Deflagration to Shock to Detonation Transition of Energetic Propellants.

Abstract

It is well known that explosive-based propellants are susceptible to detonation from the controlled deflagration mode of combustion. In some instances a confined zone of granulated propellant adjacent to a zone of cast propellant can provide a rapid enough pressure-rise rate to shock initiate the cast material. If the cast propellant has voids, the detonation will initiate at some location ahead of the granulated bed/cast material interface. This report is a summary of the research activities that focus on the analysis and modeling of the physics of such highly transient flows.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1984
Accession Number
ADA144469

Entities

People

  • C. Cudak
  • H. Krier
  • P. B. Butler

Organizations

  • University of Illinois Urbana–Champaign

Tags

Communities of Interest

  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Burning Rate
  • Chemical Reactions
  • Combustion
  • Decomposition
  • Detonation Waves
  • Differential Equations
  • Energy Transfer
  • Explosions
  • Explosives
  • Heat Transfer
  • Industrial Engineering
  • Materials
  • Materials Laboratories
  • Propellants
  • Rocket Engines
  • Solid Propellants
  • Steady State

Fields of Study

  • Physics

Readers

  • Rocket Propulsion.