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/153/?format=api
{ "id": 153, "url": "https://ll.thespacedevs.com/2.2.0/agencies/153/?format=api", "name": "McDonnell Douglas", "featured": false, "type": "Commercial", "country_code": "USA", "abbrev": "MDC", "description": null, "administrator": null, "founding_year": null, "launchers": "", "spacecraft": "", "parent": null, "launch_library_url": null, "total_launch_count": 0, "successful_launches": 0, "consecutive_successful_launches": 0, "failed_launches": 0, "pending_launches": 0, "successful_landings": 0, "failed_landings": 0, "attempted_landings": 0, "consecutive_successful_landings": 0, "info_url": null, "wiki_url": "http://en.wikipedia.org/wiki/McDonnell_Douglas", "logo_url": null, "image_url": null, "nation_url": null, "launcher_list": [ { "id": 275, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/275/?format=api", "name": "Delta 0300", "description": "The Delta 0100 series, also Delta 100, 0300 or 300 series, was an American expendable launch system which conducted orbital launches between 1968 and 1972. It was a member of the Delta family of rockets, and the first to be designated using a four digit numerical code. Two variants were flown, individually designated Delta 0300 and Delta 0900.", "family": "Delta", "full_name": "Delta 0300", "variant": "0300", "alias": "", "min_stage": 3, "max_stage": 3, "length": 34.0, "diameter": 2.44, "maiden_flight": "1972-10-15", "launch_mass": 90, "leo_capacity": null, "gto_capacity": null, "to_thrust": 1590, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_0100", "consecutive_successful_launches": 1, "successful_launches": 2, "failed_launches": 1, "pending_launches": 0 }, { "id": 276, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/276/?format=api", "name": "Delta 0900", "description": "The Delta 0100 series, also Delta 100, 0300 or 300 series, was an American expendable launch system which conducted orbital launches between 1968 and 1972. It was a member of the Delta family of rockets, and the first to be designated using a four digit numerical code. Two variants were flown, individually designated Delta 0300 and Delta 0900.", "family": "Delta", "full_name": "Delta 0900", "variant": "0900", "alias": "", "min_stage": 3, "max_stage": 3, "length": 34.0, "diameter": 2.44, "maiden_flight": "1972-07-23", "launch_mass": 116, "leo_capacity": 1300, "gto_capacity": null, "to_thrust": 2500, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/delta_0900_image_20231231081129.jpg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_0100", "consecutive_successful_launches": 2, "successful_launches": 2, "failed_launches": 0, "pending_launches": 0 }, { "id": 277, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/277/?format=api", "name": "Delta 1410", "description": "The Delta 1000 series (also referred to as Straight-Eight) was an American expendable launch system which was used to conduct eight orbital launches between 1972 and 1975. It was a member of the Delta family of rockets. Several variants existed, differentiated by a four digit numerical code.", "family": "Delta", "full_name": "Delta 1410", "variant": "1410", "alias": "", "min_stage": 3, "max_stage": 3, "length": 35.0, "diameter": 2.44, "maiden_flight": "1975-04-09", "launch_mass": 110, "leo_capacity": null, "gto_capacity": null, "to_thrust": 1863, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_1000", "consecutive_successful_launches": 1, "successful_launches": 1, "failed_launches": 0, "pending_launches": 0 }, { "id": 278, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/278/?format=api", "name": "Delta 1604", "description": "The Delta 1000 series (also referred to as Straight-Eight) was an American expendable launch system which was used to conduct eight orbital launches between 1972 and 1975. It was a member of the Delta family of rockets. Several variants existed, differentiated by a four digit numerical code.", "family": "Delta", "full_name": "Delta 1604", "variant": "1604", "alias": "", "min_stage": 4, "max_stage": 4, "length": 35.0, "diameter": 2.44, "maiden_flight": "1972-09-23", "launch_mass": 118, "leo_capacity": 600, "gto_capacity": null, "to_thrust": null, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_1000", "consecutive_successful_launches": 2, "successful_launches": 2, "failed_launches": 0, "pending_launches": 0 }, { "id": 279, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/279/?format=api", "name": "Delta 1900", "description": "The Delta 1000 series (also referred to as Straight-Eight) was an American expendable launch system which was