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/82/?format=api
{ "id": 82, "url": "https://ll.thespacedevs.com/2.2.0/agencies/82/?format=api", "name": "Lockheed Martin", "featured": false, "type": "Commercial", "country_code": "USA", "abbrev": "LMT", "description": "Lockheed Martin's Space Division started in the production of missiles and later ICBM's in the 1950s. Their TITAN missile system was used for 12 Gemini spacecraft and the Voyager probes. They have worked largely in collaboration with NASA on many of their probes, landers, and spacecraft, and hope to play a key role in NASA's return to the moon in 2024.", "administrator": null, "founding_year": "1953", "launchers": "Titan | Agena", "spacecraft": "Hubble | JUNO | InSight", "parent": null, "launch_library_url": null, "total_launch_count": 80, "successful_launches": 77, "consecutive_successful_launches": 38, "failed_launches": 3, "pending_launches": 0, "successful_landings": 0, "failed_landings": 0, "attempted_landings": 0, "consecutive_successful_landings": 0, "info_url": "http://www.lockheedmartin.com/", "wiki_url": "http://en.wikipedia.org/wiki/Lockheed_Martin", "logo_url": null, "image_url": null, "nation_url": null, "launcher_list": [ { "id": 228, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/228/?format=api", "name": "Athena I", "description": "The Athena I, known as the Lockheed Launch Vehicle (LLV) at the time of its first flight and Lockheed Martin Launch Vehicle (LMLV) at the time of its second flight, is an American small expendable launch system which was used for four launches between 1995 and 2001. It is a member of the Athena family of rockets, along with the larger Athena II.", "family": "Athena", "full_name": "Athena I", "variant": "I", "alias": "", "min_stage": 3, "max_stage": 3, "length": 18.9, "diameter": 2.36, "maiden_flight": "1995-08-15", "launch_mass": 66, "leo_capacity": 820, "gto_capacity": null, "to_thrust": 1900, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/athena_1_liftof_image_20240411090356.jpeg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Athena_I", "consecutive_successful_launches": 3, "successful_launches": 3, "failed_launches": 1, "pending_launches": 0 }, { "id": 229, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/229/?format=api", "name": "Athena II", "description": "The Athena II is an American small expendable launch system which was used for three launches between 1998 and 1999.", "family": "Athena", "full_name": "Athena II", "variant": "II", "alias": "", "min_stage": 4, "max_stage": 4, "length": 28.2, "diameter": 2.36, "maiden_flight": "1998-01-07", "launch_mass": 120, "leo_capacity": 2065, "gto_capacity": 593, "to_thrust": 1900, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/athena_2_with_l_image_20240411091736.jpeg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Athena_II", "consecutive_successful_launches": 1, "successful_launches": 2, "failed_launches": 1, "pending_launches": 0 }, { "id": 253, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/253/?format=api", "name": "Atlas II", "description": "Atlas II was a member of the Atlas family of launch vehicles, which evolved from the successful Atlas missile program of the 1950s. It was designed to launch payloads into low earth orbit, geosynchronous transfer orbit or geosynchronous orbit. Sixty-three launches of the Atlas II, IIA and IIAS models were carried out between 1991 and 2004; all sixty-three launches were successes, making the Atlas II the most reliable launch system in history.", "family": "Atlas", "full_name": "Atlas II", "variant": "II", "alias": "", "min_stage": 3, "max_stage": 3, "length": 47.54, "diameter": 3.04, "maiden_flight": "1991-12-07", "launch_mass": 204, "leo_capacity": 6580, "gto_capacity": 2810, "to_thrust": 2479, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Atlas_II", "consecutive_successful_launches": 10, "successful_launches": 10, "failed_launches": 0, "pending_launches": 0 }, { "id": 254, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/254/?format=api", "name": "Atlas IIA", "description": "Atlas II was a member of the Atlas family of launch vehicles, which evolved from the successful Atlas missile program of the 1950s. It was designed to launch payloads into low earth orbit, geosynchronous transfer orbit or geosynchronous orbit. Sixty-three launches of the Atlas