Analysis of a Solid Propellant Gas Generator Using an Ammonium Perchlorate-Polybutadiene Composite Propellant.

Abstract

An analytical program has been carried out for the purpose of studying the fluid dynamic and chemical processes occurring in a Solid Propellant Gas Generator (SPGG) device. The purpose of the SPGG device was to produce chemical exhaust species suitable for operation as a laser. The propellant used in the SPGG was Ammonium Perchlorate (AP) in a Polybutadiene (PBAN) fuel matrix. The combustion flame process was considered to occur in three successive steps: AP decomposition, PBAN pyrolysis, and combustion of the AP decomposition products with the PBAN pyrolysis products. For this combustion process a gas phase finite rate chemical reaction model was derived. The combustion process occurring near the surface of the propellant was modeled in order to derive non-equilibrium. (Author)

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1972
Accession Number
AD0749144

Entities

People

  • Douglas E. Coats
  • Gary R. Nickerson

Tags

Communities of Interest

  • Energy and Power Technologies
  • Materials and Manufacturing Processes
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Alkenes
  • Ammonium Perchlorate
  • Arrhenius Equation
  • Burning Rate
  • Chemical Kinetics
  • Chemical Reaction Properties
  • Chemical Reactions
  • Chemistry
  • Combustion
  • Combustion Products
  • Composite Propellants
  • Exothermic Reactions
  • Ignition Lag
  • Rocket Engines
  • Solid Propellants
  • Turbulent Mixing

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Rocket Propulsion.

Technology Areas

  • Directed Energy