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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    Titel :

    Evaluation of Materials and Concepts for Aircraft Fire Protection


    Beteiligte:
    Anderson, R. A. (Autor:in) / Price, J. O. (Autor:in) / Mcclure, A. H. (Autor:in) / Tustin, E. A. (Autor:in)

    Erscheinungsdatum :

    1976-04-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Evaluation of Materials and Concepts for Aircraft Fire Protection

    R. A. Anderson / J. O. Price / A. H. Mcclure et al. | NTIS | 1976


    Aircraft Fire Protection Technology Applications

    Patterson, D. M. / Tempesta, F. L. / Alexander, J. G. et al. | SAE Technical Papers | 1972


    Airport and aircraft fire protection

    Tryon III, G.H. | Engineering Index Backfile | 1946