The performance of the NATO-111-A and NATO 111-B satellite battery is reported. The electrical power subsystem is briefly described. The electrical characteristics and the reconditioning experience of the batteries is cited. The in-orbit experience is compared with results of preflight accelerated life tests.


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    Title :

    NATO: In-orbit experience


    Contributors:


    Publication date :

    1980-04-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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