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.
Hero susceptibility of 2.75 inch FFAR: Comparative results obtained from mode-stirred chambers, anechoic chambers, and ground plane test facilities
Die Suszeptibilitaet einer Flugzeugrakete: Vergleichende Ergebnisse aus einem echolosen Raum, einem Nachhallraum und Messungen auf dem flachen Boden
1985
5 Seiten, 4 Bilder, 10 Quellen
Conference paper
English
HERO AND ESD PROTECTION OF THE IMPROVED 2.75-INCH ROCKET
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