A test technique was developed for applying a full scale mean value (30 kiloampere peak) simulated lightning return stroke current on a complete flight ready aircraft to assess the threat of lightning to aircraft electrical circuits. A computer-aided generator design was used to establish the parameters of the test system. Data from previous work done on development of low inductance current paths determined the basic system configuration.


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    Titel :

    Full scale lightning test technique


    Beteiligte:
    Walko, L. C. (Autor:in) / Schneider, J. G. (Autor:in)


    Erscheinungsdatum :

    01.04.1980


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch






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