STUDY OF THE PARTICULATE MATTER IN THE EXHAUST OF A BORON-LOADED SOLID PROPELLANT.

Abstract

Particles issuing from the primary solid propellant combustor of a typical boron-loaded air-augmented rocket motor have been collected and analyzed for chemical composition and size distribution. It was found that substantial changes can occur in the chemical composition of the particulate effluent (notably, ammonium pentaborate and carbon were found), but the size analyses suggest that no important change in the boron size distribution occurs. However, this last conclusion is subject to the uncertainties involved in any particle collection technique's influence on the size distribution results, and for this reason a discussion of possible in situ measurements using light scattering is included at the end of this report. Primarily because of the high optical depths involved in the primary motor plume, however, it is concluded that such experimental techniques would be unsuccessful. (Author)

Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1970
Accession Number
AD0709678

Entities

People

  • A. M. Mellor
  • F. C. Gouldin

Organizations

  • Purdue University

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Chemical Composition
  • Combustors
  • Light Scattering
  • Measurement
  • Particles
  • Particulate Matter
  • Particulates
  • Propellants
  • Rocket Engines
  • Rockets
  • Scattering
  • Solid Propellants
  • Uncertainty

Fields of Study

  • Physics

Readers

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