@prefix ns0: . @prefix skos: . ns0:altLabel [ ] ; skos:definition """[Source: National Space Science Data Center, http://nssdc.gsfc.nasa.gov/nmc/experimentDisplay.do?id=1972-089A-01 ] The four-channel scanning radiometer, designated the sensor AVE (Aerospace Vehicle Electronics) package (SAP), was the primary experiment on the DMSP spacecraft. The purpose of this experiment was to provide global, day/night observations of cloudcover and cloud temperature measurements to support Department of Defense requirements for operational weather analysis and forecasting. The radiometer operated in two spectral intervals -- (1) visible and near infrared (0.4 to 1.1 micrometers) and (2) infrared (8 to 13 micrometers). The three-channel radiometer was essentially two scanning radiometers driven by a common motor. One radiometer provided high resolution (HR) visual and infrared (IR) data with nadir resolutions of 3.7 and 4.4 km, respectively. The other radiometer produced very high resolution (VHR) visual and infrared (WHR) data with nadir resolutions of .63 km and .67 km, respectively. On board recorders had a storage capacity of 210 min of both HR and IR data and a total of 20 min of VHR and WHR data. For direct readout to tactical sites, the experiment was programmed so that VHR and IR data were obtained during the daytime and HR and WHR data were obtained at night. The infrared channels (WHR and IR) covered a temperature range of 210 to 310 deg k with an accuracy of 1 deg c. Electronic circuitry in the sensor converted the sensed infrared energy directly into equivalent black body temperature (as opposed to radiance) prior to transmission to ground sites. The HR channel included a zero resolution sensor which measured solar input and was used to control channel gain, thereby producing an output signal that represents scene albedo. This feature also made it possible to obtain useful visual data at night. The sensor incorporated sunshades and glare suppression devices in conjunction with a long-scan automatic gain control which allowed the HR channel to provide usable data through the day/night terminator. Identical experiments were flown on all DMSP Block 5 spacecraft to date. Group: Instrument_Details Entry_ID: SR Group: Instrument_Identification Instrument_Category: Earth Remote Sensing Instruments Instrument_Class: Passive Remote Sensing Instrument_Type: Spectrometers/Radiometers Instrument_Subtype: Imaging Spectrometers/Radiometers Short_Name: SR Long_Name: Scanning Radiometer End_Group Group: Associated_Platforms Short_Name: DMSP 5B/F3 End_Group Group: Spectral_Frequency_Information Wavelength_Keyword: Visible Spectral_Frequency_Coverage_Range: 0.4 μm - 1.1 μm End_Group Group: Spectral_Frequency_Information Wavelength_Keyword: Near Infrared Spectral_Frequency_Coverage_Range: 0.4 μm - 1.1 μm End_Group Group: Spectral_Frequency_Information Wavelength_Keyword: Infrared > Thermal Spectral_Frequency_Coverage_Range: 8 μm to 13 μm End_Group Online_Resource: http://nssdc.gsfc.nasa.gov/nmc/experimentDisplay.do?id=1972-089A-01 End_Group"""@en ; skos:prefLabel "SR"@en ; skos:inScheme ; skos:broader ; a skos:Concept . skos:prefLabel "Imaging Spectrometers/Radiometers"@en ; a skos:Concept ; skos:narrower .