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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    Title :

    Rocket Launch-Induced Vibration and Ignition Overpressure Response


    Contributors:

    Conference:

    International Congress on Sound and Vibration ; 2001 ; Hong Kong


    Publication date :

    2001-01-01


    Type of media :

    Preprint


    Type of material :

    No indication


    Language :

    English




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