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  • Snow Water Equivalent Altimetry Mission: Enabling Direct Measurement of SWE on Sea Ice and Land in the Cryosphere

    Paper number

    IAC-17,E2,3-GTS.4,1,x41599

    Author

    Mr. Toby Mould, European Space Agency (ESA), United Kingdom

    Coauthor

    Mr. Dries Agten, Thales Alenia Space, Belgium

    Coauthor

    Mr. Harm-Jan Benninga, University of Twente, The Netherlands

    Coauthor

    Ms. Marie Henriksen, Norwegian University of Science and Technology, Norway

    Coauthor

    Mr. Stefano Marinaci, Università del Salento, Italy

    Coauthor

    Mr. Jorge Bordalo Monteiro, University of Beira Interior, Portugal

    Coauthor

    Mrs. Caroline Schrenker, University of Erlangen, Germany

    Coauthor

    Mr. Carlos Diaz Schümmer, Universidad Politécnica de Madrid, Spain

    Coauthor

    Ms. Kerstin Schulze, Germany

    Coauthor

    Mr. Alexandre Hippert Ferrer, Université Paris Diderot (Paris 7), France

    Coauthor

    Ms. Stephanie Rošker, TU Graz, Austria

    Coauthor

    Mr. Georg Fischer, German Aerospace Center (DLR), Germany

    Coauthor

    Ms. Julia Donnerer, Austria

    Year

    2017

    Abstract
    To study the temporal and spatial dynamics of the global water cycle, satellite and airborne remote sensing missions are essential for discovering specific patterns within the cryosphere over an extensive area within short time periods. However, measurements of true water inventories stored in sea, lake and land ice have been significantly hindered by uncertainties introduced by snow cover for the last 40 years of satellite missions. Current estimations of hydrological and climate models, Earth’s energy balance (albedo) calculations and flood predictions suffer from inaccuracies due to an inability to accurately determine the water content of snow cover.
    
    The Snow Water Equivalent Altimetry mission concept has been developed to address this fundamental issue, enabling direct measurement of surface Snow Water Equivalent (SWE) on sea ice and land at latitudes above 60 degrees and below -60 degrees. In order to achieve this, the proposed mission will implement a novel combination of Ka- and Ku-band radar altimeters (active microwave sensors), capable of penetrating into the snow microstructure. There are no other satellite missions currently capable of directly measuring SWE.
    
    The Ka-band altimeter (wavelength 0.8 cm) provides a low maximum snow pack penetration depth of up to 20 cm for dry snow, since the volume scattering of snow dominates over the scattering caused by the underlying ice or land surface. In contrast, the Ku-band altimeter (wavelength 2 cm) provides a high maximum snowpack penetration depth of up to 15 m in high latitudes regions with dry snow, as volume scattering is decreased by more than one order of magnitude compared to Ka-band. The combined difference in Ka- and Ku-band signal penetration results will provide a direct and more accurate determination of SWE. As a result, global SWE estimations interpreted from passive microwave products and the reliability of numerical snow and climate models will be advanced.
    
    The spacecraft would be launched into a 90 degree polar orbit with a 3 days revisit time in order to fulfill the priority scientific requirement of having the highest temporal resolution in the polar regions. This will enable a detailed study of these remote areas by providing a 3 day maximum revisit time. The spacecraft would be of about 850 kg and could be transported by the Vega Launcher into a 761 km orbit allowing the sharing of the launch price.
    Abstract document

    IAC-17,E2,3-GTS.4,1,x41599.brief.pdf

    Manuscript document

    IAC-17,E2,3-GTS.4,1,x41599.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.