Aluminum Combustion in Solid Rocket Motor Chamber Environment (Preprint)

Abstract

A model for prediction of particle radius and oxide cap size/shape versus time for an aluminum particle tracking a stream-tube through a solid rocket motor port has been developed. Following preliminary calculations leading to a postulated flame structure, a quasi-steady model to predict instantaneous consumption of aluminum and generation of condensed oxide (both as a cap on the aluminum particle and as smoke) as a function of instantaneous particle size, ambient conditions, and cumulative amount of oxide in the cap was developed. Finally, this model was imbedded into a framework tracking evolution of particle size, oxide cap size, and ambient conditions, which change as the particle travels along a stream-tube consuming oxidizer and releasing heat. Qualitative agreement was found between predictions and limited observations.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 2007
Accession Number
ADA489555

Entities

People

  • Merrill K. King

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force Research Laboratories
  • Aluminum
  • Aluminum Oxides
  • Boiling Point
  • Boltzmann Equation
  • Burning Rate
  • Combustion
  • Energy
  • Engineering
  • Equations
  • Free Energy
  • Particle Size
  • Payload
  • Rate Of Consumption
  • Rocket Engines
  • Rockets
  • Surface Temperature

Readers

  • Aerosol Science/Aerosol Physics
  • Combustion science or combustion engineering.
  • Computational Modeling and Simulation