{ "rocket": { "id": "c872b8a9-b034-4482-96df-0ea712929da8", "name": "Atlas V", "slug": "atlas-v", "live": true, "description": "Atlas V (\"V\" is pronounced \"Five\") is an expendable launch system in the Atlas rocket family. It was formerly operated by Lockheed Martin and is now operated by United Launch Alliance (ULA), a joint venture with Boeing. Each Atlas V rocket uses a Russian-built RD-180 engine burning kerosene and liquid oxygen to power its first stage and an American-built RL10 engine burning liquid hydrogen and liquid oxygen to power its Centaur upper stage. The RD-180 engines are provided by RD Amross, while Aerojet Rocketdyne provides both the RL10 engines and the strap-on boosters used in some configurations. The standard payload fairing sizes are 4 or 5 meters in diameter and of various lengths. Fairings sizes as large as 7.2 m in diameter and up to 32.3 m in length have been considered.[5] The rocket is assembled in Decatur, Alabama and Harlingen, Texas.", "used_for": "EELV/medium-heavy launch vehicle", "manned": false, "status": "Active", "built_by": [ { "name": "United Launch Alliance", "link": "https://en.wikipedia.org/wiki/United_Launch_Alliance", "etc": null } ], "built_for": [], "project_cost": { "value": 0, "unit": "" }, "launch_cost": { "value": 0, "unit": "" }, "country": "USA", "first_launch": "2002-08-21T00:00:00+00:00", "last_launch": "2023-09-10T00:00:00+00:00", "launches": 98, "successes": 98, "failures": 0, "success_rate": 100, "height": { "value": 58.3, "unit": "m" }, "diameter": { "value": 3.81, "unit": "m" }, "mass": { "value": 334500, "unit": "kg" }, "payload": [ { "destination": "LEO", "orbital_inclination": 28.7, "mass": null }, { "destination": "GTO", "orbital_inclination": null, "mass": null } ], "stages": 2, "engines": [ { "stage": "1", "name": "Atlas CCB", "link": "https://en.wikipedia.org/wiki/Common_Core_Booster", "height": null, "diameter": null, "thrust": null, "specific_impluse": null, "burn_time": null, "propellant": null, "mass": { "empty": null, "gross": null, "propellant": null } }, { "stage": "2", "name": "", "link": "", "height": null, "diameter": null, "thrust": null, "specific_impluse": null, "burn_time": null, "propellant": null, "mass": { "empty": null, "gross": null, "propellant": null } } ], "thrust": [ { "stage": "1", "value": 3827, "unit": "kN (Sea Level)" } ], "specific_impulse": [], "burn_time": [], "fuel": [ { "stage": "1", "name": "Liquid oxygen", "link": "https://en.wikipedia.org/wiki/LOX" }, { "stage": "1", "name": "Refined Petroleum-1", "link": "https://en.wikipedia.org/wiki/RP-1" } ], "links": [], "images": { "vector": "/xplr/rockets/atlas-v.svg", "silhouette": "/xplr/rockets/atlas-v-silo.svg", "flag": "/xplr/flags/usa.svg", "launch": "/xplr/rockets/atlas-v-launch.jpg", "etc": null, "height": 233 }, "cargo": [], "_version": 13 } }