Title :
Lightning protection testing of the E-6 wing tip antenna pod/HF probe
Author :
Enochson, G.L. ; Kormanyos, S.W. ; Severson, V.L.
Author_Institution :
Boeing Aerosp., Seattle, WA, USA
Abstract :
A brief summary is presented of lightning tests conducted on the US Navy E-6 aircraft wing tip antenna pod/HF probe in accordance with MIL-STD-1757 to demonstrate compliance with MIL-B-5087B lightning protection requirements. The tests were conducted on a 22 ft full-sized electrically representative model of the pod/HF probe. Three types of tests were conducted. Long arc attachment tests (MIL-STD-1757 test method T01) were performed to determine the lightning arc entry angle. Direct effects testing (method T02) was conducted to examine the extent of damage which could result from a direct attachment of a high-current lightning strike to the pod. Indirect effects testing (method T05) was conducted to assess the voltage levels induced on equipment cables that result from lightning strike attachment. The waveforms applied, test article configurations, and current injection points were chosen to represent worst-case conditions. Test operations and test results are discussed
Keywords :
aerospace testing; aircraft; antennas; electromagnetic induction; lightning protection; military equipment; probes; standards; 22 ft; E-6 aircraft; E-6 wing tip antenna pod/HF probe; MIL-B-5087B; MIL-STD-1757; US Navy; current injection points; direct effects testing; equipment cables; indirect effects testing; induced voltage; lightning arc entry angle; lightning protection testing; lightning strike; log arc attachment tests; method T02; test article configurations; test results; waveforms; worst-case conditions; Aerospace electronics; Aerospace testing; Bonding; Degradation; Hafnium; Lightning protection; Military aircraft; Probes; Strips; System testing;
Conference_Titel :
Electromagnetic Compatibility, 1989., IEEE 1989 National Symposium on
Conference_Location :
Denver, CO
DOI :
10.1109/NSEMC.1989.37152