An Investigation of the Effects of Acceleration on the Burning Rates of Solid Propellants

Abstract

The acceleration sensitivity of aluminized and nonmetallized composite and double-base propellants were investigated. A review of previous experimental findings and current analytical models was also conducted. An investigation was conducted to determine the cause(s) for the differences in burning rate augmentation data reported by various investigators. Strand length (burn time) was found to be the dominant factor. Lead and copper additives commonly found in double-base propellants were found to decrease the burning rate with increasing acceleration. Burning rate instability was also obtained at high accelerations. The addition of aluminum increased the burning rate at any given acceleration.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1969
Accession Number
AD0863519

Entities

People

  • David W. Netzer
  • M. J. Bulman
  • R. C. Bates
  • W. Bringhurst Jr.

Organizations

  • Naval Postgraduate School

Tags

DTIC Thesaurus Topics

  • Additives (Chemicals)
  • Aluminum Oxides
  • Ammonium Perchlorate
  • Burning Rate
  • Chemical Reaction Properties
  • Combustion
  • Composite Materials
  • Composite Propellants
  • Double Base Propellants
  • Energy
  • Floods
  • Fuel Additives
  • Iron Oxides
  • Oxides
  • Reynolds Number
  • Solid Propellants
  • Standards

Fields of Study

  • Physics

Readers

  • Rocket Propulsion.