used to conduct eight orbital launches between 1972 and 1975. It was a member of the Delta family of rockets. Several variants existed, differentiated by a four digit numerical code.", "family": "Delta", "full_name": "Delta 1900", "variant": "1900", "alias": "", "min_stage": 3, "max_stage": 3, "length": 35.0, "diameter": 2.44, "maiden_flight": "1973-12-16", "launch_mass": 130, "leo_capacity": null, "gto_capacity": null, "to_thrust": 2410, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_1000", "consecutive_successful_launches": 1, "successful_launches": 1, "failed_launches": 0, "pending_launches": 0 }, { "id": 280, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/280/?format=api", "name": "Delta 1910", "description": "The Delta 1000 series (also referred to as Straight-Eight) was an American expendable launch system which was used to conduct eight orbital launches between 1972 and 1975. It was a member of the Delta family of rockets. Several variants existed, differentiated by a four digit numerical code.", "family": "Delta", "full_name": "Delta 1910", "variant": "1910", "alias": "", "min_stage": 3, "max_stage": 3, "length": 35.0, "diameter": 2.44, "maiden_flight": "1975-06-21", "launch_mass": 130, "leo_capacity": null, "gto_capacity": null, "to_thrust": 2410, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_1000", "consecutive_successful_launches": 1, "successful_launches": 1, "failed_launches": 0, "pending_launches": 0 }, { "id": 281, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/281/?format=api", "name": "Delta 1913", "description": "The Delta 1000 series (also referred to as Straight-Eight) was an American expendable launch system which was used to conduct eight orbital launches between 1972 and 1975. It was a member of the Delta family of rockets. Several variants existed, differentiated by a four digit numerical code.", "family": "Delta", "full_name": "Delta 1913", "variant": "1913", "alias": "", "min_stage": 4, "max_stage": 4, "length": 35.0, "diameter": 2.44, "maiden_flight": "1973-06-10", "launch_mass": 130, "leo_capacity": null, "gto_capacity": null, "to_thrust": 2410, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_1000", "consecutive_successful_launches": 1, "successful_launches": 1, "failed_launches": 0, "pending_launches": 0 }, { "id": 282, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/282/?format=api", "name": "Delta 1914", "description": "The Delta 1000 series (also referred to as Straight-Eight) was an American expendable launch system which was used to conduct eight orbital launches between 1972 and 1975. It was a member of the Delta family of rockets. Several variants existed, differentiated by a four digit numerical code.", "family": "Delta", "full_name": "Delta 1914", "variant": "1914", "alias": "", "min_stage": 4, "max_stage": 4, "length": 35.0, "diameter": 2.44, "maiden_flight": "1972-11-10", "launch_mass": 130, "leo_capacity": null, "gto_capacity": null, "to_thrust": 2287, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_1000", "consecutive_successful_launches": 2, "successful_launches": 2, "failed_launches": 0, "pending_launches": 0 }, { "id": 283, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/283/?format=api", "name": "Delta 2310", "description": "The Delta 2000 series was an American expendable launch system which was used to conduct forty-four orbital launches between 1974 and 1981. It was a member of the Delta family of rockets. Several variants existed, which were differentiated by a four digit numerical code.", "family": "Delta", "full_name": "Delta 2310", "variant": "2310", "alias": "", "min_stage": 3, "max_stage": 3, "length": 35.0, "diameter": 2.44, "maiden_flight": "1974-11-15", "launch_mass": 131, "leo_capacity": null, "gto_capacity": null, "to_thrust": 1737, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_2000", "consecutive_successful_launches": 3, "successful_launches": 3, "failed_launches": 0, "pending_launches": 0 }, { "id": 284, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/284/?format=api", "name": "Delta 2313", "description": "The Delta 2000 series was an American expendable launch system which was used to conduct forty-four orbital launches between 1974 and 1981. It was a member of the Delta family of rockets. Several variants existed, which were differentiated by a four digit numerical code.", "family": "Delta", "full_name": "Delta 2313", "variant": "2313", "alias": "", "min_stage": 3, "max_stage": 3, "length": 35.0, "diameter": 2.44, "maiden_flight": "1974-01-19", "launch_mass": 131, "leo_capacity": 500, "gto_capacity": null, "to_thrust": 