II, IIA and IIAS models were carried out between 1991 and 2004; all sixty-three launches were successes, making the Atlas II the most reliable launch system in history.", "family": "Atlas", "full_name": "Atlas IIA", "variant": "IIA", "alias": "", "min_stage": 3, "max_stage": 3, "length": 47.54, "diameter": 3.04, "maiden_flight": "1992-06-10", "launch_mass": 204, "leo_capacity": 6580, "gto_capacity": 2810, "to_thrust": 2479, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Atlas_II", "consecutive_successful_launches": 23, "successful_launches": 23, "failed_launches": 0, "pending_launches": 0 }, { "id": 255, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/255/?format=api", "name": "Atlas IIAS", "description": "Atlas II was a member of the Atlas family of launch vehicles, which evolved from the successful Atlas missile program of the 1950s. It was designed to launch payloads into low earth orbit, geosynchronous transfer orbit or geosynchronous orbit. Sixty-three launches of the Atlas II, IIA and IIAS models were carried out between 1991 and 2004; all sixty-three launches were successes, making the Atlas II the most reliable launch system in history.", "family": "Atlas", "full_name": "Atlas IIAS", "variant": "IIAS", "alias": "", "min_stage": 3, "max_stage": 3, "length": 47.54, "diameter": 3.04, "maiden_flight": "1993-12-16", "launch_mass": 204, "leo_capacity": 6580, "gto_capacity": 2810, "to_thrust": 4391, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Atlas_II", "consecutive_successful_launches": 30, "successful_launches": 30, "failed_launches": 0, "pending_launches": 0 }, { "id": 471, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/471/?format=api", "name": "Atlas IIIA", "description": "American orbital launch vehicle used between 2000 and 2005.", "family": "Atlas", "full_name": "Atlas IIIA", "variant": "IIIA", "alias": "", "min_stage": 2, "max_stage": 2, "length": 52.8, "diameter": 3.05, "maiden_flight": "2000-05-24", "launch_mass": 214, "leo_capacity": 8640, "gto_capacity": 4055, "to_thrust": 4149, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/atlas_iiia_image_20210901074920.jpg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Atlas_III", "consecutive_successful_launches": 2, "successful_launches": 2, "failed_launches": 0, "pending_launches": 0 }, { "id": 472, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/472/?format=api", "name": "Atlas IIIB", "description": "American orbital launch vehicle used between 2000 and 2005.", "family": "Atlas", "full_name": "Atlas IIIB", "variant": "IIIB", "alias": "", "min_stage": 2, "max_stage": 2, "length": 52.8, "diameter": 3.05, "maiden_flight": "2002-02-21", "launch_mass": 213, "leo_capacity": 10218, "gto_capacity": 4498, "to_thrust": 4149, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/atlas_iiia_image_20210901074920.jpg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Atlas_III", "consecutive_successful_launches": 4, "successful_launches": 4, "failed_launches": 0, "pending_launches": 0 }, { "id": 272, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/272/?format=api", "name": "Commercial Titan III", "description": "The Commercial Titan III, also known as CT-3 or CT-III, was an American expendable launch system, developed by Martin Marietta during the late 1980s and flown four times during the early 1990s. It was derived from the Titan 34D, and was originally proposed as a medium-lift expendable launch system for the US Air Force, who selected the Delta II instead. Development was continued as a commercial launch system, and the first rocket flew in 1990. Due to higher costs than contemporary rockets such as the Ariane 4, orders were not forthcoming, and the CT-3 was retired in 1992.", "family": "Titan", "full_name": "Commercial Titan III", "variant": "III", "alias": "", "min_stage": 2, "max_stage": 3, "length": 47.3, "diameter": 3.05, "maiden_flight": "1990-01-01", "launch_mass": 680, "leo_capacity": 14742, "gto_capacity": 4990, "to_thrust": null, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/commercial_tita_image_20240411092244.jpeg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Commercial_Titan_III", "consecutive_successful_launches": 4, "successful_launches": 4, "failed_launches": 0, "pending_launches": 0 }, { "id": 420, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/420/?format=api", "name": "Titan 