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.


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    Titel :

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


    Beteiligte:
    Gilligan, J. E. (Autor:in) / Harada, Y. (Autor:in)

    Erscheinungsdatum :

    1976-03-15


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :