{
  "rocket": {
    "id": "19",
    "name": "Angara A5",
    "slug": "angara-a5",
    "live": true,
    "description": "The Angara rocket family is a family of space-launch vehicles being developed by the Moscow-based Khrunichev State Research and Production Space Center. The rockets are to put between 3,800 and 24,500 kg into low Earth orbit and are intended, along with Soyuz-2 variants, to replace several existing launch vehicles. The second Angara developed was the Angara A5 heavy lift launch vehicle, which consists of one URM-1 core and four URM-1 boosters, a 3.6m URM-2 second stage, and an upper stage, either the Briz-M or the KVTK.[14] Weighing 773 tonnes at lift-off, Angara A5 has a payload capacity of 24.5 tonnes to a 200 km x 60° orbit. Angara A5 is able to deliver 5.4 tonnes to GTO with Briz-M, or 7.5 tonnes to the same orbit with KVTK.[20]",
    "used_for": "heavy lift launch vehicle",
    "manned": false,
    "status": "Active",
    "built_by": [
      {
        "name": "Khrunichev",
        "link": "https://en.wikipedia.org/wiki/Khrunichev_State_Research_and_Production_Space_Center",
        "etc": null
      }
    ],
    "built_for": [],
    "project_cost": {
      "value": 0,
      "unit": ""
    },
    "launch_cost": {
      "value": 0,
      "unit": ""
    },
    "country": "RUSSIA",
    "first_launch": "2014-12-23T00:00:00+00:00",
    "last_launch": "2014-12-23T00:00:00+00:00",
    "launches": 1,
    "successes": 1,
    "failures": 0,
    "success_rate": 100,
    "height": {
      "value": 64,
      "unit": "m"
    },
    "diameter": {
      "value": 8.86,
      "unit": "m"
    },
    "mass": {
      "value": 790000,
      "unit": "kg"
    },
    "payload": [
      {
        "destination": null,
        "orbital_inclination": null,
        "mass": null
      },
      {
        "destination": null,
        "orbital_inclination": null,
        "mass": null
      }
    ],
    "stages": null,
    "engines": [
      {
        "stage": "1",
        "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": 0,
        "unit": "kN"
      }
    ],
    "specific_impulse": [
      {
        "stage": "1",
        "value": 0,
        "unit": "sec"
      }
    ],
    "burn_time": [
      {
        "stage": "1",
        "value": 0,
        "unit": "seconds"
      }
    ],
    "fuel": [
      {
        "stage": "1",
        "name": "",
        "link": ""
      }
    ],
    "links": [],
    "images": {
      "vector": "/xplr/rockets/angara-a5.svg",
      "silhouette": "/xplr/rockets/angara-a5.svg",
      "flag": "/xplr/flags/rus.svg",
      "launch": "/xplr/rockets/angara-a5-launch.jpg",
      "etc": null,
      "height": 256
    },
    "cargo": [],
    "_version": 4
  }
}