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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    Title :

    Ground Support Equipment Airborne Launcher Vibration Isolation Design


    Contributors:

    Publication date :

    1972


    Size :

    45 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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