Arcing due to spacecraft charging on spacecraft EMI margins of immunity was determined. The configuration of the P78-2 spacecraft of the SCATHA program was analyzed. A brushfire arc discharge model was developed, and a technique for initiating discharges with a spark plug trigger was for data configuration. A set of best estimate arc discharge parameters was defined. The effects of spacecraft potentials in limiting the discharge current blowout component are included. Arc discharge source models were incorporated into a SEMCAP EMI coupling analysis code for the DSP spacecraft. It is shown that with no mission critical circuits will be affected.


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    Titel :

    Implications of Arcing Due to Spacecraft Charging on Spacecraft EMI Margins of Immunity


    Beteiligte:
    G. T. Inouye (Autor:in)

    Erscheinungsdatum :

    1981


    Format / Umfang :

    171 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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