{
  "HAPI": "3.2",
  "x_description": "This dataset summarizes the individual thrusters usage for all manoeuvres conducted during the lifetime of the mission and provides an overall manoeuvres history. From the burn duration of each thruster the amount of propellant used can be calculated. This could be of interest if the amount of exhaust could influence the instrument performance.",
  "cadence": "PT86400.000000S",
  "parameters": [
    {
      "type": "isotime",
      "x_type": "ISO_TIME_RANGE",
      "units": "UTC",
      "name": "Time_tags",
      "description": "Universal time range",
      "label": "Universal time range",
      "length": 25,
      "fill": null
    },
    {
      "type": "isotime",
      "x_type": "ISO_TIME_RANGE",
      "units": "UTC",
      "name": "Time_tags_stop",
      "length": 25,
      "fill": null
    },
    {
      "type": "double",
      "name": "RPM",
      "description": "Spacecraft spin rate at the start and end of the thruster usage",
      "label": "Spacecraft spin rate",
      "units": "rpm",
      "fill": "-1e+31",
      "size": [
        2
      ]
    },
    {
      "type": "double",
      "name": "SAA",
      "description": "Solar Aspect Angle at the start and end of the thruster usage",
      "label": "Solar Aspect Angle",
      "units": "deg",
      "fill": "-1e+31",
      "size": [
        2
      ]
    },
    {
      "type": "double",
      "name": "He_T",
      "description": "Helium tank temperature at the start and end of the thruster usage",
      "label": "Helium tank temperature",
      "units": "Celsius",
      "fill": "-1e+31",
      "size": [
        2
      ]
    },
    {
      "type": "double",
      "name": "He_P",
      "description": "Helium tank pressure at the start and end of the thruster usage",
      "label": "Helium tank pressure",
      "units": "bar",
      "fill": "-1e+31",
      "size": [
        2
      ]
    },
    {
      "type": "double",
      "name": "MMH_T",
      "description": "MMH (Monomethylhydrazine) tank temperature at the start and end of the thruster usage",
      "label": "MMH tank temperature",
      "units": "Celsius",
      "fill": "-1e+31",
      "size": [
        2
      ]
    },
    {
      "type": "double",
      "name": "MMH_P",
      "description": "MMH (Monomethylhydrazine) tank pressure at the start and end of the thruster usage",
      "label": "MMH tank pressure",
      "units": "bar",
      "fill": "-1e+31",
      "size": [
        2
      ]
    },
    {
      "type": "double",
      "name": "MON_T",
      "description": "MON (Dinitrogentetraoxide) tank temperature at the start and end of the thruster usage",
      "label": "MON tank temperature",
      "units": "Celsius",
      "fill": "-1e+31",
      "size": [
        2
      ]
    },
    {
      "type": "double",
      "name": "MON_P",
      "description": "MON (Dinitrogentetraoxide) tank pressure at the start and end of the thruster usage",
      "label": "MON tank pressure",
      "units": "bar",
      "fill": "-1e+31",
      "size": [
        2
      ]
    },
    {
      "type": "double",
      "name": "MMH_M",
      "description": "MMH (Monomethylhydrazine) tank fuel mass at the start and end of the thruster usage",
      "label": "MMH fuel mass",
      "units": "kg",
      "fill": "-1e+31",
      "size": [
        2
      ]
    },
    {
      "type": "double",
      "name": "MOM_M",
      "description": "MON (Dinitrogentetraoxide) tank  fuel mass at the start and end of the thruster usage",
      "label": "MON fuel mass",
      "units": "kg",
      "fill": "-1e+31",
      "size": [
        2
      ]
    },
    {
      "type": "integer",
      "name": "Selection",
      "description": "Thruster selection (th1_A, th1_B, th2_A, th2_B, th3_A, th3_B, th4_A, th4_B)",
      "label": "selected thrusters",
      "units": null,
      "fill": "-1",
      "size": [
        8
      ]
    },
    {
      "type": "integer",
      "name": "Pulse",
      "description": "Pulse mode selection (th1, th2. th3, th4)",
      "label": "pulse mode selection",
      "units": null,
      "fill": "-1",
      "size": [
        4
      ]
    },
    {
      "type": "integer",
      "name": "Duration",
      "description": "Manoeuvre duration (thrusters or main engine) (th1, th2, th3, th4, me), where me=main engine",
      "label": "Manoeuvre duration",
      "units": null,
      "fill": "-1",
      "size": [
        5
      ]
    },
    {
      "type": "double",
      "name": "Parameters",
      "description": "Thrusters firing parameters (start phase for th1, th2. th3, th4; pulse length for  th1, th2. th3, th4)",
      "label": "pulse mode selection",
      "units": null,
      "fill": "-1e+31",
      "size": [
        8
      ]
    }
  ],
  "startDate": "2000-07-16T18:00Z",
  "stopDate": "2024-11-15T14:00Z",
  "x_tap_url": "https://csa.esac.esa.int/csa-sl-tap/data?retrieval_type=HEADER&DATASET_ID=C1_CT_AUX_ESOC_THRUSTER&FORCEPACK=false",
  "sampleStartDate": "2022-02-10T12:00Z",
  "sampleStopDate": "2022-02-10T13:00Z",
  "x_tap_data_url": "https://csa.esac.esa.int/csa-sl-tap/data?RETRIEVAL_TYPE=product&RETRIEVAL_ACCESS=streamed&DATASET_ID=C1_CT_AUX_ESOC_THRUSTER&START_DATE=2022-02-10T12:00:00.000Z&END_DATE=2022-02-10T13:00:00.000Z",
  "status": {
    "code": 1200,
    "message": "OK"
  },
  "x_LastUpdate": "2026-03-30T15:22:32Z",
  "x_LastUpdateAttempt": "2026-04-12T15:17:05Z",
  "x_LastUpdateError": "No parameters node in JSON response."
}