Hall Thruster Electron Mobility Investigation using Full 3D Monte Carlo Trajectory Simulations (Preprint)

Abstract

Axial electron transport represents a loss in efficiency for crossed field devices, such as Hall-effect thrusters (HETs). Previous experimental and computational investigations have revealed an anomalous axial mobility that cannot be explained with classical theory. This work describes the development of a computational model that calculates electron mobility in HETs using known electric and magnetic fields. Specifically, a full 3D Monte Carlo trajectory simulation code is developed to simulate HET internal electron dynamics. Simulations were completed using the AFRL/University of Michigan P5 HET. The magnetic field for this thruster is known from magnetostatic simulations and the electric field present during thruster operation has been experimentally measured by Haas. Comparison of the axial mobility from our code and the mobility calculated by Koo for the P5 shows agreement.

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Document Details

Document Type
Technical Report
Publication Date
Aug 24, 2007
Accession Number
ADA473505

Entities

People

  • Brian E. Jurczyk
  • Darren A. Alman
  • Joshua L. Rovey
  • Robert A. Stubbers

Tags

Communities of Interest

  • Energy and Power Technologies
  • Materials and Manufacturing Processes
  • Space

DTIC Thesaurus Topics

  • Air Force Research Laboratories
  • Electric Fields
  • Electric Propulsion
  • Electron Mobility
  • Electrons
  • Engineering
  • Engineers
  • Hall Effect
  • Hall Thrusters
  • Ion Thrusters
  • Magnetic Fields
  • Mobility
  • Physics
  • Plasmonic Devices
  • Simulations
  • Thrusters
  • Trajectories

Fields of Study

  • Physics

Readers

  • Aerospace Propulsion Engineering.
  • Computational Fluid Dynamics (CFD)
  • Plasma Physics / Magnetohydrodynamics

Technology Areas

  • Microelectronics
  • Space
  • Space - Hall-Effect Thruster