DocumentCode :
482442
Title :
An experimental study of local magnetic field intensity effects on the discharge characterization of Hall thrusters
Author :
Peng, E. ; Yu, Daren ; Han, Ke ; Shang, Fang ; Chen, Chao ; Zhao, Xin-shuang ; Zhan, Yan
Author_Institution :
Harbin Inst. of Technol., Harbin
fYear :
2008
fDate :
17-20 Oct. 2008
Firstpage :
920
Lastpage :
925
Abstract :
This paper investigates the magnetic field intensity effects on the discharge characterization of Hall thrusters for optimization of the magnetic fields. Vary the strength of magnetic fields with its topography holds constant (keep in ldquofocusingrdquo type), and make an experimental study of the thrusterpsilas operating performance working in different regions of magneto-ampere curve through Langmuir probe, spectrograph, etc. Detailed examination of the results shows that when the magnitude of magnetic field intensity less than its critical value, near-wall conductivity give priority to the activity that electrons traverse the magnetic field, if not, discharge current varying with magnetic field intensity abnormally, and existing electrons conductive theories are failed to explain this phenomenon.
Keywords :
aerospace propulsion; magnetic field effects; plasma accelerators; Hall thrusters; discharge characterization; local magnetic field intensity effects; Acceleration; Chaos; Conductivity; Electrons; Ionization; Magnetic fields; Plasma accelerators; Plasma sheaths; Probes; Surfaces;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electrical Machines and Systems, 2008. ICEMS 2008. International Conference on
Conference_Location :
Wuhan
Print_ISBN :
978-1-4244-3826-6
Electronic_ISBN :
978-7-5062-9221-4
Type :
conf
Filename :
4770846
Link To Document :
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