The design, analysis, fabrication and testing of a Kevlar-49/HBRF-55A filament wound chamber is reported. The chamber was fabricated and successfully tested to 80% of the design burst pressure. Results of the data reduction and analysis from the hydrotest indicate that the chamber design and fabrication techniques used for the chamber were adequate and the chamber should perform adequately in a static test.


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    Title :

    Filament wound rocket motor chambers


    Publication date :

    1976-09-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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