1737, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_2000", "consecutive_successful_launches": 2, "successful_launches": 2, "failed_launches": 1, "pending_launches": 0 }, { "id": 285, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/285/?format=api", "name": "Delta 2910", "description": "The Delta 2000 series was an American expendable launch system which was used to conduct forty-four orbital launches between 1974 and 1981. It was a member of the Delta family of rockets. Several variants existed, which were differentiated by a four digit numerical code.", "family": "Delta", "full_name": "Delta 2910", "variant": "2910", "alias": "", "min_stage": 3, "max_stage": 3, "length": 35.0, "diameter": 2.44, "maiden_flight": "1978-01-22", "launch_mass": 131, "leo_capacity": null, "gto_capacity": null, "to_thrust": 2560, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/delta_2910_image_20231231105214.jpeg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_2000", "consecutive_successful_launches": 6, "successful_launches": 6, "failed_launches": 0, "pending_launches": 0 }, { "id": 286, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/286/?format=api", "name": "Delta 2913", "description": "The Delta 2000 series was an American expendable launch system which was used to conduct forty-four orbital launches between 1974 and 1981. It was a member of the Delta family of rockets. Several variants existed, which were differentiated by a four digit numerical code.", "family": "Delta", "full_name": "Delta 2913", "variant": "2913", "alias": "", "min_stage": 3, "max_stage": 3, "length": 35.0, "diameter": 2.44, "maiden_flight": "1975-08-09", "launch_mass": 131, "leo_capacity": 2000, "gto_capacity": 700, "to_thrust": 2560, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/delta_2910_image_20231231105214.jpeg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_2000", "consecutive_successful_launches": 2, "successful_launches": 2, "failed_launches": 0, "pending_launches": 0 }, { "id": 287, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/287/?format=api", "name": "Delta 2914", "description": "The Delta 2000 series was an American expendable launch system which was used to conduct forty-four orbital launches between 1974 and 1981. It was a member of the Delta family of rockets. Several variants existed, which were differentiated by a four digit numerical code.", "family": "Delta", "full_name": "Delta 2914", "variant": "2914", "alias": "", "min_stage": 4, "max_stage": 4, "length": 35.0, "diameter": 2.44, "maiden_flight": "1974-04-13", "launch_mass": 130, "leo_capacity": 724, "gto_capacity": null, "to_thrust": 2287, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/delta_2910_image_20231231105214.jpeg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_2000", "consecutive_successful_launches": 13, "successful_launches": 28, "failed_launches": 2, "pending_launches": 0 }, { "id": 288, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/288/?format=api", "name": "Delta 3910", "description": "The Delta 3000 series was an American expendable launch system which was used to conduct 38 orbital launches between 1975 and 1989. It was a member of the Delta family of rockets. Several variants existed, which were differentiated by a four digit numerical code.", "family": "Delta", "full_name": "Delta 3910", "variant": "3910", "alias": "", "min_stage": 3, "max_stage": 3, "length": 35.0, "diameter": 2.44, "maiden_flight": "1980-02-14", "launch_mass": 190, "leo_capacity": null, "gto_capacity": null, "to_thrust": 3188, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/delta_3910_image_20231231105538.jpeg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_3000", "consecutive_successful_launches": 3, "successful_launches": 3, "failed_launches": 0, "pending_launches": 0 }, { "id": 289, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/289/?format=api", "name": "Delta 3910/PAM", "description": "The Delta 3000 series was an American expendable launch system which was used to conduct 38 orbital launches between 1975 and 1989. It was a member of the Delta family of rockets. Several variants existed, which were differentiated by a four digit numerical code.", "family": "Delta", "full_name": "Delta 3910/PAM", "variant": "3910/PAM", "alias": "", "min_stage": 4, "max_stage": 4, "length": 35.0, "diameter": 2.44, "maiden_flight": "1980-11-15", "launch_mass": 191, "leo_capacity": 1087, "gto_capacity": null, "to_thrust": 3188, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/delta_3910_image_20231231105538.jpeg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_3000", "consecutive_successful_launches": 