Avionics System Design for High Energy Fields
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1988-07-01
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Edition:Final Report
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Abstract:Because of the significant differences in transient susceptibility, the use of digital electronics in flight critical systems, and the reduced shielding effects of composite materials, there is a definite need to define design practices which will minimize electromagnetic susceptibility, to investigate the operational environment, and to develop appropriate testing methods or flight critical systems.
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Main Document Checksum:urn:sha-512:d6393985d5414b099a9d0e94535a65a32696ef397f2bbe6f0268b2100560b330ddd8a1951cc6e6977e78c328fd1aeeff103f6928838f332122b669437b7c5bda
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