Combustion Characteristics of Crystalline Rocket Oxidizers.

Abstract

The report describes a combustion research and testing program that has achieved one of its long range goals; that of providing new theory and practice for burning rate control of solid rocket propellants. In addition, new understanding has been added of the role played by the crystalline oxidizers used in those propellants. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1972
Accession Number
AD0739994

Entities

People

  • Harold C. Beachell

Organizations

  • University of Delaware

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Ammonium Perchlorate
  • Burning Rate
  • Chemical Reaction Properties
  • Chemical Synthesis
  • Chemistry
  • Combustion
  • Combustion Products
  • Composite Propellants
  • Energy Transfer
  • Heat Transfer
  • Materials Laboratories
  • Materials Processing
  • Materials Science
  • Rocket Oxidizers
  • Solid Propellants
  • Spectrometry
  • Spectroscopy

Fields of Study

  • Physics

Readers

  • Rocket Propulsion.
  • Theoretical Analysis.