This paper presents viewgraphs on the development of a non-ablative thermal management coating used as the thermal protection system material for space shuttle rocket boosters and other launch vehicles. The topics include: (1) Coating Study; (2) Aerothermal Testing; (3) Preconditioning Environments; (4) Test Observations; (5) Lightning Strike Test Panel; (6) Test Panel After Impact Testing; (7) Thermal Testing; and (8) Mechanical Testing.


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    Titel :

    Thermal Management Coating as Thermal Protection System for Space Transportation System


    Beteiligte:
    R. Kaul (Autor:in) / C. I. Stuckey (Autor:in)

    Erscheinungsdatum :

    2002


    Format / Umfang :

    20 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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