The high velocities of aerospace vehicles causes them to attain high skin temperatures both within the earth's atmosphere and upon reentry into the atmosphere. Furthermore, outside the earth's atmosphere, the operating temperatures of propulsion systems generate heat. The results of this heat generated by flight is to place strenuous temperature requirements upon materials which are used for instruments housed within a space vehicle. A problem then exists of how to prevent heat transfer from hot components of an aerospace vehicle to instrument systems within the vehicle.


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    Titel :

    Low Emissivity Coatings for Use at High Temperatures


    Beteiligte:
    B. A. Macklin (Autor:in) / J. C. Withers (Autor:in)

    Erscheinungsdatum :

    1960


    Format / Umfang :

    11 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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