 312, "leo_capacity": 8200, "gto_capacity": 3250, "to_thrust": null, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/soyuz_2.1b_image_20230802085331.jpg", "info_url": null, "wiki_url": "http://en.wikipedia.org/wiki/Soyuz-2_(rocket)", "consecutive_successful_launches": 19, "successful_launches": 19, "failed_launches": 0, "pending_launches": 0 }, { "id": 42, "launch_library_id": 65, "url": "https://ll.thespacedevs.com/2.0.0/config/launcher/42/?format=api", "name": "Soyuz 2.1b/Fregat", "description": "Soyuz-2, GRAU index 14A14, is the collective designation for the 21st-century version of the Russian Soyuz rocket. In its basic form, it is a three-stage carrier rocket for placing payloads into low Earth orbit. The first-stage boosters and two core stages feature uprated engines with improved injection systems, compared to the previous versions of the Soyuz. Digital flight control and telemetry systems allow the rocket to be launched from a fixed launch platform, whereas the launch platforms for earlier Soyuz rockets had to be rotated as the rocket could not perform a roll to change its heading in flight.\r\n\r\nThe Soyuz 2.1b represents the latest development stage of the proven rocket.\r\n\r\nIt uses the new RD-0124 engines in the first three stages, coupled with an improved injection system that significantly boosts the performance of the Soyuz.\r\nFurthermore, she wears a new, digital startup control system.\r\nThis will allow the Soyuz 2.1b to carry around 1.2 tonnes more payload into low earth orbit compared to its predecessor.", "family": "Soyuz", "full_name": "Soyuz 2.1b Fregat", "variant": "Fregat", "alias": "", "min_stage": 3, "max_stage": 4, "length": 46.3, "diameter": 2.95, "maiden_flight": "2006-12-27", "launch_mass": 312, "leo_capacity": 8200, "gto_capacity": 3250, "to_thrust": 4150, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/soyuz_2.1b_image_20230802085331.jpg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Soyuz-2", "consecutive_successful_launches": 8, "successful_launches": 22, "failed_launches": 2, "pending_launches": 2 }, { "id": 134, "launch_library_id": 153, "url": "https://ll.thespacedevs.com/2.0.0/config/launcher/134/?format=api", "name": "Soyuz 2.1b/Fregat-M", "description": "Soyuz-2, GRAU index 14A14, is the collective designation for the 21st-century version of the Russian Soyuz rocket. In its basic form, it is a three-stage carrier rocket for placing payloads into low Earth orbit. The first-stage boosters and two core stages feature uprated engines with improved injection systems, compared to the previous versions of the Soyuz. Digital flight control and telemetry systems allow the rocket to be launched from a fixed launch platform, whereas the launch platforms for earlier Soyuz rockets had to be rotated as the rocket could not perform a roll to change its heading in flight.", "family": "Soyuz", "full_name": "Soyuz 2.1b Fregat-M", "variant": "Fregat-M", "alias": "", "min_stage": 4, "max_stage": 4, "length": 46.3, "diameter": 10.3, "maiden_flight": "2008-07-26", "launch_mass": 313, "leo_capacity": 8200, "gto_capacity": 3250, "to_thrust": 4150, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/soyuz_2.1b_image_20230802085331.jpg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Soyuz-2", "consecutive_successful_launches": 28, "successful_launches": 28, "failed_launches": 0, "pending_launches": 4 }, { "id": 60, "launch_library_id": 61, "url": "https://ll.thespacedevs.com/2.0.0/config/launcher/60/?format=api", "name": "Soyuz 2-1v", "description": "The Soyuz-2-1v is a Russian expendable carrier rocket. It was derived from the Soyuz-2.1b, and is a member of the R-7 family of rockets.", "family": "Soyuz", "full_name": "Soyuz 2-1v Volga", "variant": "Volga", "alias": "", "min_stage": 2, "max_stage": 2, "length": 44.0, "diameter": 3.0, "maiden_flight": "2013-12-28", "launch_mass": 158, "leo_capacity": 2850, "gto_capacity": null, "to_thrust": null, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/soyuz25202-1v_image_20191122081651.jpg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Soyuz-2-1v", "consecutive_successful_launches": 6, "successful_launches": 7, "failed_launches": 1, "pending_launches": 0 }, { "id": 70, "launch_library_id": 102, "url": "https://ll.thespacedevs.com/2.0.0/config/launcher/70/?format=api", "name": "Soyuz-FG", "description": "The Soyuz FG is a medium-lift launch vehicle qualified for manned launches and used to deliver Soyuz Spacecraft to Orbit for Missions to the International Space Station.", "family": "", "full_name": "Soyuz-FG