The development and use of mathematical models of signals received through the multipath environmental of a TDRS-to-user spacecraft link and vice versa are discussed. The TDRS (tracking and data relay satellite) will be in synchronous orbit. The user spacecraft will be in a low altitude orbit between 200 and 4000 km.


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    Title :

    Multipath signal model development


    Contributors:

    Publication date :

    1970-11-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :


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