Three 71-cm-diameter boron/epoxy composite rocket motor chambers were filament wound. The first chamber was hydrostatically tested; the second failed in proof test as a result of fabrication deficiencies. The third chamber obtained a successful proof test, but deformed later in processing because of hydrolysis. In spite of the deformation, this chamber was test fired and then burst tested.


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    Titel :

    Fabrication of boron/epoxy rocket motor chambers.


    Beteiligte:
    Jensen, W. M. (Autor:in) / Stang, D. A. (Autor:in)

    Kongress:

    National Technical Conference and Exhibition ; 1972 ; Palo Alto, CA


    Erscheinungsdatum :

    01.01.1972


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :