The intent of this specification is for the procurement of carbon fiber and fiberglass epoxy prepreg products with 350 °F (177 °C) cure for aerospace applications; therefore, no qualification or equivalency threshold values are provided. Users that intend to conduct a new material qualification or equivalency program must refer to the production quality assurance section (4.3) of this base specification, AMS6891. Widely distributed and available industry material specifications are required for procurement of composite materials whose allowable data is published in CMH-17.


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    Title :

    Carbon Fiber and Fiberglass Epoxy Prepreg Products with 350 °F (177 °C) Cure for Aerospace Applications


    Publication date :

    2020-12-30



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English