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. (Author)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Evaluation of Materials and Concepts for Aircraft Fire Protection


    Contributors:
    R. A. Anderson (author) / J. O. Price (author) / A. H. Mcclure (author) / E. A. Tustin (author)

    Publication date :

    1976


    Size :

    38 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Evaluation of Materials and Concepts for Aircraft Fire Protection

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


    Airport and aircraft fire protection

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


    Aircraft Fire Protection Technology Applications

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