Thermal effects and space-charge limited transition in crossed-field devices

Abstract

A fully kinetic model for the electron flow in a crossed field device is derived and used to determine the system stationary states. It is found that for low injection temperatures, there is a simultaneous presence of distinct stationary solutions and an abrupt transition between accelerating and space-charge limited regimes. On the other hand, for high injection temperatures, there is only a single stationary solution branch and the change between the regimes becomes continuous. For intermediate temperatures, it is then identified a critical point that separates the abrupt and continuous behaviors. It is also investigated how intrinsic space-charge oscillations may drive stationary states unstable in certain parameter regimes. The results are verified with N-particle self-consistent simulations.

Document Details

Document Type
Pub Defense Publication
Publication Date
Aug 01, 2014
Source ID
10.1063/1.4893313

Entities

People

  • Felipe B. Rizzato
  • Renato Pakter
  • Samuel Marini

Organizations

  • Air Force Office of Scientific Research
  • Federal University of Rio Grande do Sul

Tags

Fields of Study

  • Physics

Readers

  • Electronics Engineering
  • Plasma Physics / Magnetohydrodynamics

Technology Areas

  • Microelectronics
  • Microelectronics - Graphene
  • Space
  • Space - Hall-Effect Thruster