Fuel-Rich Solid Propellant Boron Combustion

Abstract

Single particle boron ignition and combustion models developed in earlier phases of this program have been utilized and extended to treatment of boron cloud ignition, oxidizer depletion effects on cloud combustion time, laminar flame speeds in boron dust clouds, agglomerate ignition, and the effects of halogens, lithium fluoride coatings, and metal coatings on particle ignition. In addition, they have been utilized in a modular combustor model (well-stirred reactor followed by a two-dimensional mixing zone) of boron slurry combustion. Critical deficiencies in knowledge of processes of condensation of various boron oxides/hydroxides have been defined and an experiment to better quantify and understand these processes has been designed. An experimental program for definition of kinetics of boron oxide liquid plus water vapor (important to boron particle ignition) has been carried out. A comprehensive data base of ignition and combustion times for small (10 to 50 micron) boron particles in various wet and dry environments has been developed and a limited experimental study of the effects of LiF coatings on boron ignition performed. Finally, experiments aimed at characterizing dominant processes is boron solid-fuel ramjet combustion, utilizing a windowed slab burner, have been accomplished.

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Document Details

Document Type
Technical Report
Publication Date
May 31, 1984
Accession Number
ADA148522

Entities

People

  • J. Komar
  • M. K. King
  • R. S. Fry

Organizations

  • ARCO

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Burning Rate
  • Cameras
  • Chemistry
  • Combustion
  • Ignition Lag
  • Laser Induced Fluorescence
  • Liquids
  • Materials Laboratories
  • Measurement
  • Optical Materials
  • Oxides
  • Particle Size
  • Photography
  • Propulsion Systems
  • Transport Properties
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Aerosol Science/Aerosol Physics
  • Combustion science or combustion engineering.
  • Rocket Propulsion.