Effect of Temperature Sensitivity and Plasticizer Diffusive Transport on Performance of Layered Solid Propellants under Electrothermal Plasma Injection

Abstract

The temperature of the propellant's bed may play a role in the burn rates under plasma injection. In this report, a set of experiments was first conducted on the plasma-flow field to determine the spatial and temporal distribution of the plasma temperature, pressure, number density, and velocity. The experiments revealed a decreasing plasma pressure, plasma temperature, and plasma number density as plasma is leaving the capillary source and expands in air. The plasma jet velocity 2 inches from the source exit was found to be about 1300 m/s. Following characterization of the plasma-flow field, a set of experiments was conducted on JA-2 solid propellant with controlled bed temperature. Experiments, with proposed models, revealed a functional form that includes the bed temperature. Increased burn rates were observed with increased bed temperature, which appears to follow a power law. A model for the burn rate is proposed, which includes the bed temperature and has the burn rate equals A P(a) (T/T ambient)(b). Further investigation of plasma parameters helped to modify the proposed model to include plasma radiative heat flux and plasma number density. (6 tables, 19 figures, 29 refs.)

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Mar 29, 2002
Accession Number
ADA412214

Entities

People

  • Mohamed A. Bourham

Organizations

  • North Carolina State University

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Ballistics
  • Chemical Reactions
  • Combustion
  • Emission Spectroscopy
  • Engineering
  • Equations
  • Exterior Ballistics
  • Heat Energy
  • Measurement
  • Pressure Distribution
  • Pressure Transducers
  • Propellants
  • Solid Propellants
  • Spatial Distribution
  • Spectra
  • Spectroscopy
  • Static Pressure

Readers

  • Computational Modeling and Simulation
  • Pulsed Power and Plasma Physics.
  • Rocket Propulsion.