mirrored_repositories/Launch-Tracker-SpaceX/test
class TestRocketObj {
  static String rocketJson = '''[
        {
    "height": {
      "meters": 22.25,
      "feet": 73
    },
    "diameter": {
      "meters": 1.68,
      "feet": 5.5
    },
    "mass": {
      "kg": 30146,
      "lb": 66460
    },
    "first_stage": {
      "thrust_sea_level": {
        "kN": 420,
        "lbf": 94000
      },
      "thrust_vacuum": {
        "kN": 480,
        "lbf": 110000
      },
      "reusable": false,
      "engines": 1,
      "fuel_amount_tons": 44.3,
      "burn_time_sec": 169
    },
    "second_stage": {
      "thrust": {
        "kN": 31,
        "lbf": 7000
      },
      "payloads": {
        "composite_fairing": {
          "height": {
            "meters": 3.5,
            "feet": 11.5
          },
          "diameter": {
            "meters": 1.5,
            "feet": 4.9
          }
        },
        "option_1": "composite fairing"
      },
      "reusable": false,
      "engines": 1,
      "fuel_amount_tons": 3.38,
      "burn_time_sec": 378
    },
    "engines": {
      "isp": {
        "sea_level": 267,
        "vacuum": 304
      },
      "thrust_sea_level": {
        "kN": 420,
        "lbf": 94000
      },
      "thrust_vacuum": {
        "kN": 480,
        "lbf": 110000
      },
      "number": 1,
      "type": "merlin",
      "version": "1C",
      "layout": "single",
      "engine_loss_max": 0,
      "propellant_1": "liquid oxygen",
      "propellant_2": "RP-1 kerosene",
      "thrust_to_weight": 96
    },
    "landing_legs": {
      "number": 0,
      "material": null
    },
    "payload_weights": [
      {
        "id": "leo",
        "name": "Low Earth Orbit",
        "kg": 450,
        "lb": 992
      }
    ],
    "flickr_images": [
      "https://imgur.com/DaCfMsj.jpg",
      "https://imgur.com/azYafd8.jpg"
    ],
    "name": "Falcon 1",
    "type": "rocket",
    "active": false,
    "stages": 2,
    "boosters": 0,
    "cost_per_launch": 6700000,
    "success_rate_pct": 40,
    "first_flight": "2006-03-24",
    "country": "Republic of the Marshall Islands",
    "company": "SpaceX",
    "wikipedia": "https://en.wikipedia.org/wiki/Falcon_1",
    "description": "The Falcon 1 was an expendable launch system privately developed and manufactured by SpaceX during 2006-2009. On 28 September 2008, Falcon 1 became the first privately-developed liquid-fuel launch vehicle to go into orbit around the Earth.",
    "id": "5e9d0d95eda69955f709d1eb"
  },
  {
    "height": {
      "meters": 70,
      "feet": 229.6
    },
    "diameter": {
      "meters": 3.7,
      "feet": 12
    },
    "mass": {
      "kg": 549054,
      "lb": 1207920
    },
    "first_stage": {
      "thrust_sea_level": {
        "kN": 7607,
        "lbf": 1710000
      },
      "thrust_vacuum": {
        "kN": 8227,
        "lbf": 1849500
      },
      "reusable": true,
      "engines": 9,
      "fuel_amount_tons": 385,
      "burn_time_sec": 162
    },
    "second_stage": {
      "thrust": {
        "kN": 934,
        "lbf": 210000
      },
      "payloads": {
        "composite_fairing": {
          "height": {
            "meters": 13.1,
            "feet": 43
          },
          "diameter": {
            "meters": 5.2,
            "feet": 17.1
          }
        },
        "option_1": "dragon"
      },
      "reusable": false,
      "engines": 1,
      "fuel_amount_tons": 90,
      "burn_time_sec": 397
    },
    "engines": {
      "isp": {
        "sea_level": 288,
        "vacuum": 312
      },
      "thrust_sea_level": {
        "kN": 845,
        "lbf": 190000
      },
      "thrust_vacuum": {
        "kN": 914,
        "lbf": 205500
      },
      "number": 9,
      "type": "merlin",
      "version": "1D+",
      "layout": "octaweb",
      "engine_loss_max": 2,
      "propellant_1": "liquid oxygen",
      "propellant_2": "RP-1 kerosene",
      "thrust_to_weight": 180.1
    },
    "landing_legs": {
      "number": 4,
      "material": "carbon fiber"
    },
    "payload_weights": [
      {
        "id": "leo",
        "name": "Low Earth Orbit",
        "kg": 22800,
        "lb": 50265
      },
      {
        "id": "gto",
        "name": "Geosynchronous Transfer Orbit",
        "kg": 8300,
        "lb": 18300
      },
      {
        "id": "mars",
        "name": "Mars Orbit",
        "kg": 4020,
        "lb": 8860
      }
    ],
    "flickr_images": [
      "https://farm1.staticflickr.com/929/28787338307_3453a11a77_b.jpg",
      "https://farm4.staticflickr.com/3955/32915197674_eee74d81bb_b.jpg",
      "https://farm1.staticflickr.com/293/32312415025_6841e30bf1_b.jpg",
      "https://farm1.staticflickr.com/623/23660653516_5b6cb301d1_b.jpg",
      "https://farm6.staticflickr.com/5518/31579784413_d853331601_b.jpg",
      "https://farm1.staticflickr.com/745/32394687645_a9c54a34ef_b.jpg"
    ],
    "name": "Falcon 9",
    "type": "rocket",
    "active": true,
    "stages": 2,
    "boosters": 0,
    "cost_per_launch": 50000000,
    "success_rate_pct": 97,
    "first_flight": "2010-06-04",
    "country": "United States",
    "company": "SpaceX",
    "wikipedia": "https://en.wikipedia.org/wiki/Falcon_9",
    "description": "Falcon 9 is a two-stage rocket designed and manufactured by SpaceX for the reliable and safe transport of satellites and the Dragon spacecraft into orbit.",
    "id": "5e9d0d95eda69973a809d1ec"
  }
        ]''';
}
