The study was conducted to compare the performance of aluminum landing mat fabricated by Butler Manufacturing Co. The primary method of comparison was by using CBR design curves which were developed to represent 1600 operational cycles of an aircraft having a 60,000-lb gross weight with a single-wheel, main-gear assembly load of 27,000 lb and a 30-7.7 tire inflated to 400 psi. CBR design curves were also developed for 1600 passes of a 39,000-lb single-wheel load applied in a single track to represent the calculated loading imposed on the landing mat during launching of the 60,000-lb aircraft by catapult. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Evaluation of Butler AM2 Landing Mat


    Beteiligte:
    W. B. Fenwick (Autor:in) / M. J. Mathews (Autor:in)

    Erscheinungsdatum :

    1966


    Format / Umfang :

    50 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Evaluation of Various Sizes of Butler AM1 Landing Mat

    C. D. Burns / W. B. Fenwick | NTIS | 1966


    Butler. Butler aircraft company tests new plane

    Engineering Index Backfile | 1928


    Butler. Butler aircraft company tests new plane

    Engineering Index Backfile | 1928


    Butler. Butler aircraft company tests new plane

    Engineering Index Backfile | 1928


    LIFT BUTLER

    MOSKOVITS JUDITH | Europäisches Patentamt | 2016

    Freier Zugriff