A Study of the Effects of Electric Fields on Solid Propellant Burning Rates

Abstract

An experimental study, guided by theoretical considerations, was made on the effects of electric fields on burning rate of two metallized composite propellants. Mechanisms causing observed burning rate changes were sought. Experimental data include flame elctron number densities, electrical conductivities, electric field strengths, electric currents, combustion efficiencies, exhaust emissions spectra and continuous measurement of burning rates. Results show that burning rate increases are due to current heating of the nonburning propellant and that burning rate decreases involve flame electrons, causing inhibited combustion under proper voltage conditions. Non- collective reactional interference was inferred for this latter case.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1971
Accession Number
AD0731840

Entities

People

  • Robert F. Bestgen

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Burning Rate
  • Cameras
  • Chemical Reactions
  • Chemistry
  • Combustion
  • Composite Propellants
  • Electric Current
  • Electrical Conductivity
  • Electromagnetic Fields
  • Electron Density
  • Electrons
  • Heat Transfer
  • Ionization
  • Measurement
  • Solid Propellants
  • Voltage

Fields of Study

  • Physics

Readers

  • Plasma Physics / Magnetohydrodynamics
  • Rocket Propulsion.

Technology Areas

  • AI & ML
  • AI & ML - Bayesian Inference
  • Microelectronics