Initial Plasma Tests of the IPROSEC Cathode Device

Abstract

The Ion Proportional Surface Emission Cathode (IProSEC) is a low-brightness cathode technology under development for applications where large areas are available for emission and it is advantageous to avoid the space charge effects often associated with bright or intense sources. Space applications include spacecraft charge control and electrodynamic tethers. Surface Emission Cathodes emit electrons by concentrating an electric field between a p-doped insulating substrate and an adjacent metal cathode element. The substrate potential is held positive of the cathode with gate elements. In plasma, the gate is eliminated due to ambient ion flux which maintains the substrate potential near plasma ground. Prototype devices have been tested using a laboratory plasma source achieving sustained and stable operation over a wide bias voltage for a given ion flux. The principle of operation, ion flux proportionality, and prototype performance is discussed.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 2007
Accession Number
ADA476471

Entities

People

  • A. T. Wheelock
  • D. L. Cooke
  • M. W. Geis

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Air Force Research Laboratories
  • Artificial Satellites
  • Charged Particles
  • Electric Fields
  • Electron Beams
  • Electron Emission
  • Electrons
  • Emission
  • Field Emission
  • Photoexcitation
  • Space Charge
  • Spacecraft
  • Spacecraft Charging
  • Stainless Steel
  • Substrates
  • Three Dimensional
  • Vehicles

Fields of Study

  • Physics

Readers

  • Electrical Engineering
  • Plasma Physics.

Technology Areas

  • Microelectronics
  • Space
  • Space - Hall-Effect Thruster