Structural members supporting the afterburners of high thrust rocket engines are subjected to extreme heating, along with severe vibration and high acceleration levels during early lift-off. Chemically-bonded, castable, zircon composite foams were developed and successfully tested to meet specific, laboratory simulated lift-off conditions.


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    Title :

    Castable thermal insulation for use as heat shields


    Additional title:

    Giessbare thermische Isolierung fuer Abschirmung von Hitze


    Contributors:

    Published in:

    Publication date :

    1974


    Size :

    4 Seiten, 6 Bilder, 3 Tabellen, 8 Quellen


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English