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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Low Emissivity Coatings for Use at High Temperatures


    Contributors:

    Publication date :

    1960


    Size :

    11 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    High-Emissivity Coatings For High-Temperature Surfaces

    Deininger, William D. / King, David Q. | NTRS | 1988


    Emissivity data for metals at high temperatures

    BICE, V. / JACOBSON, D. | AIAA | 1985



    Emissivity Measurements on Space Relevant Coatings

    Zehnder, A. / Heidenreich, G. / Konter, J.A. et al. | SAE Technical Papers | 1992


    Emissivity Coatings for Low-Temperature Space Radiators

    G. R. Cunnington / J. R. Grammer / F. J. Smith | NTIS | 1969