Gas-Phase Metal Reactions.

Abstract

The use of new advanced solid rocket propellant constituents, such as, e.g., boron as HEDM and ammonium nitrate as replacement for halogen-containing oxidants, requires knowledge of their combustion characteristics. To this end experimental rate coefficient k measurements on individual important Al and B species reactions were made in the 300-1800 K temperature range using a high- temperature fast-flow reactor. Temperature dependent rate coefficient expressions k(T) = AT(super n)exp(-E/RT) are found for the reactions between AlO and CH4, O2; Al and N2O: AlCl and N2O, CO2, SO 2; BCl and N2O, SO2; BO and CO2. To allow semi-empirical predictions for further metal oxidation reactions, two semi-empirical theories have been developed and utilized. These are Semi-Empirical Configuration Interaction theory for prediction of E from one species to another and metals-Transition State Theory for prediction of k(T) from k at one temperature. Dual military-civilian applications of this work are discussed. jg p. 1

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Document Details

Document Type
Technical Report
Publication Date
May 24, 1995
Accession Number
ADA298066

Entities

People

  • Arthur Fontijn

Organizations

  • Rensselaer Polytechnic Institute

Tags

Communities of Interest

  • Advanced Electronics
  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Chemical Compounds
  • Chemical Engineering
  • Chemical Kinetics
  • Chemical Reaction Properties
  • Chemical Reactions
  • Chemical Synthesis
  • Chemistry
  • Combustion
  • Databases
  • Engineering
  • Exothermic Reactions
  • High Temperature
  • Measurement
  • Metal Oxides
  • Physical Chemistry
  • Propellants
  • Rocket Propellants

Readers

  • Combustion science or combustion engineering.