Causes, Effects and Diagnostic Measurements of the Reentry Plasma Sheath

Abstract

During entry into the earth's atmosphere of a manned or unmanned space vehicle, a plasma sheath envelops the vehicle because of shock heating of the ambient gases and ablation of the heat shield material. This plasma sheath causes the interruption of radio communications between the space vehicle and ground based stations commonly referred to as the reentry communications blackout. To solve the blackout problem, a knowledge of the reentry plasma sheath properties (electron density, electron collision frequency, electron temperature and plasma stand-off distance) is required. A summary of the causes and effects of the reentry plasma sheath is presented in this report together with a discussion of reentry plasma diagnostic techniques and review of the flight experiments performed to determine the properties of the reentry plasma.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1970
Accession Number
AD0718428

Entities

People

  • James P. Rybak

Organizations

  • Colorado State University

Tags

Communities of Interest

  • Advanced Electronics
  • Sensors
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Atmosphere Entry
  • Boundary Layer
  • Charged Particles
  • Electron Density
  • Electrons
  • Electrostatic Probes
  • Flow Fields
  • Measurement
  • Physics Laboratories
  • Plasma Sheaths
  • Radiation Patterns
  • Radio Frequency
  • Reentry Vehicles
  • Space Flight
  • Spacecraft
  • Standing Waves

Fields of Study

  • Physics

Readers

  • Pulsed Power and Plasma Physics.
  • Space Exploration and Orbital Mechanics.
  • Systems Analysis and Design

Technology Areas

  • Autonomy
  • Microelectronics
  • Space
  • Space - Hall-Effect Thruster
  • Space - Orbital Debris