• DocumentCode
    3773359
  • Title

    Boron nitride utilization in radomes

  • Author

    R. O. Howe

  • Author_Institution
    Aerophysics Department Missile Systems, Division Raytheon Company, Bedford, Massachusetts
  • fYear
    1967
  • Firstpage
    175
  • Lastpage
    178
  • Abstract
    Effective interceptor type homing guided missiles must operate at velocities of more than three thousand feet a second in the atmosphere. Developments and studies have indicated that certain of these may eventually be operational in the velocity regime of six to more than eight thousand feet a second. This operational regime is different from the exo-atmospheric regime with a re-entry type vehicle, which encounters its own set of environmental problems.
  • Keywords
    "Temperature","Tensile stress","Silicon compounds","Boron","Dielectrics","Shape","Electromagnetics"
  • Publisher
    ieee
  • Conference_Titel
    Electrical Insulation Conference, 1967 Seventh
  • Print_ISBN
    978-1-5090-3106-1
  • Type

    conf

  • DOI
    10.1109/EIC.1967.7468798
  • Filename
    7468798