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SPECIAL MESSAGE: GOES-East GOES-14 is providing GOES-East coverage. GOES-14 is stationary at 105 degrees West with no current plans to drift east. GOES-13 will remain in storage mode while the anomaly is being investigated. There is no estimate on return to operations at this time. More information: http://www.ssd.noaa.gov/PS/SATS/messages.html. |
The GOES I-M Sounder is a 19-channel radiometer that senses specific data parameters for atmospheric temperature and moisture profiles, surface and cloud top temperature, and ozone distribution. The atmospheric profiles that are produced are very similar to what has been achieved for decades using balloon-borne radiosondes. But the satellite Sounder system is able to achieve a greater number of profiles, and many more locations than is possible with a ground-based, balloon system.
The Sounder has 4 sets of detectors (visible, long wave IR, medium wave IR, short wave IR). The incoming radiation passes through a set of filters before reaching the detectors. The filters are mounted on a rotating (28.2 cm) wheel containing 18 filter windows, divided into 3 concentric rings, one for each IR detector group. The outer ring contains 7 long wave filters, the middle ring 6 short wave filters, and the inner ring 5 medium wave channels. The visible wave lengths do not pass through a filter. Approximately one-fourth of the wheel has no filters. While this "dead zone" is rotating in front of the detectors, the scanning mirror is stepped to the next location then stopped while the channels are sampled. The mirror scanning sequence takes places by sweeping in an East-West direction, stepping in the North-South direction, than sweeping back in a West-East direction, stepping North-South, sweeping East-West, and so on, similar to the Imager.
The Sounder consists of electronics, power supply, and sensor modules. The sensor module containing the telescope, scan assembly, and detectors, is mounted on a baseplate outside the main structure of the spacecraft, together with shields and louvers for thermal control. The electronics and power supply modules are mounted inside the spacecraft on the internal equipment panel.
| Sounder Instrument Characteristics (GOES I-M) | ||
| Channel Numbers | Wavelength (um) | Maximum Temperature Range (K) |
| Long wave IR 1 2 3 4 5 6 7 |
14.71 14.37 14.06 13.64 13.37 12.66 12.02 |
space - 280 space - 280 space - 290 space - 310 space - 320 space - 330 space - 340 |
| Medium wave IR 8 9 10 11 12 |
11.03 9.71 7.43 7.02 6.51 |
space - 345 space - 330 space - 310 space - 295 space - 290 |
| Short wave IR 13 14 15 6 17 18 |
4.57 4.52 4.45 4.13 3.98 3.74 |
space - 320 space - 310 space - 295 space - 340 space - 345 space - 345 |
| Visible 19 | 0.70 | Not Applicable |
| Nominal Circular Field of View (IGFOV) | 242 urad for all channels | |
| Radiometric calibration | Space and 300 K infrared internal backbody | |
| Calibration frequency | Space: 2 minutes typical Infrared: 30 minutes typical |
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| System absolute accuracy | IR channels: less than or equal to 1 K Visible channel: 5% of maximum scene irradiance |
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| Sounding rate | 3000 by 3000 km, less than or equal to 42 minutes | |
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Satellite Products and Services Division Direct Services Branch Phone: 301-817-4521/4523 Fax: 301-817-3904 |
Mailing Address: NSOF (E/SPO53) 1315 East-West Hwy Silver Spring, MD 20910-3282 USA |