Schlieren Study of Composite Propellant Combustion.

Abstract

A photographic investigation of metallized and non-metallized composite solid propellant combustion was made. Propellant strands made from large unimodal AP and PBAN binder, both with and without aluminum powder, were burned in a conventional stainless steel combustion bomb. High speed color Schlieren motion pictures were taken of the combustion process to determine the effects of pressure and strand thickness on propellant deflagration. Results are discussed and compared with data on AP/binder sandwich experiments. (Author)

Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1974
Accession Number
AD0781343

Entities

People

  • Robert Ross Gerhardt

Organizations

  • Naval Postgraduate School

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aluminum
  • Combustion
  • Composite Materials
  • Composite Propellants
  • Deflagration
  • Energetic Materials
  • Materials
  • Motion Pictures
  • Propellants
  • Solid Propellants
  • Stainless Steel
  • Steel
  • Thickness

Fields of Study

  • Physics

Readers

  • Rocket Propulsion.