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
Link To Document :
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