DocumentCode
2566706
Title
Research of heaterless thermionic hollow cathode for micro electric propulsion systems
Author
Vekselman, V. ; Krasik, Ya E. ; Gleizer, S. ; Warshavskii, A. ; Rabinovich, L. ; Loyan, A.
Author_Institution
Phys. Dept., Technion - Israel Inst. of Technol., Haifa, Israel
fYear
2012
fDate
8-13 July 2012
Firstpage
5E-05
Lastpage
5E-05
Abstract
Summary form only given. Hollow cathode based on thermionic electron emission serves as crucial component in electric propulsion systems where this cathode used as source of electrons for propellant ionization and ion beam neutralization. In this research, a novel design of the hollow cathode without the heater was studied in the diode mode operation. The simplicity of the cathode design and its unique ignition characteristics (few ms) are attractive features for microsatellite propulsion applications. However, physical processes involved in the cathode ignition, heating and main discharge formation are still poorly understood.
Keywords
aerospace propulsion; diodes; electric ignition; electric propulsion; glow discharges; propellants; thermionic cathodes; thermionic electron emission; cathode ignition characteristics; diode mode operation; discharge formation; heaterless thermionic hollow cathode design; ion beam neutralization; microelectric propulsion system; microsatellite propulsion application; propellant ionization; thermionic electron emission; Cathodes; Discharges (electric); Heating; Ignition; Probes; Propulsion; Thermionic emission;
fLanguage
English
Publisher
ieee
Conference_Titel
Plasma Science (ICOPS), 2012 Abstracts IEEE International Conference on
Conference_Location
Edinburgh
ISSN
0730-9244
Print_ISBN
978-1-4577-2127-4
Electronic_ISBN
0730-9244
Type
conf
DOI
10.1109/PLASMA.2012.6384012
Filename
6384012
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