PLASMA-INJECTION VACUUM ENERGY DIVERTER (CROWBAR).

Abstract

The purpose of this program was to conduct a theoretical and experimental study toward establishing design concepts for high-voltage energy diverters. The approach utilized the relatively new principle of plasmoid injection for triggering the breakdown of a high-vacuum multiple-section gap. After the metallic arc conduction period the gap returns to a high-vacuum state and voltage hold-off capability, ready for a subsequent controlled operation by the plasmoid trigger. Studies were made on the effects of electrode material, geometry, sputtering, vacuum conditions, external geometry, methods of generating the plasmoid, electron and ion densities and their rate of propagation through vacuum, the trigger geometrical arrangement and location with respect to the hold-off electrodes, use of multiple triggering elements, factors influencing operating range, use of variable spacing and triggering speed, power-handling capabilities and recovery characteristics. The principles studied were used to construct a model of a high-power triggered vacuum gap with an operation objective of 350,000 volts DC. The limited tests results on the model are presented and recommendations for further work. (Author)

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1966
Accession Number
AD0478494

Entities

People

  • H. S. Dunkerley

Organizations

  • General Electric

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Charged Particles
  • Electrodes
  • Electrons
  • Geometry
  • High Vacuum
  • High Voltage
  • Ion Density
  • Ions
  • Materials
  • Recovery
  • Sputtering
  • Vacuum
  • Voltage

Fields of Study

  • Physics

Readers

  • Electrical Engineering
  • Pulsed Power and Plasma Physics.
  • Systems Analysis and Design

Technology Areas

  • Microelectronics
  • Space
  • Space - Hall-Effect Thruster