Experimental Study of Plasma/Propellant Interactions

Abstract

The overall objective of the project was to improve our understanding of the various chemical and physical processes that occur during ignition by the plasma igniter. During the project period, electrical circuits, experimental setups were designed and manufactured, as well as data acquisition systems were acquired. The following primary findings have been obtained from this project: 1) to achieve ignition, a closed chamber configuration is needed, 2) JA2 propellant is readily ignitable, whereas nitramine-composite propellants show a two-stage mass generation behavior, 3) recovered samples from JA2 show changes in surface and sub-surface structure, in-depth melting, vaporization and chemical reactions, 4) recombination rates among plasma species are high, resulting in measurement of hydrocarbons at the surface having molecular weights from 1 to about 30 (H, H2, C, CH, CH2, etc.) and primarily NO, HCO and H2CO from propellants, 5) the radiative heat flux reaches a maximum when the electrical power conversion reaches a maximum, 6) the UV component is significant, and 7) the near-surface emission from the plasma is significantly reduced compared to peak values due to plasma expansion and to rapid heat losses by radiation.

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Document Details

Document Type
Technical Report
Publication Date
Apr 23, 2004
Accession Number
ADA424481

Entities

People

  • Stefan T. Thynell
  • Thomas A. Litzinger

Organizations

  • Pennsylvania State University

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Chemical Reactions
  • Combustion
  • Composite Propellants
  • Data Acquisition
  • Electrical Circuits
  • Energy
  • Heat Flux
  • Heat Transfer
  • Ignition
  • Mass Spectrometers
  • Mass Spectrometry
  • Materials
  • Materials Science
  • Measurement
  • Peak Values
  • Pressure Measurement
  • Propellants

Fields of Study

  • Physics

Readers

  • Rocket Propulsion.
  • Thermal Physics or Thermal Science.
  • Thin Film Deposition Science.