A modified 2.75-Inch FFAR (folding fin aircraft rocket) was subjected to radiated susceptibility tests in four different test facilities: ground plane, anechoic chamber, and two mode-stirred chambers. A comparison of the peak response data indicates: a. good repeatability between the two mode-stirred chambers. b. consistently higher responses measured in the anechoic chamber and ground plane than in the mode-stirred chambers. There is evidence that the 'correlation factor' between 'free space' and mode-stirred chamber EMEs is simply the gain of the equipment under test. Absolute correlation would thus require an a priori estimate of the gain.


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    Titel :

    Hero susceptibility of 2.75 inch FFAR: Comparative results obtained from mode-stirred chambers, anechoic chambers, and ground plane test facilities


    Weitere Titelangaben:

    Die Suszeptibilitaet einer Flugzeugrakete: Vergleichende Ergebnisse aus einem echolosen Raum, einem Nachhallraum und Messungen auf dem flachen Boden


    Beteiligte:
    Rean, J.L. (Autor:in)


    Erscheinungsdatum :

    1985


    Format / Umfang :

    5 Seiten, 4 Bilder, 10 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    HERO AND ESD PROTECTION OF THE IMPROVED 2.75-INCH ROCKET

    Frasch, H. / Bentley, R. / Manley, D. et al. | British Library Conference Proceedings | 1993


    Microwave absorbers and anechoic chambers

    Pyck, J. | Tema Archiv | 1985


    Free Field Simulation in Anechoic Chambers

    Weinstein, Jonathan / Clemente, Victor | SAE Technical Papers | 2001


    Multi-Wire Transmission Lines for EMC Susceptibility Measurements in Anechoic Chambers

    Carbonini, L. / Tarducci, D. / Politecnico di Torino et al. | British Library Conference Proceedings | 1991


    GROUND FACILITIES-ALTITUDE TEST CHAMBERS, ADVANTAGES AND LIMITATIONS

    ROSS, LT. COL. D. M. | SAE Technical Papers | 1952