Experimental and Analytical Study of Erosive Burning of Solid Propellants

Abstract

Experimental and analytical modeling studies of the erosive burning of solid propellants were conducted at Atlantic Research and Penn State University, with additional modeling efforts at Aeronautical Research Associates of Princeton. At Atlantic Research, erosive burning characteristics of approximately 15 AP- composite solid propellant formulations with systematically varied compositions and ingredient particle sizes were determined over a wide range of pressure and crossflow velocity. It was found that the most important parameter in determining sensitivity of burn rate to crossflow is the no- crossflow (base) burning rate versus pressure behavior of the formulation. An analytical model of the erosive burning of AP-composite formulations was developed and found to yield good a prior predictions of burn rate as a function of pressure and crossflow velocity, given only composition and ingredient particle sizes. This model was also found to predict an observed decrease in crossflow sensitivity with increasing grain port diameter.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1981
Accession Number
ADA102850

Entities

People

  • Kenneth Kuo
  • Merrill K. King
  • Robert Beddini
  • Rohit Arora

Organizations

  • ARCO

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Birds
  • Boundary Layer
  • Burning Rate
  • Cameras
  • Chemical Reaction Properties
  • Chemical Reactions
  • Combustion
  • Composite Propellants
  • Computational Fluid Dynamics
  • Fluid Dynamics
  • Fluid Flow
  • Heat Transfer
  • Mechanical Engineering
  • Motion Picture Cameras
  • Thermodynamics
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Aerosol Science/Aerosol Physics
  • Computational Fluid Dynamics (CFD)
  • Organic Chemistry