Rocket-induced vibration and ignition overpressure response environments are predicted in the low-frequency (5 to 200 hertz) range. The predictions are necessary to evaluate their impact on critical components, structures, and facilities in the immediate vicinity of the rocket launch pad.


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    Titel :

    Rocket Launch-Induced Vibration and Ignition Overpressure Response


    Beteiligte:

    Kongress:

    ICSV8 International Congress on Sound and Vibration ; 2001 ; Hong Kong


    Erscheinungsdatum :

    2001-01-01


    Medientyp :

    Preprint


    Format :

    Keine Angabe


    Sprache :

    Englisch




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