The potential of zinc orthotitanate as a pigment for spacecraft thermal control was demonstrated. The properties and performance of pigments prepared by solid state, coprecipitation, and mixed oxalate methods were compared. Environmental tests and subsequent spectral analysis were given primary emphasis.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Development of space-stable thermal control coatings for use on large space vehicles


    Contributors:

    Publication date :

    1976-03-15


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English