Presents a design to develop a Compact Coherent Laser Ranging with the following goals: Match the performance as GRACE-FO, with much reduced SWaP to fit on mini-Sat or CubeSat; Enables low cost and more frequent LL-SST gravitational missions; Immunes from ionosphere propagation delay with optical ranging; Increases the body pointing capability due to small satellite.


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    Title :

    Compact Coherent Laser Ranging (CCLR)


    Contributors:
    Yang, Guangning (author) / Chen, Jeffrey (author) / Numata, Kenji (author) / Luthcke, Scott (author) / Yu, Tony (author)

    Publication date :

    2019-07-31


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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