{
  "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
  }
}