TY - JOUR
T1 - Characteristics of dusty plasma sheath over a spacecraft surface near Jupiter’s ring with oblique magnetic field and non-extensive electrons
AU - Chen, Long
AU - Tan, Congqi
AU - Fa, Meichen
AU - Duan, Ping
AU - Liu, Miao
AU - Liu, Xintong
AU - Chen, Junyu
AU - Liu, Yang
AU - Cui, Wanxin
AU - Zheng, Bocong
N1 - Publisher Copyright:
© 2025 IOP Publishing Ltd. All rights, including for text and data mining, AI training, and similar technologies, are reserved.
PY - 2025/6/23
Y1 - 2025/6/23
N2 - Space plasma significantly affects spacecraft charging, and accurate sheath modeling is essential for predicting surface potential and mitigating related issues. This study investigates the characteristics of a dusty plasma sheath near a spacecraft surface in an oblique magnetic field using a 1D3V fluid model, where electrons follow a non-extensive distribution. A modified orbital-motion-limited model is used to determine the dust charge. The dust surface potential shows distinct behavior at the sheath edge and in the bulk region. By employing the Sagdeev potential method, a generalized Bohm criterion incorporating dust charging is derived. Results show that the effective Bohm velocity decreases with increasing dust radius, reflecting the strong influence of dust on sheath structure. The results reveal that as the dust particle radius decreases, the sheath floating potential increases, intensifying the surface charging effects of spacecraft. A stronger oblique magnetic field increases the positive charging of dust particles, thereby modifying the sheath structure. A key finding is that dust particles near the floating wall carry significantly lower charges than previously predicted, due to the coupling between the dust charging process and the floating potential condition. Additionally, a sub-extensive electron distribution leads to a higher wall potential than in the super-extensive case, further amplifying spacecraft charging effects.
AB - Space plasma significantly affects spacecraft charging, and accurate sheath modeling is essential for predicting surface potential and mitigating related issues. This study investigates the characteristics of a dusty plasma sheath near a spacecraft surface in an oblique magnetic field using a 1D3V fluid model, where electrons follow a non-extensive distribution. A modified orbital-motion-limited model is used to determine the dust charge. The dust surface potential shows distinct behavior at the sheath edge and in the bulk region. By employing the Sagdeev potential method, a generalized Bohm criterion incorporating dust charging is derived. Results show that the effective Bohm velocity decreases with increasing dust radius, reflecting the strong influence of dust on sheath structure. The results reveal that as the dust particle radius decreases, the sheath floating potential increases, intensifying the surface charging effects of spacecraft. A stronger oblique magnetic field increases the positive charging of dust particles, thereby modifying the sheath structure. A key finding is that dust particles near the floating wall carry significantly lower charges than previously predicted, due to the coupling between the dust charging process and the floating potential condition. Additionally, a sub-extensive electron distribution leads to a higher wall potential than in the super-extensive case, further amplifying spacecraft charging effects.
KW - Bohm criterion
KW - dusty plasma
KW - magnetized sheath
KW - non-extensive distribution
UR - http://www.scopus.com/inward/record.url?scp=105008451950&partnerID=8YFLogxK
U2 - 10.1088/1361-6463/ade166
DO - 10.1088/1361-6463/ade166
M3 - Article
AN - SCOPUS:105008451950
SN - 0022-3727
VL - 58
JO - Journal of Physics D: Applied Physics
JF - Journal of Physics D: Applied Physics
IS - 25
M1 - 255204
ER -