DocumentCode
86862
Title
Influence of Electron and Ion Thermodynamics on the Magnetic Nozzle Plasma Expansion
Author
Merino, Mario ; Ahedo, Eduardo
Author_Institution
Univ. Carlos III de Madrid, Leganés, Spain
Volume
43
Issue
1
fYear
2015
fDate
Jan. 2015
Firstpage
244
Lastpage
251
Abstract
A two-fluid 2-D model of the supersonic plasma flow in a propulsive magnetic nozzle (MN) is extended to include simple electron and ion thermodynamics to study the effects of electron cooling and ion thermal energy on the expansion. A faster electron cooling rate is seen to reduce plasma jet divergence, increase radial rarefaction, and enhance detachment from the closed magnetic lines. Ion thermal energy is converted to directed kinetic energy by the MN without the mediation of an ambipolar electric field, and alters the electric response of the plasma.
Keywords
nozzles; plasma jets; plasma simulation; plasma temperature; plasma thermodynamics; plasma-wall interactions; supersonic flow; ambipolar electric field; electron cooling rate; electron-ion thermodynamics; ion temperature; ion thermal energy; magnetic nozzle plasma expansion; plasma jet; plasma-wall interactions; radial rarefaction; supersonic plasma flow; two-fluid 2D model; Cooling; Electron tubes; Ions; Isothermal processes; Magnetic separation; Manganese; Plasmas; Plasma accelerators; plasma devices; plasma simulation; plasma temperature; propulsion; propulsion.;
fLanguage
English
Journal_Title
Plasma Science, IEEE Transactions on
Publisher
ieee
ISSN
0093-3813
Type
jour
DOI
10.1109/TPS.2014.2316020
Filename
6851173
Link To Document