Title :
Design, construction, computational EM modelling, and characterisation of an aircraft sized reverberation chamber and stirrer
Author :
Goldsmith, Kevin R. ; Johnson, Paul A.
Author_Institution :
Defence Sci. & Technol. Organ., Salisbury, SA, Australia
fDate :
31 Oct-7 Nov 1998
Abstract :
The Defence Science and Technology Organisation has conducted a research program to investigate the performance of reverberation chambers in establishing military aircraft electromagnetic vulnerability (EMV). The construction of an aircraft-sized chamber for research purposes offers special challenges, mostly financial. The most critical design parameters are the chamber dimensions, mode tuner size and wall material
Keywords :
aerospace test facilities; electromagnetic interference; military aircraft; reverberation chambers; aircraft sized reverberation chamber; chamber dimensions; computational EM modelling; electromagnetic vulnerability; military aircraft; mode tuner size; stirrer; wall material; Aerospace electronics; Aircraft manufacture; Aircraft propulsion; Anechoic chambers; Australia; Computational modeling; Costs; Military aircraft; Reverberation chamber; Tuners;
Conference_Titel :
Digital Avionics Systems Conference, 1998. Proceedings., 17th DASC. The AIAA/IEEE/SAE
Conference_Location :
Bellevue, WA
Print_ISBN :
0-7803-5086-3
DOI :
10.1109/DASC.1998.741554
