Initial Plasma Testing of the Ion Proportional Surface Emission Cathode

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 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. Chip-based sources are compared to carbon nanotube mats. The principle of operation, ion flux proportionality, and prototype performance is discussed.

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Document Details

Document Type
Technical Report
Publication Date
Jul 15, 2008
Accession Number
ADA490909

Entities

People

  • Adrian Wheelock
  • D. L. Cooke
  • Michael W. Geis

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Advanced Electronics
  • Space

DTIC Thesaurus Topics

  • Air Force Research Laboratories
  • Artificial Satellites
  • Astronautics
  • Carbon Nanotubes
  • Charged Particles
  • Electric Fields
  • Electron Beams
  • Electron Emission
  • Electrons
  • Emission
  • Field Emission
  • Fullerenes
  • Geosynchronous Orbits
  • Low Earth Orbits
  • Materials Laboratories
  • Space Charge
  • Spacecraft

Fields of Study

  • Physics

Readers

  • Integrated Circuit Design and Technology.
  • Plasma Physics.

Technology Areas

  • Microelectronics
  • Space
  • Space - Hall-Effect Thruster