TY - GEN
T1 - Dielectric Charging of Polyetheretherketone Insulation Used in Spacecraft Superimposed DC Voltage
AU - Bu, Wen
AU - Wang, Weiwang
AU - Zheng, Shusai
AU - Li, Shengtao
N1 - Publisher Copyright:
© 2019 IEEE.
PY - 2019/10
Y1 - 2019/10
N2 - Spacecraft charging of dielectrics superimposed dc voltage is a key issue in insulation that exposed in the space environment. In this paper, charge deposition, transport, accumulation of polyetheretherketone (PEEK) dielectric were studied under electron irradiation (0.3 MeV and 5×10-7 A/m2). The effects of operating voltage on the charging process were considered. A 2D finite element simulation model was conducted for modeling the charging in a plate sample structure. The operating voltage ranges from -5 kV to +5 kV. Charge transport process considering the energy deposition of the irradiated electrons, the radiation-induced conduction, and the charge injection was employed in the modeling. The calculation results indicate that the charging results of PEEK material present a rapid charging rate by the electron beam. Positive voltages can decrease the surface potential, while it has little influence on the space charge and the electric field inside the sample. For example, the maximum electric field difference between ±5 kV operating voltages is 2.06 kV/m, but the surface potential difference is 10152V. It can be concluded that a high surface potential with a rapid charging rate occurs in the PEEK material under the electron beam superimposed the dc voltage. The applied voltage affects the electron energy so as to the change of dielectric charging processes.
AB - Spacecraft charging of dielectrics superimposed dc voltage is a key issue in insulation that exposed in the space environment. In this paper, charge deposition, transport, accumulation of polyetheretherketone (PEEK) dielectric were studied under electron irradiation (0.3 MeV and 5×10-7 A/m2). The effects of operating voltage on the charging process were considered. A 2D finite element simulation model was conducted for modeling the charging in a plate sample structure. The operating voltage ranges from -5 kV to +5 kV. Charge transport process considering the energy deposition of the irradiated electrons, the radiation-induced conduction, and the charge injection was employed in the modeling. The calculation results indicate that the charging results of PEEK material present a rapid charging rate by the electron beam. Positive voltages can decrease the surface potential, while it has little influence on the space charge and the electric field inside the sample. For example, the maximum electric field difference between ±5 kV operating voltages is 2.06 kV/m, but the surface potential difference is 10152V. It can be concluded that a high surface potential with a rapid charging rate occurs in the PEEK material under the electron beam superimposed the dc voltage. The applied voltage affects the electron energy so as to the change of dielectric charging processes.
UR - https://www.scopus.com/pages/publications/85081666630
U2 - 10.1109/CEIDP47102.2019.9009689
DO - 10.1109/CEIDP47102.2019.9009689
M3 - 会议稿件
AN - SCOPUS:85081666630
T3 - Annual Report - Conference on Electrical Insulation and Dielectric Phenomena, CEIDP
SP - 434
EP - 437
BT - 2019 IEEE Conference on Electrical Insulation and Dielectric Phenomena, CEIDP 2019 - Proceedings
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2019 IEEE Conference on Electrical Insulation and Dielectric Phenomena, CEIDP 2019
Y2 - 20 October 2019 through 23 October 2019
ER -