Ignition Transients and Pressurization in Closed Chambers

Abstract

Pressure versus time data obtained from igniting and burning propellants in highly loaded closed chambers (loading densities between 0.1 and 0.3 g/cc) are being used to evaluate propellants in empirical quality and production control procedures. Interpretations obtained from such production control devices are hampered by uncertainties concerning ignition delays, dynamic burning, heat loss, propellant surface area versus distance burned, and real gas effects. In this study, attention is focused on devising a closed chamber experiment for measuring dynamic burning rates and on developing a comprehensive analytical model of the experiment. Features of the model include the energy equation, heat-up to ignition, generalized real gas effects, and dynamic burning. Calculated results lead to improved methods for analyzing and reporting closed chamber results so as to include information on the dynamic processes that dominate ignition and the early stages of pressurization.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1975
Accession Number
ADA017747

Entities

People

  • Carl W. Nelson
  • Leonard H. Caveny
  • Martin Summerfield

Organizations

  • Princeton University

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Burning Rate
  • Combustion
  • Differential Equations
  • Double Base Propellants
  • Dynamic Response
  • Equations
  • Heat Flux
  • Heat Loss
  • Heat Of Combustion
  • Heat Transfer
  • High Pressure
  • Ignition Lag
  • Pressurization
  • Production Control
  • Propellants
  • Solid Propellants
  • Specific Heat

Fields of Study

  • Physics

Readers

  • Computational Modeling and Simulation
  • Rocket Propulsion.
  • Theoretical Analysis.