Towards Reduced Wall Effect Hall Plasma Accelerators

Abstract

The primary objective of our existing grant, as stated in our original proposal, was to (i) develop a better understanding of the electron transport in Hall thrusters; (ii) greatly reduce or eliminate the influence of the walls on the electron transport; and (iii) replace the role of the wall in electron conduction with enhancement and control of the bulk conductivity. in this way, the selection of wall material and thruster geometry can be made independently of its effect that the wall will have on conductivity, so as to optimize the thruster performance with respect to reliability and service life.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 2007
Accession Number
ADA471583

Entities

People

  • Mark Cappelli

Organizations

  • Stanford University

Tags

Communities of Interest

  • Advanced Electronics
  • Energy and Power Technologies
  • Human Systems

DTIC Thesaurus Topics

  • Air Force
  • Electric Propulsion
  • Electron Mobility
  • Fluids
  • Geometry
  • Hall Effect
  • Hall Thrusters
  • Magnetic Fields
  • Measurement
  • Mechanical Engineering
  • Millimeter Waves
  • Near Field
  • Simulations
  • Three Dimensional
  • Thrusters
  • Two Dimensional
  • Voltage

Fields of Study

  • Physics

Readers

  • Materials Science and Engineering.
  • Pulsed Power and Plasma Physics.
  • Software Engineering

Technology Areas

  • Microelectronics
  • Space
  • Space - Hall-Effect Thruster