Some Research Problems in the Steady-State Burning of Composite Solid Propellants

Abstract

This paper outlines a number of basic problems in the theory of steady-state combustion of solid propellants, particularly of the ammonium perchlorate composite type. It represents an extension of the earlier research at Princeton that led to a theoretical burning rate law for composite propellants that was based on the concept of granular diffusion flame. This paper is in the nature of a progress report in which the new experimental approaches are described, and some puzzling difficulties are analyzed. Specifically, the experiments deal with three topics: refinement of methods for measuring burning rate; the role of radiative energy transfer in the burning process; and the connection between oxidizer particle size and the b parameter in the above-mentioned theoretical burning rate law.

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Document Details

Document Type
Technical Report
Publication Date
Mar 10, 1960
Accession Number
AD0605700

Entities

People

  • C. E. Hermance
  • D. W. Blair
  • E. K. Bastress
  • K. P. Hall
  • M. Summerfield

Organizations

  • Princeton University

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Ammonium Perchlorate
  • Burning Rate
  • Chemical Reactions
  • Chemical Synthesis
  • Chemistry
  • Combustion
  • Composite Materials
  • Composite Propellants
  • Energy Transfer
  • Engineering
  • Jet Propulsion
  • Measurement
  • Munitions
  • New Jersey
  • Particle Size
  • Solid Propellants

Readers

  • Combustion science or combustion engineering.
  • Theoretical Analysis.