Development of Electric: Field Sensors

Abstract

The purpose of this program was to obtain parametric data and develop criteria needed in the design of wire-mesh-type electric-potential sensors for arbitrary Electromagnetic pulse (EMP) and Internal Electromagnetic Pulse (IEMP) environments. Tests were performed with various grid materials, thicknesses, and configurations in selected environments provided by the Febetron 706, Febetron 705, and Aurora flash gamma-ray machines, with varied environmental parameters such as air pressure and cavity material. It is shown that this technique can be used successfully when an essentially open-circuit voltage measurement is made, provided that care is taken to prevent large amounts of charge from being deposited on or scattered from the grid, which causes it to depart from the space-charge potential it is intended to measure. The various sources of these charges are described, and methods of minimizing the problem have been demonstrated. Furthermore, a method is illustrated that allows discrimination between the desired space-charge potential and the error-producing charge-deposition potential.

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Document Details

Document Type
Technical Report
Publication Date
Feb 26, 1974
Accession Number
AD0783717

Entities

People

  • Arthur L. Whitson
  • Duane C. Gates
  • William C. Taylor

Organizations

  • SRI International

Tags

Communities of Interest

  • Energy and Power Technologies
  • Sensors
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Pressure
  • Cellular Structures
  • Electric Fields
  • Electromagnetic Fields
  • Electromagnetic Pulses
  • Electron Density
  • Electron Flux
  • Electrons
  • Ionization
  • Measurement
  • Nanofibers
  • Radiation Effects
  • Scattering
  • Vacuum Chambers
  • Voltage
  • X Rays

Fields of Study

  • Physics

Readers

  • Aerospace Test and Evaluation
  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)
  • Pulsed Power and Plasma Physics.

Technology Areas

  • Space
  • Space - Hall-Effect Thruster