In manufacture of missile, compromise must be made between tooling costs and amount of allowable "slop" or backlash in control vane linkages; use of "time-frequency response" for missile and describing function for backlash allows reasonable tolerances to be set on control linkages; paper summarizes procedure by which such tolerances can be derived for missile system.


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    Titel :

    Backlash tolerances and their effects on guided missile


    Weitere Titelangaben:

    Aerospace Eng


    Beteiligte:
    Bailey, J.M. (Autor:in) / Kuca, S.A. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1962


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Guided missile

    Green, C.F. | Engineering Index Backfile | 1948


    Guided-missile development

    Millikan, C.B. | Engineering Index Backfile | 1949



    Guided missile incubator

    Ewan, T.K. | Engineering Index Backfile | 1954