A family of ceramic, reusable surface insulations developed for the thermal protection of reentry vehicles is discussed. Their thermal properties are summarized and their thermal capabilities are compared. The insulation requirements for the Personnel Launch System are evaluated.


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    Title :

    Reusable surface insulations for reentry spacecraft


    Contributors:

    Publication date :

    1991-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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