If operating restrictions are to be avoided in V/STOL service, features and capabilities beyond conventional landing gear requirements are necessary. Challenges imposed by longer strokes, drift landings, and take-offs without forward velocity, high ground flotation, and rough field operation must be met without exceeding exceptionally low weight targets. The general approach to the design of the XC-142A, a V/STOL transport, landing gear system is described. Certain design features resulting from V/STOL requirements are described in detail.


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    Titel :

    Challenges in Landing Gear Design for V/STOL Service XC-142A


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Fewel, K. J. (Autor:in) / Albach, W. C. (Autor:in)

    Kongress:

    Aeronautic and Space Engineering and Manufacturing Meeting ; 1965



    Erscheinungsdatum :

    1965-02-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Challenges in landing gear design for V/STOL service XC-142a

    Albach, W.C. / Fewel, K.J. | Engineering Index Backfile | 1965





    Flyover noise characteristics of a tilt-wing V/STOL aircraft (XC-142A)

    Pegg, Robert J. / Henderson, Herbert R. / Hilton, David A. | TIBKAT | 1974