Initial objectives of this work were to develop a high temperature resistant material capable of withstanding rocket nozzle throat, leading edge, or re-entry environments by virtue of its high temperature strength, resistance to oxidation, and ability to cool itself ablatively. (Author)


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    Title :

    High Viscosity Thermal Protection Materials


    Contributors:
    R. E. Wilson (author) / F. J. Koubek (author)

    Publication date :

    1969


    Size :

    63 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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