Fregat", "variant": "Fregat", "alias": "", "min_stage": 3, "max_stage": 3, "length": 4.95, "diameter": 2.68, "maiden_flight": "2003-06-02", "launch_mass": 305, "leo_capacity": 7100, "gto_capacity": null, "to_thrust": null, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/soyuz_image_20190717035842.jpeg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Soyuz-FG", "consecutive_successful_launches": 10, "successful_launches": 10, "failed_launches": 0, "pending_launches": 0 }, { "id": 49, "launch_library_id": 76, "url": "https://ll.thespacedevs.com/2.0.0/config/launcher/49/?format=api", "name": "Soyuz STA", "description": "The 2.1a version includes conversion from analog to digital flight control system and uprated engines on the booster and the first stage with improved injection systems. The new digital flight control and telemetry systems allow the rocket to launch from a fixed rather than angled launch platform and adjust its heading in flight. A digital control system also enables the launch of larger commercial satellites with wider and longer payload fairings such as the ST-type fairing. These fairings introduce too much aerodynamic instability for the old analog system to handle. This stage continues to use the RD-0110 engine.\r\n\r\nThe 2.1a/ST version is sometimes called Soyuz ST-A.", "family": "Soyuz", "full_name": "Soyuz STA Fregat", "variant": "Fregat", "alias": "", "min_stage": 3, "max_stage": 3, "length": 46.3, "diameter": 2.95, "maiden_flight": "2011-12-17", "launch_mass": 312, "leo_capacity": 7020, "gto_capacity": 2810, "to_thrust": null, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/soyuz2520sta_image_20191210133244.jpg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Soyuz-2_(rocket)", "consecutive_successful_launches": 8, "successful_launches": 8, "failed_launches": 0, "pending_launches": 0 }, { "id": 72, "launch_library_id": 96, "url": "https://ll.thespacedevs.com/2.0.0/config/launcher/72/?format=api", "name": "Soyuz STB", "description": "The 2.1b version adds an upgraded engine (RD-0124) with improved performance to the second stage. First launch took place from Plesetsk Cosmodrome Site 43 on 26 July 2008 with a classified military payload.\r\n\r\nThe 2.1b/ST version is sometimes called Soyuz ST-B.", "family": "Soyuz", "full_name": "Soyuz STB Fregat-MT", "variant": "Fregat-MT", "alias": "", "min_stage": 3, "max_stage": 3, "length": 46.3, "diameter": 2.95, "maiden_flight": "2012-10-12", "launch_mass": 310, "leo_capacity": 8200, "gto_capacity": 3250, "to_thrust": null, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/soyuz2520stb_image_20191201201634.jpg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Soyuz-2#Soyuz-2.1b", "consecutive_successful_launches": 5, "successful_launches": 5, "failed_launches": 0, "pending_launches": 0 }, { "id": 171, "launch_library_id": 52, "url": "https://ll.thespacedevs.com/2.0.0/config/launcher/171/?format=api", "name": "Soyuz STB", "description": "The 2.1b version adds an upgraded engine (RD-0124) with improved performance to the second stage. First launch took place from Plesetsk Cosmodrome Site 43 on 26 July 2008 with a classified military payload.\r\n\r\nThe 2.1b/ST version is sometimes called Soyuz ST-B.", "family": "Soyuz", "full_name": "Soyuz STB Fregat", "variant": "STB/Fregat", "alias": "", "min_stage": 3, "max_stage": 3, "length": 46.3, "diameter": 2.95, "maiden_flight": "2011-10-21", "launch_mass": 312, "leo_capacity": 8200, "gto_capacity": 3250, "to_thrust": null, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/soyuz_stb_image_20211130181029.jpeg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Soyuz-2_(rocket)", "consecutive_successful_launches": 11, "successful_launches": 13, "failed_launches": 1, "pending_launches": 0 }, { "id": 378, "launch_library_id": null, "url": "https://ll.thespacedevs.com/2.0.0/config/launcher/378/?format=api", "name": "Soyuz-U-PVB", "description": "A Russian orbital launch vehicle. A version of the Soyuz-U with safety modifications to prevent and resist fires in all stages and the upper stage avionics compartment.", "family": "Soyuz", "full_name": "Soyuz-U-PVB", "variant": "U-PVB", "alias": "", "min_stage": 2, "max_stage": 2, "length": 51.0, "diameter": 3.0, "maiden_flight": "1984-03-21", "launch_mass": 313, "leo_capacity": 6900, "gto_capacity": null, "to_thrust": null, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": "", "wiki_url": "https://en.wikipedia.org/wiki/Soyuz-U", "consecutive_successful_launches": 12, "successful_launches": 72, "failed_launches": 2, "pending_launches": 0 } ], "spacecraft_list": [] }
