Experimental Study of Plasma-Propellant Interactions

Abstract

The use of a plasma as an ignition source has revealed several attractive benefits over conventional igniter systems, such as a shorter ignition delay, reduced temperature sensitivity of the propellant, better controlled propellant mass generation rates, and reduced susceptibility to anomalous ignition transients. However, the causes of these attractive benefits at a fundamental level are not well understood. To address the issues in this experimental program, different diagnostic tools are used, including high-speed photography, fast-response heat flux gages, and species measurements using a micro-probe mass spectrometer. Tests with homogeneous and composite propellants, including JA-2 and an azido/AP propellant, were conducted to determine the conditions required for ignition.

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Document Details

Document Type
Technical Report
Publication Date
Jun 19, 2001
Accession Number
ADP012129

Entities

People

  • Stefan T. Thynell
  • Thomas A. Litzinger

Organizations

  • Pennsylvania State University

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Blood
  • Chemical Reactions
  • Chemistry
  • Combustion
  • Composite Propellants
  • Electrical Circuits
  • Films
  • Heat Flux
  • Ignition
  • Ignition Lag
  • Mass Spectrometers
  • Measurement
  • Propellants
  • Radiation
  • Resistance
  • Spectrometers
  • Thermal Radiation

Fields of Study

  • Physics

Readers

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