23B", "description": "Titan IIIB was the collective name for a number of derivatives of the Titan II ICBM and Titan III launch vehicle, modified by the addition of an Agena upper stage. It consisted of four separate rockets. The Titan 23B was a basic Titan II with an Agena upper stage, and the Titan 24B was the same concept, but using the slightly enlarged Titan IIIM rocket as the base. The Titan 33B was a Titan 23B with the Agena (which had a smaller diameter than the Titan) enclosed in an enlarged fairing, in order to allow larger payloads to be launched. The final member of the Titan IIIB family was the Titan 34B which was a Titan 24B with the larger fairing used on the Titan 33B.", "family": "Titan", "full_name": "Titan 23B", "variant": "23B", "alias": "", "min_stage": 3, "max_stage": 3, "length": 45.0, "diameter": 3.05, "maiden_flight": "1969-08-23", "launch_mass": 165, "leo_capacity": 3000, "gto_capacity": null, "to_thrust": 2300, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": "", "wiki_url": "https://en.wikipedia.org/wiki/Titan_IIIB", "consecutive_successful_launches": 9, "successful_launches": 9, "failed_launches": 0, "pending_launches": 0 }, { "id": 421, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/421/?format=api", "name": "Titan 24B", "description": "Titan IIIB was the collective name for a number of derivatives of the Titan II ICBM and Titan III launch vehicle, modified by the addition of an Agena upper stage. It consisted of four separate rockets. The Titan 23B was a basic Titan II with an Agena upper stage, and the Titan 24B was the same concept, but using the slightly enlarged Titan IIIM rocket as the base. The Titan 33B was a Titan 23B with the Agena (which had a smaller diameter than the Titan) enclosed in an enlarged fairing, in order to allow larger payloads to be launched. The final member of the Titan IIIB family was the Titan 34B which was a Titan 24B with the larger fairing used on the Titan 33B.", "family": "Titan", "full_name": "Titan 24B", "variant": "24B", "alias": "", "min_stage": 3, "max_stage": 3, "length": 45.0, "diameter": 3.05, "maiden_flight": "1971-08-12", "launch_mass": 170, "leo_capacity": 3000, "gto_capacity": null, "to_thrust": 2410, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": "", "wiki_url": "https://en.wikipedia.org/wiki/Titan_IIIB", "consecutive_successful_launches": 15, "successful_launches": 21, "failed_launches": 2, "pending_launches": 0 }, { "id": 422, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/422/?format=api", "name": "Titan 33B", "description": "Titan IIIB was the collective name for a number of derivatives of the Titan II ICBM and Titan III launch vehicle, modified by the addition of an Agena upper stage. It consisted of four separate rockets. The Titan 23B was a basic Titan II with an Agena upper stage, and the Titan 24B was the same concept, but using the slightly enlarged Titan IIIM rocket as the base. The Titan 33B was a Titan 23B with the Agena (which had a smaller diameter than the Titan) enclosed in an enlarged fairing, in order to allow larger payloads to be launched. The final member of the Titan IIIB family was the Titan 34B which was a Titan 24B with the larger fairing used on the Titan 33B.", "family": "Titan", "full_name": "Titan 33B", "variant": "33B", "alias": "", "min_stage": 3, "max_stage": 3, "length": 45.0, "diameter": 3.05, "maiden_flight": "1971-03-21", "launch_mass": 185, "leo_capacity": 3000, "gto_capacity": null, "to_thrust": 2300, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": "", "wiki_url": "https://en.wikipedia.org/wiki/Titan_IIIB", "consecutive_successful_launches": 1, "successful_launches": 2, "failed_launches": 1, "pending_launches": 0 }, { "id": 423, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/423/?format=api", "name": "Titan 34B", "description": "Titan IIIB was the collective name for a number of derivatives of the Titan II ICBM and Titan III launch vehicle, modified by the addition of an Agena upper stage. It consisted of four separate rockets. The Titan 23B was a basic Titan II with an Agena upper stage, and the Titan 24B was the same concept, but using the slightly enlarged Titan IIIM rocket as the base. The Titan 33B was a Titan 23B with the Agena (which had a smaller diameter than the Titan) enclosed in an enlarged fairing, in order to allow larger payloads to be launched. The final member of the Titan IIIB family was the Titan 34B which was a Titan 24B with the larger fairing used on the Titan 33B.", "family": "Titan", "full_name": "Titan 34B", "variant": "34B", "alias": "", "min_stage": 3, "max_stage": 3, "length": 48.0, "diameter": 3.05, "maiden_flight": "1975-03-10", "launch_mass": 188, "leo_capacity": 3500, "gto_capacity": null, "to_thrust": 1997, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Titan_IIIB", "consecutive_successful_launches": 11, "successful_launches": 11, "failed_launches": 0, "pending_launches": 0 }, { "id": 424, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/424/?format=api", "name": "Titan 34D", "description": "The Titan 34D was a United States expendable launch vehicle used to launch a number of satellites for military applications.", "family": "Titan", "full_name": "Titan 34D", "variant": "34D", "alias": "", "min_stage": 2, "max_stage": 2, "length": 50.0, "diameter": 3.05, "maiden_flight": "1983-06-20", "launch_mass": 723, "leo_capacity": 14515, "gto_capacity": 5000, "to_thrust": 11279, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Titan_34D", "consecutive_successful_launches": 2, "successful_launches": 5, "failed_launches": 2, "pending_launches": 0 }, { "id": 425, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/425/?format=api", "name": "Titan 34D IUS", "description": "The Titan 34D was a United States expendable launch vehicle used to launch a number of satellites for military applications.", "family": "Titan", "full_name": "Titan 34D IUS", "variant": "34D IUS", "alias": "", "min_stage": 2, "max_stage": 2, "length": 52.4, "diameter": 3.05, "maiden_flight": "1982-10-30", "launch_mass": 725, "leo_capacity": null, "gto_capacity": 5000, "to_thrust": 11279, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": "", "wiki_url": "https://en.wikipedia.org/wiki/Titan_34D", "consecutive_successful_launches": 1, "successful_launches": 1, "failed_launches": 0, "pending_launches": 0 }, { "id": 426, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/426/?format=api", "name": "Titan 34D Transtage", "description": "The Titan 34D was a United States expendable launch vehicle used to launch a number of satellites for military applications.", "family": "Titan", "full_name": "Titan 34D Transtage", "variant": "34D Transtage", "alias": "", "min_stage": 2, "max_stage": 2, "length": 50.0, "diameter": 3.05, "maiden_flight": "1984-01-31", "launch_mass": 720, "leo_capacity": null, "gto_capacity": 5000, "to_thrust": 11280, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": "", "wiki_url": "https://en.wikipedia.org/wiki/Titan_34D", "consecutive_successful_launches": 7, "successful_launches": 7, "failed_launches": 0, "pending_launches": 0 }, { "id": 427, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/427/?format=api", "name": "Titan 401A Centaur", "description": "Titan IV was a family of heavy-lift space launch vehicles developed by Martin Marietta and operated by the United States Air Force from 1989 to 2005.", "family": "Titan", "full_name": "Titan 401A Centaur", "variant": "401A Centaur", "alias": "", "min_stage": 3, "max_stage": 3, "length": 63.1, "diameter": 3.05, "maiden_flight": "1994-02-07", "launch_mass": 868, "leo_capacity": 21680, "gto_capacity": 9000, "to_thrust": 14200, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": "", "wiki_url": "https://en.wikipedia.org/wiki/Titan_IV", "consecutive_successful_launches": 0, "successful_launches": 8, "failed_launches": 1, "pending_launches": 0 }, { "id": 428, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/428/?format=api", "name": "Titan 402A IUS", "description": "Titan IV was a family of heavy-lift space launch vehicles developed by Martin Marietta and operated by the United States Air Force from 1989 to 2005.", "family": "Titan", "full_name": "Titan 402A IUS", "variant": "402A IUS", "alias": "", "min_stage": 3, "max_stage": 3, "length": 54.0, "diameter": 3.05, "maiden_flight": "1989-06-14", "launch_mass": 910, "leo_capacity": 21680, "gto_capacity": null, "to_thrust": 14200, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": "", "wiki_url": "https://en.wikipedia.org/wiki/Titan_IV", "consecutive_successful_launches": 3, "successful_launches": 3, "failed_launches": 0, "pending_launches": 0 }, { "id": 429, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/429/?format=api", "name": "Titan 402B IUS", "description": "Titan IV was a family of heavy-lift space launch vehicles developed by Martin Marietta and operated by the United States Air Force from 1989 to 2005.", "family": "Titan", "full_name": "Titan 402B IUS", "variant": "402B IUS", "alias": "", "min_stage": 3, "max_stage": 3, "length": 54.0, "diameter": 3.05, "maiden_flight": "1997-02-23", "launch_mass": 925, "leo_capacity": 21680, "gto_capacity": null, "to_thrust": 15000, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": "", "wiki_url": "https://en.wikipedia.org/wiki/Titan_IV", "consecutive_successful_launches": 3, "successful_launches": 4, "failed_launches": 1, "pending_launches": 0 }, { "id": 430, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/430/?format=api", "name": "Titan 403A", "description": "Titan IV was a family of heavy-lift space launch vehicles developed by Martin Marietta and operated by the United States Air Force from 1989 to 2005.", "family": "Titan", "full_name": "Titan 403A", "variant": "403A", "alias": "", "min_stage": 2, "max_stage": 2, "length": 54.0, "diameter": 3.05, "maiden_flight": "1991-03-08", "launch_mass": 906, "leo_capacity": 17700, "gto_capacity": null, "to_thrust": 14200, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": "", "wiki_url": "https://en.wikipedia.org/wiki/Titan_IV", "consecutive_successful_launches": 2, "successful_launches": 4, "failed_launches": 1, "pending_launches": 0 }, { "id": 431, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/431/?format=api", "name": "Titan 403B", "description": "Titan IV was a family of heavy-lift space launch vehicles developed by Martin Marietta and operated by the United States Air Force from 1989 to 2005.", "family": "Titan", "full_name": "Titan 403B", "variant": "403B", "alias": "", "min_stage": 2, "max_stage": 2, "length": 54.0, "diameter": 3.05, "maiden_flight": "2000-08-17", "launch_mass": 910, "leo_capacity": 21680, "gto_capacity": null, "to_thrust": 15000, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": "", "wiki_url": "https://en.wikipedia.org/wiki/Titan_IV", "consecutive_successful_launches": 1, "successful_launches": 1, "failed_launches": 0, "pending_launches": 0 }, { "id": 432, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/432/?format=api", "name": "Titan 404A", "description": "Titan IV was a family of heavy-lift space launch vehicles developed by Martin Marietta and operated by the United States Air Force from 1989 to 2005.", "family": "Titan", "full_name": "Titan 404A", "variant": "404A", "alias": "", "min_stage": 2, "max_stage": 2, "length": 54.0, "diameter": 3.05, "maiden_flight": "1992-11-28", "launch_mass": 906, "leo_capacity": 17700, "gto_capacity": null, "to_thrust": 14200, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": "", "wiki_url": "https://en.wikipedia.org/wiki/Titan_IV", "consecutive_successful_launches": 3, "successful_launches": 3, "failed_launches": 0, "pending_launches": 0 }, { "id": 433, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/433/?format=api", "name": "Titan 404B", "description": "Titan IV was a family of heavy-lift space launch vehicles developed by Martin Marietta and operated by the United States Air Force from 1989 to 2005.", "family": "Titan", "full_name": "Titan 404B", "variant": "404B", "alias": "", "min_stage": 2, "max_stage": 2, "length": 54.0, "diameter": 3.05, "maiden_flight": "1999-05-22", "launch_mass": 910, "leo_capacity": 21680, "gto_capacity": null, "to_thrust": 15000, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": "", "wiki_url": "https://en.wikipedia.org/wiki/Titan_IV", "consecutive_successful_launches": 3, "successful_launches": 3, "failed_launches": 0, "pending_launches": 0 }, { "id": 434, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/434/?format=api", "name": "Titan 405A", "description": "Titan IV was a family of heavy-lift space launch vehicles developed by Martin Marietta and operated by the United States Air Force from 1989 to 2005.", "family": "Titan", "full_name": "Titan 405A", "variant": "405A", "alias": "", "min_stage": 2, "max_stage": 2, "length": 54.0, "diameter": 3.05, "maiden_flight": "1990-06-08", "launch_mass": 906, "leo_capacity": 17700, "gto_capacity": null, "to_thrust": 14200, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": "", "wiki_url": "https://en.wikipedia.org/wiki/Titan_IV", "consecutive_successful_launches": 