7, "successful_launches": 7, "failed_launches": 0, "pending_launches": 0 }, { "id": 290, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/290/?format=api", "name": "Delta 3913", "description": "The Delta 3000 series was an American expendable launch system which was used to conduct 38 orbital launches between 1975 and 1989. It was a member of the Delta family of rockets. Several variants existed, which were differentiated by a four digit numerical code.", "family": "Delta", "full_name": "Delta 3913", "variant": "3913", "alias": "", "min_stage": 4, "max_stage": 4, "length": 35.0, "diameter": 2.44, "maiden_flight": "1981-08-03", "launch_mass": 190, "leo_capacity": null, "gto_capacity": null, "to_thrust": 3188, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/delta_3910_image_20231231105538.jpeg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_3000", "consecutive_successful_launches": 1, "successful_launches": 1, "failed_launches": 0, "pending_launches": 0 }, { "id": 291, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/291/?format=api", "name": "Delta 3914", "description": "The Delta 3000 series was an American expendable launch system which was used to conduct 38 orbital launches between 1975 and 1989. It was a member of the Delta family of rockets. Several variants existed, which were differentiated by a four digit numerical code.", "family": "Delta", "full_name": "Delta 3914", "variant": "3914", "alias": "", "min_stage": 4, "max_stage": 4, "length": 35.0, "diameter": 2.44, "maiden_flight": "1975-12-13", "launch_mass": 185, "leo_capacity": 951, "gto_capacity": 954, "to_thrust": 3046, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/delta_3910_image_20231231105538.jpeg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_3000", "consecutive_successful_launches": 0, "successful_launches": 10, "failed_launches": 2, "pending_launches": 0 }, { "id": 292, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/292/?format=api", "name": "Delta 3920", "description": "The Delta 3000 series was an American expendable launch system which was used to conduct 38 orbital launches between 1975 and 1989. It was a member of the Delta family of rockets. Several variants existed, which were differentiated by a four digit numerical code.", "family": "Delta", "full_name": "Delta 3920", "variant": "3920", "alias": "", "min_stage": 3, "max_stage": 3, "length": 36.0, "diameter": 2.44, "maiden_flight": "1982-07-16", "launch_mass": 191, "leo_capacity": null, "gto_capacity": null, "to_thrust": 3188, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/delta_3910_image_20231231105538.jpeg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_3000", "consecutive_successful_launches": 3, "successful_launches": 3, "failed_launches": 0, "pending_launches": 0 }, { "id": 293, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/293/?format=api", "name": "Delta 3920-8", "description": "The Delta 3000 series was an American expendable launch system which was used to conduct 38 orbital launches between 1975 and 1989. It was a member of the Delta family of rockets. Several variants existed, which were differentiated by a four digit numerical code.", "family": "Delta", "full_name": "Delta 3920-8", "variant": "3920-8", "alias": "", "min_stage": 3, "max_stage": 3, "length": 36.0, "diameter": 2.44, "maiden_flight": "1989-03-24", "launch_mass": 190, "leo_capacity": null, "gto_capacity": null, "to_thrust": 3188, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/delta_3910_image_20231231105538.jpeg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_3000", "consecutive_successful_launches": 1, "successful_launches": 1, "failed_launches": 0, "pending_launches": 0 }, { "id": 294, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/294/?format=api", "name": "Delta 3920/PAM", "description": "The Delta 3000 series was an American expendable launch system which was used to conduct 38 orbital launches between 1975 and 1989. It was a member of the Delta family of rockets. Several variants existed, which were differentiated by a four digit numerical code.", "family": "Delta", "full_name": "Delta 3920/PAM", "variant": "3920/PAM", "alias": "", "min_stage": 4, "max_stage": 4, "length": 36.0, "diameter": 2.44, "maiden_flight": "1982-08-26", "launch_mass": 191, "leo_capacity": 1280, "gto_capacity": null, "to_thrust": 3188, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/delta_3910_image_20231231105538.jpeg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_3000", "consecutive_successful_launches": 