Woven fiberglass fluted-core simulated aircraft interior panels were flame tested and structurally evaluated against the Boeing 747 present baseline interior panels. The NASA-defined panels, though inferior on a strength-to-weight basis, showed better structural integrity after flame testing, due to the woven fiberglass structure.


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    Title :

    Evaluation of Materials and Concepts for Aircraft Fire Protection


    Contributors:

    Publication date :

    1976-04-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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