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