BURNING RATES OF SOLID COMPOSITE PROPELLANTS AT PRESSURES UP TO 20,000 PSIG

Abstract

Strand burning rates of ammonium perchlorate-containing composite propellants having plastisol-nitrocellulose, carboxyl-terminated-polybutadiene, and NF binders have been measured to 20,000 psig. For the first two types and probably the NF type the major influences on burning-rate transition are those resulting from variations in binder type and in oxidizer concentration and particle size; the presence of aluminum or burning-rate promoters has little effect on the pressure-dependence of the burning rate at high pressure. The pressure exponents of plastisol-nitrocellulose formulations reach constant values of 1.0 to 1.3 at about 6000 psi, with little dependence on AP particle size. Carboxyl-terminated-polybutadiene formulations examined give indexes from 0.3 at 2000 psi to 2 up to 10,000 psi, with appreciable AP-particle-size dependence; above 10,000 psi the index decreases to 0.9 and appears to be insensitive to oxidizer size. A proposed model suggests an alteration in the volatilization processes which ensue from differences in pressure-dependence of the respective binder and oxidizer release rates.

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Document Details

Document Type
Technical Report
Publication Date
Sep 15, 1966
Accession Number
AD0375686

Entities

People

  • R. B. Cole

Tags

DTIC Thesaurus Topics

  • Burning Rate
  • Chemical Reactions
  • Combustion
  • Composite Propellants
  • Diagrams
  • Double Base Propellants
  • Dynamic Pressure
  • Materials
  • Measurement
  • Phase
  • Photographs
  • Pressure Measurement
  • Pressurization
  • Schematic Diagrams
  • Solid Propellants
  • Surface Finishing
  • Thermal Shock

Readers

  • Mathematics or Statistics
  • Rocket Propulsion.