Unified Study of Plasma-Surface Interactions for Space Power and Propulsion.

Abstract

The interaction of a high speed (10-20 km/sec) plasma flow of modest temperature (0.5-5 eV) with a solid surface is a basic phenomenon in a variety of high specific power devices, such as advanced high specific impulse thrusters. Study of the details of processes involved in the immediate vicinity of the surface is normally precluded by the very limited diagnostic access afforded in mission-oriented devices. The present research program establishes a plasma flow by means of a quasi-steady magnetoplasmadynamic arcjet and exposes simple solid surfaces to this flow while examining the plasma surface interaction spectroscopically. Detailed measurements provide the benchmark for theoretical modeling that may then be applied to the more complex geometries of actual plasmadynamic devices. The present report covers the development and characterization of the arcjet plasma source and the initial results from experimental diagnostics focused near the surface of a dielectric blunt body in a high speed argon flow. Keywords: Electric propulsion.

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Document Details

Document Type
Technical Report
Publication Date
Jul 14, 1987
Accession Number
ADA186211

Entities

People

  • Peter Turchi

Tags

Communities of Interest

  • Advanced Electronics
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Acquisition
  • Air Force
  • Air Force Facilities
  • Blunt Bodies
  • Classification
  • Current Density
  • Data Acquisition
  • Dielectric Polymers
  • Electron Density
  • Electrons
  • Energy Levels
  • Equations
  • Films
  • Jet Flow
  • Magnetic Fields
  • Measurement
  • Plasma Jets

Fields of Study

  • Physics

Readers

  • Explosive Engineering.
  • Plasma Physics.
  • Theoretical Analysis.

Technology Areas

  • Space
  • Space - Hall-Effect Thruster