• DocumentCode
    1357567
  • Title

    Some effects of hypersonic ionization on the design of electrical and electronic components

  • Author

    Sisco, W. B. ; Fiskin, J. M.

  • Author_Institution
    Douglas Aircraft Company, Inc., Long Beach, Calif.
  • Volume
    78
  • Issue
    5
  • fYear
    1959
  • Firstpage
    352
  • Lastpage
    356
  • Abstract
    VEHICLES traveling at hypersonic velocities in a gaseous atmosphere will be surrounded by a shock-induced high-temperature sheath. As a result of the high temperature, the gaseous sheath has an electron density greater than that of the ambient atmosphere. Since the craft will be immersed in a high-temperature envelope, both it and its components will be subjected to unusual temperatures. Fig. 1 indicates the way in which the air temperature and density varies from the shock front to vehicle surface for a given velocity and altitude.
  • Keywords
    Electric shock; Equations; Ionization; Plasma temperature; Power system reliability; Reliability; Vehicles;
  • fLanguage
    English
  • Journal_Title
    American Institute of Electrical Engineers, Part II: Applications and Industry, Transactions of the
  • Publisher
    ieee
  • ISSN
    0097-2185
  • Type

    jour

  • DOI
    10.1109/TAI.1959.6369063
  • Filename
    6369063