2, "successful_launches": 2, "failed_launches": 0, "pending_launches": 0 }, { "id": 435, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/435/?format=api", "name": "Titan 405B", "description": "Titan IV was a family of heavy-lift space launch vehicles developed by Martin Marietta and operated by the United States Air Force from 1989 to 2005.", "family": "Titan", "full_name": "Titan 405B", "variant": "405B", "alias": "", "min_stage": 2, "max_stage": 2, "length": 54.0, "diameter": 3.05, "maiden_flight": "2005-04-30", "launch_mass": 906, "leo_capacity": 14500, "gto_capacity": null, "to_thrust": 14200, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": "", "wiki_url": "https://en.wikipedia.org/wiki/Titan_IV", "consecutive_successful_launches": 1, "successful_launches": 1, "failed_launches": 0, "pending_launches": 0 }, { "id": 148, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/148/?format=api", "name": "Titan III", "description": "", "family": "Titan", "full_name": "Titan IIIE", "variant": "E", "alias": "", "min_stage": 3, "max_stage": 4, "length": 48.8, "diameter": 3.05, "maiden_flight": "1974-02-11", "launch_mass": 632, "leo_capacity": 15400, "gto_capacity": null, "to_thrust": 12991, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/titan2520iii_image_20190222030055.jpeg", "info_url": "https://archive.org/embed/gov.dod.dimoc.20693", "wiki_url": "https://en.wikipedia.org/wiki/Titan_IIIE", "consecutive_successful_launches": 6, "successful_launches": 6, "failed_launches": 1, "pending_launches": 0 }, { "id": 437, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/437/?format=api", "name": "Titan IIIA", "description": "The Titan IIIA or Titan 3A was an American expendable launch system, launched four times in 1964 and 1965,[1] to test the Transtage upper stage which was intended for use on the larger Titan IIIC. The Transtage was mounted atop two core stages derived from the Titan II. The Titan IIIA was also used as the core of the Titan IIIC.", "family": "Titan", "full_name": "Titan IIIA", "variant": "IIIA", "alias": "", "min_stage": 3, "max_stage": 3, "length": 42.0, "diameter": 3.05, "maiden_flight": "1964-09-01", "launch_mass": 161, "leo_capacity": 3100, "gto_capacity": null, "to_thrust": 1941, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": "", "wiki_url": "https://en.wikipedia.org/wiki/Titan_IIIA", "consecutive_successful_launches": 3, "successful_launches": 3, "failed_launches": 1, "pending_launches": 0 }, { "id": 438, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/438/?format=api", "name": "Titan IIIB", "description": "Titan IIIB was the collective name for a number of derivatives of the Titan II ICBM and Titan III launch vehicle, modified by the addition of an Agena upper stage. It consisted of four separate rockets. The Titan 23B was a basic Titan II with an Agena upper stage, and the Titan 24B was the same concept, but using the slightly enlarged Titan IIIM rocket as the base. The Titan 33B was a Titan 23B with the Agena (which had a smaller diameter than the Titan) enclosed in an enlarged fairing, in order to allow larger payloads to be launched. The final member of the Titan IIIB family was the Titan 34B which was a Titan 24B with the larger fairing used on the Titan 33B.", "family": "Titan", "full_name": "Titan IIIB", "variant": "IIIB", "alias": "", "min_stage": 3, "max_stage": 3, "length": 45.0, "diameter": 3.05, "maiden_flight": "1966-07-29", "launch_mass": 156, "leo_capacity": 3000, "gto_capacity": null, "to_thrust": 1913, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": "", "wiki_url": "https://en.wikipedia.org/wiki/Titan_IIIB", "consecutive_successful_launches": 17, "successful_launches": 21, "failed_launches": 1, "pending_launches": 0 }, { "id": 439, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/439/?format=api", "name": "Titan IIIC", "description": "The Titan IIIC was an expendable launch system used by the United States Air Force from 1965 until 1982. It was the first Titan booster to feature large solid rocket motors and was planned to be used as a launcher for the Dyna-Soar, though the spaceplane was cancelled before it could fly. The majority of the launcher's payloads were DoD satellites, for military communications and early warning, though one flight (ATS-6) was