Ignition and Flame Propagation in Narrow Channels of Solid Propellant

Abstract

Future direct-fire gun systems will require solid propellant at high loading density, which can be achieved with propellant in slab-type geometry such as radial discs, concentric wraps, or scrolls. Adjacent propellant slabs will form porosity as narrow sheet-like channels (with entirely different permeability than bundled sticks or cylindrical grains). Successful functioning of the charge requires rapid ignition and unimpeded flame propagation throughout this system of channels. The present investigation is concerned with characterizing the fundamental ignition and transient combustion behavior of energetic materials when packed in such configurations. A special laboratory apparatus was designed to isolate two propellant channels and allow direct comparison of the influence of variable gap width, wall composition (inert or JA2 here), and channel end closure. Diagnostics include multiple pressure time histories along each channel length and high-speed cinematography of the propagation of flame. Results are presented for several channel configurations, showing influence of JA2 or plastic wall material, gap widths of 0-0.89 mm, and channel downstream ends either open or closed.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 2003
Accession Number
ADA416554

Entities

People

  • Douglas E. Kooker
  • Lang-mann Chang

Organizations

  • United States Army Research Laboratory

Tags

DTIC Thesaurus Topics

  • Burning Rate
  • Combustion
  • Combustion Chambers
  • Double Base Propellants
  • Energetic Materials
  • Fires
  • Flame Propagation
  • Flames
  • Ignition
  • Materials
  • Materials Laboratories
  • Military Research
  • Pressure Gradients
  • Propellants
  • Propelling Charges
  • Rdx
  • Solid Propellants

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Electrical Engineering
  • ballistics.