DIAGNOSIS OF PERFORMANCE OF ELECTRIC PROPULSION ENGINES.

Abstract

A program of research has been carried out on the response of electron emissive particle beam systems to electric fields. These 'E-field meters' may be used in turn for determinations of the surface electric field strength of isolated spacecraft. The experimental and analytical studies have resulted in the development of a comparatively sensitive device capable of electric field strength measurements within approximately a .1 volt/cm with an extended range capability up to electric field strengths of 100 volts/cm at reduced sensitivities. The meter performance is adequate for its operation in the space environment where the factors of the geo-magnetic field and the ambient space plasma and photo-electric effects, though present, constitute only minimum perturbations to the meter performance. Although effort remains to be done in the transformation of this laboratory type field sensor into a fully operational spacecraft instrument, the present program of research has successfully examined and determined the basic questions of scientific merit for this device. (Author)

Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1967
Accession Number
AD0812563

Entities

People

  • J. M. Sellen Jr.
  • Jack W. Geis
  • Robert F. Kemp
  • Robert K. Cole

Organizations

  • TRW Inc.

Tags

Communities of Interest

  • Sensors

DTIC Thesaurus Topics

  • Electric Fields
  • Electric Propulsion
  • Electrons
  • Environment
  • Magnetic Fields
  • Measurement
  • Particle Beams
  • Particles
  • Perturbations
  • Sensitivity
  • Space Environments
  • Spacecraft

Fields of Study

  • Physics

Readers

  • Plasma Physics.
  • Systems Analysis and Design

Technology Areas

  • Directed Energy
  • Microelectronics
  • Space
  • Space - Hall-Effect Thruster