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    Title :

    FINITE ELEMENT METHOD FOR ABLATIVE THERMAL PROTECTION SYSTEMS DESIGN FOR ATMOSPHERIC RE-ENTRY VEHICLES (AIAA 2018-5207)


    Contributors:

    Conference:

    AIAA International Space Planes and Hypersonic Systems and Technolgies (Conference)



    Publication date :

    2018-01-01


    Size :

    8 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English



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