6, "successful_launches": 6, "failed_launches": 0, "pending_launches": 0 }, { "id": 295, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/295/?format=api", "name": "Delta 3924", "description": "The Delta 3000 series was an American expendable launch system which was used to conduct 38 orbital launches between 1975 and 1989. It was a member of the Delta family of rockets. Several variants existed, which were differentiated by a four digit numerical code.", "family": "Delta", "full_name": "Delta 3924", "variant": "3924", "alias": "", "min_stage": 4, "max_stage": 4, "length": 36.0, "diameter": 2.44, "maiden_flight": "1982-10-28", "launch_mass": 191, "leo_capacity": null, "gto_capacity": 954, "to_thrust": 3188, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/delta_3910_image_20231231105538.jpeg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_3000", "consecutive_successful_launches": 5, "successful_launches": 5, "failed_launches": 0, "pending_launches": 0 }, { "id": 296, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/296/?format=api", "name": "Delta 4925-8", "description": "The Delta 4000 series was an American expendable launch system which was used to conduct two orbital launches in 1989 and 1990. It was a member of the Delta family of rockets.", "family": "Delta", "full_name": "Delta 4925-8", "variant": "4925-8", "alias": "", "min_stage": 4, "max_stage": 4, "length": 34.0, "diameter": 2.44, "maiden_flight": "1989-08-27", "launch_mass": 200, "leo_capacity": 3400, "gto_capacity": 1200, "to_thrust": 3468, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_4000", "consecutive_successful_launches": 2, "successful_launches": 2, "failed_launches": 0, "pending_launches": 0 }, { "id": 297, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/297/?format=api", "name": "Delta 5920-8", "description": "The Delta 5000 series was an American expendable launch system which was used to conduct an orbital launch in 1989. It was a member of the Delta family of rockets. Although several variants were put forward, only the Delta 5920 was launched.", "family": "Delta", "full_name": "Delta 5920-8", "variant": "5920-8", "alias": "", "min_stage": 3, "max_stage": 3, "length": 34.0, "diameter": 2.44, "maiden_flight": "1989-11-18", "launch_mass": 201, "leo_capacity": 3848, "gto_capacity": 1405, "to_thrust": 3468, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_5000", "consecutive_successful_launches": 1, "successful_launches": 1, "failed_launches": 0, "pending_launches": 0 }, { "id": 308, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/308/?format=api", "name": "Delta II", "description": "Delta II was an expendable launch system, originally designed and built by McDonnell Douglas. Delta II was part of the Delta rocket family and entered service in 1989. Delta II vehicles included the Delta 6000, and the two later Delta 7000 variants (\"Light\" and \"Heavy\"). The rocket flew its final mission ICESat-2 on 15 September 2018, earning the launch vehicle a streak of 100 successful missions in a row, with the last failure being GPS IIR-1 in 1997.", "family": "Delta", "full_name": "Delta II 7925-10", "variant": "7925-10", "alias": "", "min_stage": 4, "max_stage": 4, "length": 38.9, "diameter": 2.44, "maiden_flight": "1994-11-01", "launch_mass": 231, "leo_capacity": null, "gto_capacity": null, "to_thrust": 4000, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_II", "consecutive_successful_launches": 2, "successful_launches": 2, "failed_launches": 0, "pending_launches": 0 }, { "id": 300, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/300/?format=api", "name": "Delta II", "description": "Delta II was an expendable launch system, originally designed and built by McDonnell Douglas. Delta II was part of the Delta rocket family and entered service in 1989. Delta II vehicles included the Delta 6000, and the two later Delta 7000 variants (\"Light\" and \"Heavy\"). The rocket flew its final mission ICESat-2 on 15 September 2018, earning the launch vehicle a streak of 100 successful missions in a row, with the last failure being GPS IIR-1 in 1997.", "family": "Delta", "full_name": "Delta II 6925", "variant": "6925", "alias": "", "min_stage": 4, "max_stage": 4, "length": 38.1, "diameter": 2.44, "maiden_flight": "1989-02-14", "launch_mass": 218, "leo_capacity": 3981, "gto_capacity": 1446, "to_thrust": 3981, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_II", "consecutive_successful_launches": 13, "successful_launches": 13, "failed_launches": 0, "pending_launches": 0 }, { "id": 305, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/305/?format=api", "name": "Delta