TY - GEN
T1 - Hall thruster with externally driven breathing oscillations
AU - Raitses, Yevgeny
AU - Romadanov, Ivan
AU - Smolyakov, Andrei
AU - Simmonds, Jacob
AU - Kaganovich, Igor
N1 - Publisher Copyright:
© 2019 by American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2019
Y1 - 2019
N2 - Hall thrusters exhibit usually two types of large amplitude low frequency (10-30 kHz) oscillatory modes, so called breathing mode and spoke mode. In our previous works, it was demonstrated that both these modes can be controlled via the external modulations of the discharge voltage applied to the anode or anode segments. Two regimes of the thruster response, linear and nonlinear, have been revealed depending on the modulation amplitude. There was also observed a resonance-kind behavior-the amplitudes of the excited oscillations of the discharge current and the ion current reach their respective maximum as the modulation frequency approaches the frequency of natural oscillations (breathing or spoke). A one-dimensional model explained this result, in part, due to a decrease of the phase between low-frequency oscillations of the plasma density and the electric field. In this paper, we briefly review recent results on a modulated cylindrical Hall thruster. One important practical implication of these results is that the thruster operation with externally driven breathing oscillations may open a new way to implement enhanced thrust-to-power ratio Hall thrusters.
AB - Hall thrusters exhibit usually two types of large amplitude low frequency (10-30 kHz) oscillatory modes, so called breathing mode and spoke mode. In our previous works, it was demonstrated that both these modes can be controlled via the external modulations of the discharge voltage applied to the anode or anode segments. Two regimes of the thruster response, linear and nonlinear, have been revealed depending on the modulation amplitude. There was also observed a resonance-kind behavior-the amplitudes of the excited oscillations of the discharge current and the ion current reach their respective maximum as the modulation frequency approaches the frequency of natural oscillations (breathing or spoke). A one-dimensional model explained this result, in part, due to a decrease of the phase between low-frequency oscillations of the plasma density and the electric field. In this paper, we briefly review recent results on a modulated cylindrical Hall thruster. One important practical implication of these results is that the thruster operation with externally driven breathing oscillations may open a new way to implement enhanced thrust-to-power ratio Hall thrusters.
UR - https://www.scopus.com/pages/publications/85095979281
UR - https://www.scopus.com/inward/citedby.url?scp=85095979281&partnerID=8YFLogxK
U2 - 10.2514/6.2019-4078
DO - 10.2514/6.2019-4078
M3 - Conference contribution
AN - SCOPUS:85095979281
SN - 9781624105906
T3 - AIAA Propulsion and Energy Forum and Exposition, 2019
BT - AIAA Propulsion and Energy Forum and Exposition, 2019
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Propulsion and Energy Forum and Exposition, 2019
Y2 - 19 August 2019 through 22 August 2019
ER -