• DocumentCode
    2687718
  • Title

    Analysis, design and testing of integrated structural radomes built using photonic bandgap structures

  • Author

    Scott, Craig

  • Author_Institution
    Northrop Grumman Corp., Pico Rivera, CA, USA
  • Volume
    3
  • fYear
    1998
  • fDate
    21-28 Mar 1998
  • Firstpage
    463
  • Abstract
    The moment method is applied in the spectral domain to produce a matrix eigenvalue equation for 3D photonic band structures having conductive and dielectric elements. The eigenvalue equation for conductive elements is an electric field integral equation (EFIE), obtained by setting the total tangential field equal to zero on the surface of the element. The equation for dielectric elements is a combined field equation (CFIE) obtained by enforcing continuity of tangential electric and magnetic fields across the surface of the element. Calculated dispersion relations are obtained for several types of conductive and dielectric photonic band structures and measured transmission curves are presented for a wire mesh structure
  • Keywords
    eigenvalues and eigenfunctions; electric field integral equations; matrix algebra; method of moments; photonic band gap; radomes; spectral-domain analysis; 3D photonic band structures; CFIE; EFIE; combined field equation; conductive elements; dielectric elements; eigenvalue equation; electric field integral equation; integrated structural radomes; matrix eigenvalue equation; measured transmission curves; moment method; photonic bandgap structures; spectral domain; total tangential field; wire mesh structure; Dielectric substrates; Eigenvalues and eigenfunctions; Fourier series; Frequency; Integral equations; Magnetic field measurement; Passband; Photonic band gap; Propagation constant; Testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 1998 IEEE
  • Conference_Location
    Snowmass at Aspen, CO
  • ISSN
    1095-323X
  • Print_ISBN
    0-7803-4311-5
  • Type

    conf

  • DOI
    10.1109/AERO.1998.685860
  • Filename
    685860