Approximate spectral analysis faster and less expensive than transient analysis. Method of vibration analysis combines separate modes of spacecraft and launcher to determine approximate conditions for resonance. Useful for analysis of any complex structure made up of substructures not coupled too closely; however important to note, method includes effect of dynamic impedance between launcher and payload.


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    Titel :

    Estimating Design Loads in Coupled Vibrating Structures


    Beteiligte:
    Trubert, M. R. (Autor:in) / Salama, M. A. (Autor:in) / Bamford, R. M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.10.1983



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Methods for Estimating Payload/Vehicle Design Loads

    Chen, J. C. / Garba, J. A. / Salama, M. A. et al. | NTRS | 1983




    Identification of vibrating flexible structures

    RAJARAM, S. / Virginia Polytechnic Institute / State University et al. | AIAA | 1985


    Identification of vibrating flexible structures

    RAJARAM, S. / JUNKINS, J. | AIAA | 1984