II", "description": "Delta II was an expendable launch system, originally designed and built by McDonnell Douglas. Delta II was part of the Delta rocket family and entered service in 1989. Delta II vehicles included the Delta 6000, and the two later Delta 7000 variants (\"Light\" and \"Heavy\"). The rocket flew its final mission ICESat-2 on 15 September 2018, earning the launch vehicle a streak of 100 successful missions in a row, with the last failure being GPS IIR-1 in 1997.", "family": "Delta", "full_name": "Delta II 7426-9.5", "variant": "7426-9.5", "alias": "", "min_stage": 4, "max_stage": 4, "length": 39.0, "diameter": 2.44, "maiden_flight": "1999-02-07", "launch_mass": 170, "leo_capacity": null, "gto_capacity": null, "to_thrust": 3020, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_II", "consecutive_successful_launches": 1, "successful_launches": 1, "failed_launches": 0, "pending_launches": 0 }, { "id": 307, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/307/?format=api", "name": "Delta II", "description": "Delta II was an expendable launch system, originally designed and built by McDonnell Douglas. Delta II was part of the Delta rocket family and entered service in 1989. Delta II vehicles included the Delta 6000, and the two later Delta 7000 variants (\"Light\" and \"Heavy\"). The rocket flew its final mission ICESat-2 on 15 September 2018, earning the launch vehicle a streak of 100 successful missions in a row, with the last failure being GPS IIR-1 in 1997.", "family": "Delta", "full_name": "Delta II 7920-8", "variant": "7920-8", "alias": "", "min_stage": 3, "max_stage": 3, "length": 39.0, "diameter": 2.44, "maiden_flight": "1997-08-25", "launch_mass": 220, "leo_capacity": null, "gto_capacity": null, "to_thrust": 4000, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_II", "consecutive_successful_launches": 1, "successful_launches": 1, "failed_launches": 0, "pending_launches": 0 }, { "id": 301, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/301/?format=api", "name": "Delta II", "description": "Delta II was an expendable launch system, originally designed and built by McDonnell Douglas. Delta II was part of the Delta rocket family and entered service in 1989. Delta II vehicles included the Delta 6000, and the two later Delta 7000 variants (\"Light\" and \"Heavy\"). The rocket flew its final mission ICESat-2 on 15 September 2018, earning the launch vehicle a streak of 100 successful missions in a row, with the last failure being GPS IIR-1 in 1997.", "family": "Delta", "full_name": "Delta II 6925-8", "variant": "6925-8", "alias": "", "min_stage": 4, "max_stage": 4, "length": 39.0, "diameter": 2.44, "maiden_flight": "1990-04-13", "launch_mass": 219, "leo_capacity": 1500, "gto_capacity": null, "to_thrust": null, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_II", "consecutive_successful_launches": 1, "successful_launches": 1, "failed_launches": 0, "pending_launches": 0 }, { "id": 467, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/467/?format=api", "name": "Delta II", "description": "Delta II was an expendable launch system, originally designed and built by McDonnell Douglas. Delta II was part of the Delta rocket family and entered service in 1989. 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The rocket flew its final mission ICESat-2 on 15 September 2018, earning the launch vehicle a streak of 100 successful missions in a row, with the last failure being GPS IIR-1 in 1997.", "family": "Delta", "full_name": "Delta II 7420-10C", "variant": "7420-10C", "alias": "", "min_stage": 3, "max_stage": 3, "length": 39.0, "diameter": 2.44, "maiden_flight": "1998-02-14", "launch_mass": 170, "leo_capacity": null, "gto_capacity": null, "to_thrust": 3020, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_II", "consecutive_successful_launches": 8, "successful_launches": 8, "failed_launches": 0, "pending_launches": 0 }, { "id": 298, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/298/?format=api", "name": "Delta II", "description": "Delta II was an expendable launch system, originally designed and built by McDonnell Douglas. Delta II was part of the Delta rocket family and entered service in 1989. 