Emittance of a Field Emission Electron Source

Abstract

An analytical formula of the emittance of a field emitter is given. In contrast to thermal and photoemission, such a formula contains complexity due to the multidimensional nature of the source. A formulation of emittance is given for one- and three-dimensional 3D field emitters. The 3D formulation makes use of the point charge model of a unit cell emitter coupled with a trajectory analysis to follow electrons to an evaluation plane where emittance is determined. The single tip theory is extended to an array and the resulting theory predicts the emittance of a Spindt-type square array of emitters 0.2 cm on a side producing 2000 A/sq cm is 23 mm mrad. Theory compares favorably with experimental measurements in the literature from ungated and gated sources. The impacts of several complications are estimated: the effects of a gate for modulating the emitter; the influence of space charge within the unit cell on the beam; and constraints imposed by modulation frequency, emitter dimensions, and rise/fall time requirements for turning a beam on and off, as determined by the array's RLC characterization.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jan 05, 2010
Accession Number
ADA512275

Entities

People

  • D. W. Feldman
  • J. L. Shaw
  • K. L. Jensen
  • P. G. O'shea

Organizations

  • United States Naval Research Laboratory

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Charged Particles
  • Current Density
  • Electron Beams
  • Electrons
  • Emission
  • Emittance
  • Emitters
  • Field Emission
  • Free Electron Lasers
  • Free Electrons
  • Frequency
  • Geometric Forms
  • Geometry
  • Lasers
  • Light Sources
  • Microwave Amplifiers
  • Three Dimensional

Fields of Study

  • Physics

Readers

  • Computational Modeling and Simulation
  • Electronics Engineering
  • Pulsed Power and Plasma Physics.

Technology Areas

  • Microelectronics
  • Space
  • Space - Hall-Effect Thruster