A baseline structure proposed for the microwave radiometer spacecraft (MRS) reflector is a large graphite-epoxy truss. The truss structure was selected to provide adequate stiffness to minimize control problems and to provide a low-expansion 'strong back' on which to mount and control reflector mesh panels. Details of the structural members, joints and assembly concepts are presented, a concept for the reflector mesh surface is discussed, and preliminary estimates of the mass and structural natural frequencies of the reflector system are presented.


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    Title :

    Preliminary design of tetrahedral truss reflector structure


    Contributors:
    Card, M. F. (author) / Jensen, J. K. (author)


    Publication date :

    1981-12-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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