Two mechanism types are presented, a rigid boom system and a 'hold and release' mechanism for spherical sensors. Both mechanisms have been designed, developed and tested by Saab-Space AB, Linkoping, Sweden for the VIKING project under a contract from the Swedish Space Corporation.


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    Title :

    Deployment and release mechanisms on the Swedish satellite, VIKING


    Contributors:


    Publication date :

    1983-05-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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