A battery-charger-controller system comprising a 28V nickel-cadmium battery and a 270 Vdc -powered charger-controller unit is described.


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    Title :

    F-22 Aircraft Battery-Charger-Controller System


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    Aerospace Power Systems Conference ; 1999



    Publication date :

    1999-04-06




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    F-22 Aircraft Battery-Charger-Controller System

    Stoneham, T. A. / Society of Automotive Engineers | British Library Conference Proceedings | 1999


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