THEORETICAL DETERMINATION OF THE IMPEDANCE CHARACTERISTICS OF A CAPACITIVE IONOSPHERE ROCKET PROBE

Abstract

The impedance characteristics of a capacitive ionospheric rocket probe have been determined as a function of the electron density, collision frequency, and temperature. The physical model used in developing the theory incorporated both effects of the ion sheath which forms about the rocket body and the anisotropic nature of the surrounding magnetoionic medium. Results are obtained and numerically evaluated to show that the sheath makes a very significant contribution to the impedance characteristics.

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Document Details

Document Type
Technical Report
Publication Date
Jan 31, 1963
Accession Number
AD0403135

Entities

People

  • J. R. Herman

Organizations

  • Pennsylvania State University

Tags

Communities of Interest

  • Advanced Electronics
  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Capacitance
  • Coordinate Systems
  • Electric Fields
  • Electrical Engineering
  • Electromagnetic Fields
  • Electromagnetic Radiation
  • Electron Density
  • Electrons
  • Equations
  • Frequency
  • Geometry
  • Impedance
  • Ionosphere
  • Magnetic Fields
  • Measurement
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Plasma Physics / Magnetohydrodynamics
  • Plasma Physics.
  • Rocket Propulsion.

Technology Areas

  • Microelectronics