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    Titel :

    Novel Hybrid Ablative/Ceramic Development for Re-Entry in Planetary Atmospheric Thermal Protection: Interfacial Adhesive Selection and Test Verification Plan


    Beteiligte:

    Kongress:

    19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference



    Erscheinungsdatum :

    2014-01-01



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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