STUDIES OF ANTENNA BREAKDOWN IN THE PRESENCE OF A PLASMA SHEATH INCLUDING EFFECTS OF FORCED CONVECTION.

Abstract

Interest in the reentry communications problem has motivated an effort to generate a plasma layer on a model in a supersonic wind tunnel using a nitrogen dc plasma jet mounted in the blunt nose of the model. Langmuir probe data indicate non-uniform charged particle distribution with a peak about 0.25 to 0.4 inches from the model surface. Results of high power X-band antenna measurements, both visually and with VSWR and received power instrumentation, show a distinct indication of antenna breakdown persisting with the plasma layer present. However, changes in VSWR and received power after breakdown are more gradual. It is suggested that changes in slope of a received power curve as a function of applied power be used as an indication of breakdown in the presence of a plasma layer. (Author)

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1967
Accession Number
AD0651233

Entities

People

  • Eugene E. Covert
  • Laurence R. Boedeker

Organizations

  • Massachusetts Institute of Technology

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Charged Particles
  • Convection
  • Instrumentation
  • Langmuir Probes
  • Measurement
  • Measuring Instruments
  • Nitrogen
  • Particles
  • Plasma Jets
  • Plasma Sheaths
  • Probes
  • Supersonic Wind Tunnels
  • Wind Tunnels
  • X Band

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Phased Array Antenna Design.
  • Plasma Physics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flight