A theoretical analysis of simple mathematical models of mechanical systems is carried out with a view toward the design of a vibration isolation system for helicopter mounted rocket launchers. Possible future problems and their possible solutions are discussed. An alternative to the vibration isolation system as a means of reducing launching errors due to helicopter induced motion is given. (Author)


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    Titel :

    Ground Support Equipment Airborne Launcher Vibration Isolation Design


    Beteiligte:
    J. M. Oliver (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    45 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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