Analysis of response of erector to artificially roughened test course was conducted, using various assumptions to determine relative importance of structural flexibilities and suspension system nonlinearities; mathematical model used consists of 3 distributed mass bodies representing missile, container, and tractor, 7 point masses representing wheels and axles, and interconnecting springs and dampers; reasonable agreement between analytic results and test data was achieved with analysis including structural flexibilities and suspension system nonlinearities.


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    Titel :

    Analysis methods and results of digital dynamic analysis of minuteman transporter-erector


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Kennedy, Jr., J.E. (Autor:in) / Levien, K.W. (Autor:in)

    Kongress:

    SAE Meeting ; 1963 Ground equipment



    Erscheinungsdatum :

    1963


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Missile Transporter Erector

    B. I. Leefer | NTIS | 1964



    Minuteman

    Pike, I. | Engineering Index Backfile | 1963


    Minuteman Stage I overtest results

    ANDERSON, G. | AIAA | 1976