Report summarizes program of measurements and calculations of vibrations in filament-wound composite models of Space Shuttle solid-rocket boosters. Vibrational behavior predicted by finite-element computer model of structural dynamics correlates well with data from tests on full- and quarter-scale models. Computer model developed with NASTRAN general-purpose structural-analysis computer code.


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    Titel :

    Structural Dynamics of Filament-Wound Booster Rockets


    Beteiligte:
    Bugg, F. M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.10.1987



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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