• DocumentCode
    868435
  • Title

    Ablation Study in a Capillary Sustained Discharge

  • Author

    Keidar, Michael ; Boyd, Iain D. ; Williams, Anthony ; Beyer, Richard

  • Author_Institution
    Dept. of Aerosp. Eng., Michigan Univ., Ann Arbor, MI
  • Volume
    43
  • Issue
    1
  • fYear
    2007
  • Firstpage
    308
  • Lastpage
    312
  • Abstract
    Electrothermal-chemical ignition systems have been demonstrated in gun systems to provide desirable characteristics including reproducible shorter ignition delays. We present a combined theoretical and experimental study of the capillary discharge with an aim to develop a capillary plasma source with efficient energy conversion. The major emphasis in the present capillary discharge model is the ablation phenomenon. Consideration is given to different characteristic subregions near the ablated surface: namely, a space-charge sheath, a Knudsen layer, and a hydrodynamic layer. A kinetic approach is used to determine the parameters at the interface between the kinetic Knudsen layer and the hydrodynamic layer. Coupling the solution of the nonequilibrium Knudsen layer with the hydrodynamic layer provides a self-consistent solution for the ablation rate. According to the model predictions, the peak electron temperature is about 1.4 eV, the polyethylene surface temperature is about 700 K, and the pressure is about 10 MPa in the case of a 0.6 kJ discharge. In parallel, a parametric experimental study of the capillary ablation process is conducted. The ablation rates are measured for capillary tubes made of polyethylene and Teflon. Both experimental measurements and simulations indicate that the ablated mass increases with the peak discharge current and that a smaller diameter capillary yields a larger ablated mass. It is found that model predictions agree well with experimental measurements
  • Keywords
    delays; discharges (electric); electrothermal launchers; hydrodynamics; ignition; plasma sheaths; plasma sources; space charge; Knudsen layer; Teflon; ablation; capillary plasma source; capillary sustained discharge; capillary tube; electrothermal-chemical ignition systems; gun system; hydrodynamic layer; polyethylene; reproducible shorter ignition delays; space-charge sheath; Delay; Electrothermal launching; Fault location; Hydrodynamics; Ignition; Kinetic theory; Plasma temperature; Polyethylene; Predictive models; Surface discharges; Ablation; capillary discharge; electrothermal chmical (ETC); plasma; propellant;
  • fLanguage
    English
  • Journal_Title
    Magnetics, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9464
  • Type

    jour

  • DOI
    10.1109/TMAG.2006.887672
  • Filename
    4033064