RESPONSE OF A BURNING PROPELLANT SURFACE TO EROSIVE TRANSIENTS

Abstract

A review of the past quarter's activity on combustion instability is given. In the experimental work a study of solid phase exothermic reactions is being performed. An attempt is also being made to study the gas phase reactions occurring at the surface during instable burning using real time spectroscopy. (A rapid scan of 60 microseconds to study the 2 millisecond disturbance.).

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Document Details

Document Type
Technical Report
Publication Date
Jul 19, 1966
Accession Number
AD0487792

Entities

People

  • E. L. Capener
  • G. A. Marxman
  • L. A. Dickinson

Organizations

  • SRI International

Tags

DTIC Thesaurus Topics

  • Air Force
  • Ammonium Perchlorate
  • Burning Rate
  • Combustion
  • Differential Thermal Analysis
  • Double Base Propellants
  • Emission Spectra
  • Energy
  • Exothermic Reactions
  • High Temperature
  • Phase
  • Propellants
  • Scientific Research
  • Solid Phases
  • Spectra
  • Spectroscopy
  • Thermal Analysis

Fields of Study

  • Physics

Readers

  • Molecular Photonics/Laser Physics
  • Rocket Propulsion.
  • Systems Analysis and Design