Fast-Burning Rate/High Slope Propellant Technology Program

Abstract

Two candidate propellant formulations, ANB-3394 and ANB-3395-1, were developed that satisfied all the technical goals. Additionally, these propellants were successfully test fired in small scale motors verifying propellant ballistic properties, excellent liner propellant bonds, and propellant processability adequate for good grains. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1971
Accession Number
AD0517602

Entities

People

  • A. Katzakian
  • R. L. Lou

Organizations

  • Aerojet Rocketdyne Holdings

Tags

DTIC Thesaurus Topics

  • Ammonium Perchlorate
  • Burning Rate
  • Ceramic Materials
  • Combustion
  • Curing Agents
  • Explosives
  • Ignition
  • Iron Oxides
  • Materials Testing
  • Measurement
  • Mechanical Properties
  • Particle Size
  • Plastic Explosives
  • Shear Stresses
  • Tensile Strength
  • Test And Evaluation
  • Test Methods

Fields of Study

  • Physics

Readers

  • Rocket Propulsion.
  • Software Engineering