Particle Sizing in a Solid Rocket Motor Using the Management of Scattered Light

Abstract

A previous study discussed the formulation of the theory for the scattering properties in the general case of particles of arbitrary size and refractive index occurring in a polydispersion of finite optical depth. Roberts and Webb concluded that three volume-surface mean diameter (Sauter) D sub 32 of the polydispersion may be determined from the intensity of diffraction scattered light from spherical particles. An experimental investigation was conducted to determine the feasibility of measuring the change in particle size across the exhaust nozzle of a small solid propellant rocket motor. Light scattering measurements were made at small forward angles at the entrance and exit of the exhaust nozzle. The experimental technique was found to be practical, especially if used in conjunction with measurements of transmitted light of multiple wave lengths. However, the determination of D sub 32 is difficult in the motor environment and is biased toward the larger particles in the size distribution. Particle size measurements were in reasonable agreement with sizes determined from collected exhaust products. Recommendations for further improvement of the apparatus are made. Keywords: Diffractively scattered light; Particle sizing.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1985
Accession Number
ADA156480

Entities

People

  • K. Abubakar

Organizations

  • Naval Postgraduate School

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Aluminized Propellants
  • Aluminum Oxides
  • Chemistry
  • Combustion
  • Data Acquisition
  • Diameters
  • Diffraction
  • Lasers
  • Light Sources
  • Light Transmission
  • Particle Size
  • Particles
  • Refraction
  • Refractive Index
  • Rocket Engines
  • Solid Propellants

Fields of Study

  • Physics

Readers

  • Aerosol Science/Aerosol Physics
  • Combustion and Flow Dynamics.