TY - GEN
T1 - Effect of density inhomogeneity in azimuth on discharge oscillation suppression and electron diffusion in hall thrusters
AU - Bak, Junhwi
AU - Kawashima, Rei
AU - Komurasaki, Kimiya
AU - Koizumi, Hiroyuki
N1 - Funding Information:
This work was supported by JSPS KAKENHI Grant Number 18J14592.
Publisher Copyright:
© 2018, American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
PY - 2018
Y1 - 2018
N2 - Azimuthal non-uniform propellant supply operation shows representative characteristics of suppressed discharge oscillation and increased axial electron current. These characteristics implicate that, with non-uniform operation, physics underlying oscillation and electron transport in Hall thrusters may be able to be studied in a spatiotemporally less strict experimental setup. From this insight, we investigated azimuthal plasma properties of non-uniform propellant operation and its influences on discharge oscillation and electron cross-field transport. The image analysis result reveals non-linear plasma structures elongated in direction of electron azimuthal E × B drift, showing the structure is governed by electrons. From probe measurements, inhomogeneous electron temperature distribution in azimuth direction is observed, and corresponding azimuthal inharmonic ionization is thought to partially contributes to the suppressed discharge oscillation. Also, macroscopic zeroth order azimuthal distribution of plasma potential and electron density shows the distribution is self-consistently generated in a way to enhance electron cross-field drift towards the anode. We estimated amount of current carried by equilibrium zeroth order distribution, which accounts for about 20% of total increased electron current in the non-uniform operation. The physical similarities of the macroscopic transport to microscopic instability induced electron transport are also compared.
AB - Azimuthal non-uniform propellant supply operation shows representative characteristics of suppressed discharge oscillation and increased axial electron current. These characteristics implicate that, with non-uniform operation, physics underlying oscillation and electron transport in Hall thrusters may be able to be studied in a spatiotemporally less strict experimental setup. From this insight, we investigated azimuthal plasma properties of non-uniform propellant operation and its influences on discharge oscillation and electron cross-field transport. The image analysis result reveals non-linear plasma structures elongated in direction of electron azimuthal E × B drift, showing the structure is governed by electrons. From probe measurements, inhomogeneous electron temperature distribution in azimuth direction is observed, and corresponding azimuthal inharmonic ionization is thought to partially contributes to the suppressed discharge oscillation. Also, macroscopic zeroth order azimuthal distribution of plasma potential and electron density shows the distribution is self-consistently generated in a way to enhance electron cross-field drift towards the anode. We estimated amount of current carried by equilibrium zeroth order distribution, which accounts for about 20% of total increased electron current in the non-uniform operation. The physical similarities of the macroscopic transport to microscopic instability induced electron transport are also compared.
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U2 - 10.2514/6.2018-4424
DO - 10.2514/6.2018-4424
M3 - Conference contribution
AN - SCOPUS:85066474939
SN - 9781624105708
T3 - 2018 Joint Propulsion Conference
BT - 2018 Joint Propulsion Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 54th AIAA/SAE/ASEE Joint Propulsion Conference, 2018
Y2 - 9 July 2018 through 11 July 2018
ER -