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Poster Sessions
  • Session 1
  • Session 2
  • Session 3
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  • Session 5
  • Session 6



  • ACRS 1999


    Poster Session 6
    The FY-1C Meteorological Satellite and Its Remote Sensor

    Operation in orbit
    The FY-1C satellite was launched into the predetermined orbit at 09:45 am on May 10th, 1999, and the scanning radiometer began to operate at 11:16 am, the ground station received the image signals from four visible bands, three near infrared bands and one short wavelength infrared band at once. The radiant cooler began to cool on June 9th after the heating for outgassing for about one month. On June 10th, the temperature of the cooler's patch reached 105 K, three infrared channels were switched on, all of ten channels of the scanning radiometer operated. The image data of FY-1C satellite are being applied in weather forecast, flood monitoring, vegetation index estimation, observation of ocean chlorophyll and suspended sediment and monitoring of the global weather and ocean temperature and etc.

    Table 2. Main specifications of the 
    10-channel scanning radiometer
    Parameters Measured specifications
    IFOV1.26mr
    Ground resolution of image 1.1 km
    Swath width 3100 km
    Effective view angle±55.4°
    Scanning rate 360 rpm
    Number of detecting channels 10
    Detectors Si (channels 1, 2, 7, 8, 9, 10)
    HgCdTe (channels 6, operating at room temperature)
    Cooling method Radiant cooling, 105 K
    Detection sensitivity NED r£3×10-4 (channels 1, 2, 7, 8, 9, 10)
    NED r£1×10 -3 (channel 6)
    NEDT£0.27K(channel 3)
    NEDT£0.25K(channel 4, 5)
    Radiation calibration accuracy Better than 10% for visible and IR channels;
    1.0 K for IR channels
    Data quantization 10 bit
    Data rate1.3308 Mbps
    Weight 53.5 Kg
    Power consumption 43.5 W

    Up to now, the FY-1C satellite has been operating normally in orbit for more than four months. We hope it to continue its stable operation so as to reach its expected lifetime of two years.

    In 2001, China will launch its meteorological satellite FY-1D to replace the FY-1C satellite.

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