• DocumentCode
    1938260
  • Title

    Challenging fundamental limits in the fabrication of vector vortex waveplates

  • Author

    Hakobyan, R.S. ; Tabiryan, N.V. ; Serabyn, E.

  • Author_Institution
    BEAM Eng. for Adv. Meas. Co., Winter Park, FL, USA
  • fYear
    2013
  • fDate
    2-9 March 2013
  • Firstpage
    1
  • Lastpage
    10
  • Abstract
    Vector vortex waveplates (VVWs) are in the heart of vortex coronagraphs aimed at exoplanet detection close to bright stars. VVWs made of liquid crystal polymers (LCPs) provide structural continuity, opportunity of high order singularities, large area, and inexpensive manufacturing technology. However, to date, the performance of such devices is compromised by imperfections in singularity area that allow some residual starlight leakage. Reducing the singularity to subwavelength sizes increases the energy of elastic deformations of the LC. As a result, the azimuthally symmetric orientation pattern gives way to 3D deformations that reduce the elastic energy of the LC. The stability of radial orientation is determined by elastic constants of the LC, the thickness of the layer and the boundary conditions. In the current paper, we examin the role of those factors to determine the fundamental limits the singularity area could be reduced to for LCP VVWs.
  • Keywords
    coronagraphs; elastic constants; elastic deformation; liquid crystal polymers; stars; 3D deformations; LCP; VVW; azimuthally symmetric orientation pattern; bright stars; elastic constants; elastic deformations; elastic energy; exoplanet detection; high order singularity; inexpensive manufacturing technology; liquid crystal polymers; radial orientation; residual starlight leakage; vector vortex waveplates; vortex coronagraphs; Boundary conditions; Equations; Optical device fabrication; Optical films; Optical scattering; Optical vortices; Vectors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2013 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4673-1812-9
  • Type

    conf

  • DOI
    10.1109/AERO.2013.6497192
  • Filename
    6497192