Landing gear design challenges for V/STOL service are identified as imposed by weight, ground flotation, rough field operation, drift landings and takeoffs, landing load factor, cost, maintainability, and reliability; general approach, taken by LTV Aerospace Corp, to design of XC-142A, V/STOL transport, landing gear system is described; design of nose gear presented unusually complex requirements which are indicated.


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    Titel :

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


    Weitere Titelangaben:

    SAE -- Paper


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

    Kongress:

    SAE Meeting ; 1965



    Erscheinungsdatum :

    1965


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :