Conventional spacecraft power system components are typically ill-suited to small satellites of less than approximately 300 kg total dry mass. In this paper the unique challenges of small satellite power systems are discussed. The development programs at the Air Force Research Laboratory which address these unique needs are presented.


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    Title :

    Enabling Power Technologies for Small Satellites


    Contributors:

    Conference:

    Seventh International Conference and Exposition on Engineering, Construction, Operations, and Business in Space ; 2000 ; Albuquerque, New Mexico, United States


    Published in:

    Space 2000 ; 530-536


    Publication date :

    2000-02-18




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




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