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The rocket flew its final mission ICESat-2 on 15 September 2018, earning the launch vehicle a streak of 100 successful missions in a row, with the last failure being GPS IIR-1 in 1997.", "family": "Delta", "full_name": "Delta II 7326-9.5", "variant": "7326-9.5", "alias": "", "min_stage": 4, "max_stage": 4, "length": 38.4, "diameter": 2.44, "maiden_flight": "1998-10-24", "launch_mass": 155, "leo_capacity": null, "gto_capacity": null, "to_thrust": 2500, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_II", "consecutive_successful_launches": 3, "successful_launches": 3, "failed_launches": 0, "pending_launches": 0 }, { "id": 306, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/306/?format=api", "name": "Delta II", "description": "Delta II was an expendable launch system, originally designed and built by McDonnell Douglas. Delta II was part of the Delta rocket family and entered service in 1989. 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The rocket flew its final mission ICESat-2 on 15 September 2018, earning the launch vehicle a streak of 100 successful missions in a row, with the last failure being GPS IIR-1 in 1997.", "family": "Delta", "full_name": "Delta II 7920-10L", "variant": "7920-10L", "alias": "", "min_stage": 3, "max_stage": 3, "length": 40.0, "diameter": 2.44, "maiden_flight": "2002-05-04", "launch_mass": 232, "leo_capacity": null, "gto_capacity": null, "to_thrust": null, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_II", "consecutive_successful_launches": 2, "successful_launches": 2, "failed_launches": 0, "pending_launches": 0 }, { "id": 299, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/299/?format=api", "name": "Delta II", "description": "Delta II was an expendable launch system, originally designed and built by McDonnell Douglas. Delta II was part of the Delta rocket family and entered service in 1989. 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The rocket flew its final mission ICESat-2 on 15 September 2018, earning the launch vehicle a streak of 100 successful missions in a row, with the last failure being GPS IIR-1 in 1997.", "family": "Delta", "full_name": "Delta II 7425-10", "variant": "7425-10", "alias": "", "min_stage": 4, "max_stage": 4, "length": 39.0, "diameter": 2.44, "maiden_flight": "2001-06-30", "launch_mass": 170, "leo_capacity": null, "gto_capacity": null, "to_thrust": 3020, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_II", "consecutive_successful_launches": 1, "successful_launches": 1, "failed_launches": 0, "pending_launches": 0 }, { "id": 309, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/309/?format=api", "name": "Delta II", "description": "Delta II was an expendable launch system, originally designed and built by McDonnell Douglas. Delta II was part of the Delta rocket family and entered service in 1989. 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The rocket flew its final mission ICESat-2 on 15 September 2018, earning the launch vehicle a streak of 100 successful missions in a row, with the last failure being GPS IIR-1 in 1997.", "family": "Delta", "full_name": "Delta II 7925-8", "variant": "7925-8", "alias": "", "min_stage": 4, "max_stage": 4, "length": 38.2, "diameter": 2.44, "maiden_flight": "1994-02-19", "launch_mass": 220, "leo_capacity": null, "gto_capacity": null, "to_thrust": 4000, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Delta_II", "consecutive_successful_launches": 2, "successful_launches": 2, "failed_launches": 0, "pending_launches": 0 }, { "id": 304, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/304/?format=api", "name": "Delta II", "description": "Delta II was an expendable launch system, originally designed and built by McDonnell Douglas. Delta II was part of the Delta rocket family and entered service in 1989. 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Thor with Able stage derived from Vanguard second stage.", "family": "Thor", "full_name": "Thor Able I", "variant": "Able I", "alias": "", "min_stage": 2, "max_stage": 2, "length": 30.0, "diameter": 2.44, "maiden_flight": "1958-04-24", "launch_mass": 51, "leo_capacity": 120, "gto_capacity": null, "to_thrust": 667, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Thor-Able", "consecutive_successful_launches": 0, "successful_launches": 1, "failed_launches": 2, "pending_launches": 0 }, { "id": 389, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/389/?format=api", "name": "Thor Able II", "description": "American orbital launch vehicle. Thor with Able stage derived from Vanguard second stage.", "family": "Thor", "full_name": "Thor Able II", "variant": "Able II", "alias": "", "min_stage": 2, "max_stage": 2, "length": 27.3, "diameter": 2.44, "maiden_flight": "1959-01-23", "launch_mass": 52, "leo_capacity": null, "gto_capacity": null, "to_thrust": 668, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": "", "wiki_url": "https://en.wikipedia.org/wiki/Thor-Able", "consecutive_successful_launches": 