performed by NASA. The Titan IIIC was launched exclusively from Cape Canaveral while its sibling, the Titan IIID, was launched only from Vandenberg AFB.", "family": "Titan", "full_name": "Titan IIIC", "variant": "IIIC", "alias": "", "min_stage": 2, "max_stage": 3, "length": 42.0, "diameter": 3.0, "maiden_flight": "1965-06-18", "launch_mass": 626, "leo_capacity": 13100, "gto_capacity": 3000, "to_thrust": 10586, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": "", "wiki_url": "https://en.wikipedia.org/wiki/Titan_IIIC", "consecutive_successful_launches": 8, "successful_launches": 34, "failed_launches": 2, "pending_launches": 0 }, { "id": 440, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/440/?format=api", "name": "Titan IIID", "description": "The Titan IIID or Titan 3D was an American expendable launch system, part of the Titan rocket family. Titan IIID was flown 22 times with KH-9 and KH-11 satellites between 1971 and 1982, all successful launches.", "family": "Titan", "full_name": "Titan IIID", "variant": "IIID", "alias": "", "min_stage": 2, "max_stage": 2, "length": 36.0, "diameter": 3.05, "maiden_flight": "1971-06-15", "launch_mass": 612, "leo_capacity": 12300, "gto_capacity": null, "to_thrust": 10586, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": "", "wiki_url": "https://en.wikipedia.org/wiki/Titan_IIID", "consecutive_successful_launches": 22, "successful_launches": 22, "failed_launches": 0, "pending_launches": 0 }, { "id": 436, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/436/?format=api", "name": "Titan II SLV", "description": "The Titan 23G, Titan II(23)G, Titan 2(23)G or Titan II SLV was an American expendable launch system derived from the LGM-25C Titan II intercontinental ballistic missile. Retired Titan II missiles were converted by Martin Marietta, into which the Glenn L. Martin Company, which built the original Titan II, had merged. It was used to carry payloads for the United States Air Force, NASA and NOAA. Thirteen were launched from Space Launch Complex 4W at the Vandenberg Air Force Base between 1988 and 2003.", "family": "Titan", "full_name": "Titan II SLV", "variant": "23G", "alias": "", "min_stage": 2, "max_stage": 3, "length": 31.4, "diameter": 3.05, "maiden_flight": "1988-09-05", "launch_mass": 117, "leo_capacity": 3600, "gto_capacity": null, "to_thrust": 1900, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/titan_ii_slv_image_20231231110038.jpeg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Titan_23G", "consecutive_successful_launches": 9, "successful_launches": 12, "failed_launches": 1, "pending_launches": 0 }, { "id": 130, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/130/?format=api", "name": "Titan IVB", "description": "", "family": "Titan", "full_name": "Titan IVB/Centaur", "variant": "Centaur", "alias": "", "min_stage": null, "max_stage": null, "length": null, "diameter": null, "maiden_flight": "1997-10-15", "launch_mass": null, "leo_capacity": null, "gto_capacity": null, "to_thrust": null, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/titan2520ivb_image_20190222030244.jpeg", "info_url": "https://archive.org/embed/gov.dod.dimoc.20693", "wiki_url": "https://en.wikipedia.org/wiki/Titan_IV", "consecutive_successful_launches": 4, "successful_launches": 6, "failed_launches": 1, "pending_launches": 0 }, { "id": 449, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/449/?format=api", "name": "Vanguard", "description": "The Vanguard rocket was intended to be the first launch vehicle the United States would use to place a satellite into orbit. Instead, the Sputnik crisis caused by the surprise launch of Sputnik 1 led the U.S., after the failure of Vanguard TV3, to quickly orbit the Explorer 1 satellite using a Juno I rocket, making Vanguard I the second successful U.S. orbital launch.", "family": "", "full_name": "Vanguard", "variant": "", "alias": "", "min_stage": 3, "max_stage": 3, "length": 23.0, "diameter": 1.14, "maiden_flight": "1957-10-23", "launch_mass": 10, "leo_capacity": 9, "gto_capacity": null, "to_thrust": 123, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/vanguard_1_on_p_image_20240411114304.jpeg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Vanguard_(rocket)", "consecutive_successful_launches": 1, "successful_launches": 3, "failed_launches": 8, "pending_launches": 0 } ], "spacecraft_list": [] }
