Development of Advanced Hall Plume Models

Abstract

The purpose of this work was twofold: (a) To develop numerical or analytical methods capable of dealing with the combination of three-dimensionality and strong anisotropy that occurs in the plume region near the exit of a Hall thruster, and (b) To explore the use of fluid-based models in plume computations, so as to overcome the granularity associated with normal particle-based approaches. In area (a) we have carefully formulated the 3D near-plume problem using a combination of heavy particle tracking and magnetized electron fluid equations, and have to a large extent clarified the structure of the solutions, such that numerical implementation should be greatly facilitated. In area (b) we have concentrated on an examination of the far-field of the plume, where the geomagnetic field takes over the dynamics. Again, only a formulation and a suggested method for numerical implementation were completed. Two graduate Theses are still in progress in these two areas, and we expect to issue a supplementary report when they are finalized.

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Document Details

Document Type
Technical Report
Publication Date
Aug 11, 2006
Accession Number
ADA455687

Entities

People

  • Jaume Peraire
  • Manuel Martinez-sanchez

Organizations

  • Massachusetts Institute of Technology

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Computational Science
  • Conductivity
  • Current Density
  • Diffusion
  • Electrons
  • Energy Conservation
  • Equations
  • Far Field
  • Fluids
  • Geometry
  • Hall Thrusters
  • Layers
  • Magnetic Fields
  • Mean Free Path
  • Particles
  • Thrusters

Readers

  • Aerospace Propulsion Engineering.
  • Computational Fluid Dynamics (CFD)
  • Systems Analysis and Design

Technology Areas

  • Microelectronics
  • Space
  • Space - Hall-Effect Thruster