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
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