• DocumentCode
    3405547
  • Title

    Lightning protection testing of the E-6 long trailing wire antenna

  • Author

    Severson, V. ; Enochson, G.

  • Author_Institution
    Boeing Co., Seattle, WA, USA
  • fYear
    1990
  • fDate
    21-23 Aug 1990
  • Firstpage
    212
  • Lastpage
    217
  • Abstract
    Lightning test were conducted on the US Navy E-6 aircraft long trailing wire antenna (LTWA) in accordance with MIL-STD-1757 to demonstrate compliance with MIL-B-5087B lightning protection requirements. The tests were conducted on a 22-foot-long, full-sized, electrically representative model of the LTWA. Two types of tests were conducted: direct structural effects and indirect effects. In the direct effects testing, the test article withstood the application of four series of lightning current waveforms with no structural damage. In the indirect effects testing, initial induced current and voltage measurements were performed on each of the 16 wires in the test article wire harness. The measured voltages, when extrapolated to the full thread strike level, exceeded the MIL-B-5087B limit of 500 volts
  • Keywords
    aircraft communication; electronic equipment testing; lightning protection; military equipment; mobile antennas; standards; 22 ft; E-6 long trailing wire antenna; MIL-B-5087B; MIL-STD-1757; US Navy E-6 aircraft; direct structural effects; electrically representative model; full thread strike level; indirect effects; induced current; induced voltage; lightning current waveforms; lightning protection testing; military standards; wire harness; Aircraft; Assembly; Bonding; Grounding; Lightning protection; Pulleys; Testing; Underwater vehicles; Winches; Wire;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Electromagnetic Compatibility, 1990. Symposium Record., 1990 IEEE International Symposium on
  • Conference_Location
    Washington, DC
  • Print_ISBN
    0-7803-7264-6
  • Type

    conf

  • DOI
    10.1109/ISEMC.1990.252760
  • Filename
    252760