Pulsed Plasma Radio Frequency Interference Studies.

Abstract

An unshielded external test set was developed which allows the millipound thrust level pulsed plasma thruster to be repetitvely operated in air. The present design was operated at a peak discharge current of 47 kiloamperes. Electromagnetic emission tests carried out showed that the present unshielded test set would have to be shielded if the pulsed noise generated by it has to meet RE02 electric field and magnetic field requirements. The results of the noise measurements presented can be used as a basis for the design of the shielding. Shielding effectiveness measurements have shown that EMI gaskets are not required in the covers of the thruster enclosure if the covers are well fitted and secured by a double row of alternately spaced screws. (Author)

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1977
Accession Number
ADA049581

Entities

People

  • Martin Begun
  • William Gunman

Tags

Communities of Interest

  • Advanced Electronics
  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Barriers
  • Electric Fields
  • Electric Propulsion
  • Electromagnetic Fields
  • Electromagnetic Radiation
  • Electromagnetic Shielding
  • Electromagnetism
  • Field Emission
  • Geometry
  • Magnetic Fields
  • Magnetic Properties
  • Measurement
  • Pulsed Plasma Thrusters
  • Radio Frequency
  • Rocket Propulsion
  • Waveforms

Fields of Study

  • Physics

Readers

  • Electrical Engineering
  • Electromagnetic Wave Scattering and Antenna Radiation Engineering
  • Logistics and Supply Chain Management.

Technology Areas

  • Space
  • Space - Hall-Effect Thruster