1, "successful_launches": 1, "failed_launches": 1, "pending_launches": 0 }, { "id": 390, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/390/?format=api", "name": "Thor Able III", "description": "American orbital launch vehicle. Thor with Able stage derived from Vanguard second stage.", "family": "Thor", "full_name": "Thor Able III", "variant": "Able III", "alias": "", "min_stage": 3, "max_stage": 3, "length": 27.4, "diameter": 2.44, "maiden_flight": "1959-08-07", "launch_mass": 52, "leo_capacity": null, "gto_capacity": null, "to_thrust": 668, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": "", "wiki_url": "https://en.wikipedia.org/wiki/Thor-Able", "consecutive_successful_launches": 1, "successful_launches": 1, "failed_launches": 0, "pending_launches": 0 }, { "id": 391, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/391/?format=api", "name": "Thor Able IV", "description": "American orbital launch vehicle. Thor with Able stage derived from Vanguard second stage.", "family": "Thor", "full_name": "Thor Able IV", "variant": "Able IV", "alias": "", "min_stage": 3, "max_stage": 3, "length": 27.2, "diameter": 2.44, "maiden_flight": "1960-03-11", "launch_mass": 52, "leo_capacity": null, "gto_capacity": null, "to_thrust": 668, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": "", "wiki_url": "https://en.wikipedia.org/wiki/Thor-Able", "consecutive_successful_launches": 1, "successful_launches": 1, "failed_launches": 0, "pending_launches": 0 }, { "id": 418, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/418/?format=api", "name": "Thorad SLV-2G Agena D", "description": "Thor-Agena was a series of orbital launch vehicles. The rockets used Thor first stages and Agena second stages. 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They are thus cousins of the more-famous Thor-Deltas, which founded the Delta rocket family.", "family": "Thor", "full_name": "Thor Agena A", "variant": "Agena A", "alias": "", "min_stage": 2, "max_stage": 2, "length": 28.0, "diameter": 2.44, "maiden_flight": "1959-01-21", "launch_mass": 53, "leo_capacity": 250, "gto_capacity": null, "to_thrust": 667, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Thor-Agena", "consecutive_successful_launches": 3, "successful_launches": 9, "failed_launches": 6, "pending_launches": 0 }, { "id": 393, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/393/?format=api", "name": "Thor Agena D", "description": "Thor-Agena was a series of orbital launch vehicles. The rockets used Thor first stages and Agena second stages. 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"description": "American orbital launch vehicle family with Thor first stage and a delta second stage.", "family": "Thor", "full_name": "Thor Delta E1", "variant": "Delta E1", "alias": "", "min_stage": 4, "max_stage": 4, "length": 28.0, "diameter": 2.44, "maiden_flight": "1966-07-01", "launch_mass": 68, "leo_capacity": 540, "gto_capacity": 150, "to_thrust": 1450, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": "", "wiki_url": "https://en.wikipedia.org/wiki/Thor-Delta", "consecutive_successful_launches": 1, "successful_launches": 16, "failed_launches": 1, "pending_launches": 0 }, { "id": 406, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/406/?format=api", "name": "Thor Delta G", "description": "American orbital launch vehicle family with Thor first stage and a delta second stage.", "family": "Thor", "full_name": "Thor Delta G", "variant": "Delta G", "alias": "", "min_stage": 3, "max_stage": 3, "length": 30.0, "diameter": 2.44, "maiden_flight": 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"successful_launches": 1, "failed_launches": 0, "pending_launches": 0 }, { "id": 408, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/408/?format=api", "name": "Thor Delta L", "description": "American orbital launch vehicle family with Thor first stage and a delta second stage.", "family": "Thor", "full_name": "Thor Delta L", "variant": "Delta L", "alias": "", "min_stage": 4, "max_stage": 4, "length": 35.0, "diameter": 2.44, "maiden_flight": "1969-08-27", "launch_mass": 89, "leo_capacity": 300, "gto_capacity": 300, "to_thrust": 1452, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Thor-Delta", "consecutive_successful_launches": 1, "successful_launches": 1, "failed_launches": 1, "pending_launches": 0 }, { "id": 409, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/409/?format=api", "name": "Thor Delta M", "description": "American orbital launch vehicle family with Thor first stage and a delta 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