The integration of the Get Away Special (GAS) payload for the space shuttle is discussed in terms of systems design. In addition to the primary power, control, and distribution networks to electrically integrate the spaceborne experiments, an instrument measuring system, a data system, and a radio frequency downlink system were designed. A brief review of these systems is given.


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    Title :

    Marshall Amateur Club experiment (MARCE)


    Contributors:


    Publication date :

    1984-07-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English






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