TY - JOUR
T1 - 微阴极电弧推力器羽流探针诊断研究
AU - Wang, Shuai
AU - Liu, Xiangyang
AU - Zhao, Zijing
AU - Guo, Haoran
AU - Geng, Jinyue
AU - Shen, Yan
AU - Wang, Ningfei
N1 - Publisher Copyright:
© 2023 Chinese Academy of Space Technology. All rights reserved.
PY - 2023/4/25
Y1 - 2023/4/25
N2 - Owing to the characteristics of low power and simple structure, micro-cathode arc thruster((iCAT)meets the mission requirements of micro-nano satellites, and thus has a good development prospect. The diagnosis of (iCAT plume can reveal the acceleration mechanism of the thruster, which is of great significance for improving the performance of jmCAT. The electron temperature, electron density and ion velocity at different positions of jmCAT plume were obtained by using Langmuir three-probe. The effects of external magnetic field, charging time and cathode material on plasma characteristics and ion velocity were investigated. The results show that the plasma generated at the initial stage of fiCAT discharge has the characteristics of higher electron temperature and density. As the plume moves downstream, electron temperature and electron density decrease, and ion velocity increases. With the stronger external magnetic field, electron temperature and ion velocity increase, and electron density decreases. The electron density of the central axis of thruster is improved effectively when the external magnetic field is shifted to the downstream of thruster. As the charging time of juCAT is longer, the electron temperature, electron density and ion velocity increase.compared with CuW and AgW cathodes!the electron temperature of Ti cathode plume is higher and electron density is lower.
AB - Owing to the characteristics of low power and simple structure, micro-cathode arc thruster((iCAT)meets the mission requirements of micro-nano satellites, and thus has a good development prospect. The diagnosis of (iCAT plume can reveal the acceleration mechanism of the thruster, which is of great significance for improving the performance of jmCAT. The electron temperature, electron density and ion velocity at different positions of jmCAT plume were obtained by using Langmuir three-probe. The effects of external magnetic field, charging time and cathode material on plasma characteristics and ion velocity were investigated. The results show that the plasma generated at the initial stage of fiCAT discharge has the characteristics of higher electron temperature and density. As the plume moves downstream, electron temperature and electron density decrease, and ion velocity increases. With the stronger external magnetic field, electron temperature and ion velocity increase, and electron density decreases. The electron density of the central axis of thruster is improved effectively when the external magnetic field is shifted to the downstream of thruster. As the charging time of juCAT is longer, the electron temperature, electron density and ion velocity increase.compared with CuW and AgW cathodes!the electron temperature of Ti cathode plume is higher and electron density is lower.
KW - Langmuir probe
KW - ion velocity
KW - micro-cathode arc thruster
KW - plasma characteristic
KW - plume diagnosis
UR - http://www.scopus.com/inward/record.url?scp=85160687626&partnerID=8YFLogxK
U2 - 10.16708/j.cnki.1000-758X.2023.0019
DO - 10.16708/j.cnki.1000-758X.2023.0019
M3 - 文章
AN - SCOPUS:85160687626
SN - 1000-758X
VL - 43
SP - 47
EP - 54
JO - Chinese Space Science and Technology
JF - Chinese Space Science and Technology
IS - 2
ER -