Behavior of Ionized Plasma in the High Latitude Topside Ionosphere.

Abstract

We have developed a numerical model to study the steady state behavior of a fully ionized plasma (H+, O+ and the electrons) encompassing the geomagnetic field lines. The theoretical formulation is based on the 16-moment system of transport equations. The electron gas is collision is dominated below 2500 km. Above this altitude electron temperature anisotropy develops with temperature perpendicular to the field line being higher than that parallel to the field line. The H+ ion temperature anisotropy shows H+ temperature parallel to the field line being higher than that perpendicular to the field line. H+ ion temperature also exhibits adiabatic cooling as to the supersonic ion gas cools down as it expands in a diverging magnetic field. Our results are in good agreement with the pervious theoretical studies of the polar wind and recent experimental observations. This is the first successful steady state solution to the 16-moment set of transport equations. Keywords include: Polar wind, Temperature anisotropy, and Adiabatic cooling.

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Document Details

Document Type
Technical Report
Publication Date
Aug 27, 1985
Accession Number
ADA157930

Entities

People

  • H. G. Mitchell Jr.
  • P. J. Palmadesso
  • S. G. Ganguli

Organizations

  • United States Naval Research Laboratory

Tags

Communities of Interest

  • Advanced Electronics
  • Energy and Power Technologies
  • Space

DTIC Thesaurus Topics

  • Agreements
  • Altitude
  • Anisotropy
  • Boltzmann Equation
  • Charged Particles
  • Electron Gas
  • Electrons
  • Equations
  • Geography
  • High Latitudes
  • Ion Density
  • Magnetic Fields
  • Plasmas (Physics)
  • Protons
  • Space Sciences
  • Steady State
  • Temperature Gradients

Fields of Study

  • Physics

Readers

  • Combustion Dynamics and Shock Wave Physics.
  • Space/Atmospheric Physics.
  • Thermal Physics or Thermal Science.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow
  • Microelectronics