Two cylindrical rocket thrust chamber cylinders were coated with a 0.203 mm layer of zirconium-oxide using a process that employed electrodeposition of metal to a spray coated mandrel. The cylinders were cylindrically tested using hydrogen-oxygen propellants at a nominal chamber pressure of 4.14 MN/m2 to show the effect of the coating on life. Both cylinders failed prematurely due to causes unrelated to the coatings. (Kursetz)


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    Title :

    Investigation of the effect of ceramic coatings on rocket thrust chamber life


    Additional title:

    Untersuchung der Auswirkung von keramischen Ueberzuegen bei Schubduesenkammern von Raketentriebwerken


    Contributors:

    Published in:

    Publication date :

    1978


    Size :

    15 Seiten, 25 Bilder, 2 Tabellen, 16 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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