YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • AMS
    • Journal of Atmospheric and Oceanic Technology
    • View Item
    •   YE&T Library
    • AMS
    • Journal of Atmospheric and Oceanic Technology
    • View Item
    • All Fields
    • Source Title
    • Year
    • Publisher
    • Title
    • Subject
    • Author
    • DOI
    • ISBN
    Advanced Search
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Archive

    A Blackbody Design for SI-Traceable Radiometry for Earth Observation

    Source: Journal of Atmospheric and Oceanic Technology:;2008:;volume( 025 ):;issue: 011::page 2046
    Author:
    Gero, P. Jonathan
    ,
    Dykema, John A.
    ,
    Anderson, James G.
    DOI: 10.1175/2008JTECHA1100.1
    Publisher: American Meteorological Society
    Abstract: Spaceborne measurements pinned to international standards are needed to monitor the earth?s climate, quantify human influence thereon, and test forecasts of future climate change. The International System of Units (SI, from the French for Système International d?Unités) provides ideal measurement standards for radiometry as they can be realized anywhere, at any time in the future. The challenge is to credibly prove on-orbit accuracy at a claimed level against these international standards. The most accurate measurements of thermal infrared spectra are achieved with blackbody-based calibration. Thus, SI-traceability is obtained through the kelvin scale, making thermometry the foundation for on-orbit SI-traceable spectral infrared measurements. Thermodynamic phase transitions are well established as reproducible temperature standards and form the basis of the international practical temperature scale (International Temperature Scale of 1990, ITS-90). Appropriate phase transitions are known in the temperature range relevant to thermal infrared earth observation (190?330 K) that can be packaged such that they are chemically stable over the lifetime of a space mission, providing robust and traceable temperature calibrations. A prototype blackbody is presented that is compact, highly emissive, thermally stable and homogeneous, and incorporates a small gallium melting point cell. Precision thermal control of the blackbody allows the phase transition to be identified to within 5 mK. Based on these results, the viability of end-to-end thermometric calibration of both single-temperature and variable-temperature blackbodies on orbit by employing multiple-phase-change cells was demonstrated.
    • Download: (526.2Kb)
    • Show Full MetaData Hide Full MetaData
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      A Blackbody Design for SI-Traceable Radiometry for Earth Observation

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4209125
    Collections
    • Journal of Atmospheric and Oceanic Technology

    Show full item record

    contributor authorGero, P. Jonathan
    contributor authorDykema, John A.
    contributor authorAnderson, James G.
    date accessioned2017-06-09T16:25:35Z
    date available2017-06-09T16:25:35Z
    date copyright2008/11/01
    date issued2008
    identifier issn0739-0572
    identifier otherams-67654.pdf
    identifier urihttp://onlinelibrary.yabesh.ir/handle/yetl/4209125
    description abstractSpaceborne measurements pinned to international standards are needed to monitor the earth?s climate, quantify human influence thereon, and test forecasts of future climate change. The International System of Units (SI, from the French for Système International d?Unités) provides ideal measurement standards for radiometry as they can be realized anywhere, at any time in the future. The challenge is to credibly prove on-orbit accuracy at a claimed level against these international standards. The most accurate measurements of thermal infrared spectra are achieved with blackbody-based calibration. Thus, SI-traceability is obtained through the kelvin scale, making thermometry the foundation for on-orbit SI-traceable spectral infrared measurements. Thermodynamic phase transitions are well established as reproducible temperature standards and form the basis of the international practical temperature scale (International Temperature Scale of 1990, ITS-90). Appropriate phase transitions are known in the temperature range relevant to thermal infrared earth observation (190?330 K) that can be packaged such that they are chemically stable over the lifetime of a space mission, providing robust and traceable temperature calibrations. A prototype blackbody is presented that is compact, highly emissive, thermally stable and homogeneous, and incorporates a small gallium melting point cell. Precision thermal control of the blackbody allows the phase transition to be identified to within 5 mK. Based on these results, the viability of end-to-end thermometric calibration of both single-temperature and variable-temperature blackbodies on orbit by employing multiple-phase-change cells was demonstrated.
    publisherAmerican Meteorological Society
    titleA Blackbody Design for SI-Traceable Radiometry for Earth Observation
    typeJournal Paper
    journal volume25
    journal issue11
    journal titleJournal of Atmospheric and Oceanic Technology
    identifier doi10.1175/2008JTECHA1100.1
    journal fristpage2046
    journal lastpage2054
    treeJournal of Atmospheric and Oceanic Technology:;2008:;volume( 025 ):;issue: 011
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian