PROCEEDINGS OF THE SYMPOSIUM ON THE PLASMA SHEATH-PLASMA ELECTROMAGNETICS OF HYPERSONIC FLIGHT (3RD). VOLUME II. ELECTRICAL PROPERTIES OF SHOCK-IONIZED FLOW FIELDS

Abstract

Research approaches to the problem of reentry communications blackout; Estimates of nonequilibrium ionization phenomena in the inviscid apollo plasma sheath; The effect of glide re-entry shock induced ionization on the communication system of the asset vehicle; The use of Langmuir probes in diagnosing ionized flow fields; Antenna breakdown in a hypersonic re- entry environment; Electromagnetic wave properties in a nonlinear, anisotropic, time-dependent plasma medium; Effects of re-entry and space environments on antenna breakdown; and A mathematical model for predicting RF interference effects in rocket exhaust plumes.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1967
Accession Number
AD0825617

Entities

People

  • H. Moore
  • J. Lennon
  • R. Papa
  • W. Rotman

Organizations

  • Air Force Cambridge Research Laboratories

Tags

Communities of Interest

  • Advanced Electronics
  • Air Platforms
  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Birds
  • Boundary Layer
  • Chemical Reaction Properties
  • Chemical Reactions
  • Chemistry
  • Computational Fluid Dynamics
  • Electromagnetic Fields
  • Electron Density
  • Electron Gas
  • Energy Transfer
  • Flow
  • Fluid Dynamics
  • Fluid Flow
  • Fluid Mechanics
  • Frequency
  • Physics Laboratories
  • Pressure Distribution

Fields of Study

  • Physics

Readers

  • Electromagnetic Wave Scattering and Antenna Radiation Engineering
  • Fluid Dynamics.
  • Plasma Physics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flight
  • Space
  • Space - Hall-Effect Thruster