This presentation discusses ground based proof of concept hardware under development at NASA GSFC to address high heat flux thermal management in silicon substrates. The goal is to develop proof of concept hardware for space flight validation. The space flight hardware will provide gravity insensitive thermal management for electronics applications such as transmit receive modules that are severely limited by thermal concerns.


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    Title :

    Micro- and Nano-Scale Electrically Driven Two-Phase Thermal Management


    Contributors:

    Conference:

    Spacecraft Thermal Control Workshop ; 2016 ; El Segundo, CA, United States


    Publication date :

    2016-03-21


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English





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