This is a closed form solution for the longitudinal oscillation of the Solar Array Flight Experiment (SAFE) blanket for all phases of deployment. The frequency response shows that the blanket frequency increases shortly before full deployment. That fact causes a coupling between the mast and the blanket frequency but, because of the relatively high speed of deployment, a buildup of resonance is unlikely.


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    Title :

    Solar Array Flight Experiment


    Contributors:
    J. Slaby (author)

    Publication date :

    1985


    Size :

    17 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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