TY - GEN
T1 - Research on Measurement Method for Secondary Electron Emission Coefficient of Aerospace Material
AU - Sizhan, Wang
AU - Zhihao, Wang
AU - Xiangyu, Nie
AU - Xiaoyi, Yang
N1 - Publisher Copyright:
© 2024 IEEE.
PY - 2024
Y1 - 2024
N2 - When charged particles incident on the material surface, they will excite secondary electrons and backscattered electrons from the material surface. For low conductivity dielectric materials, the emission of secondary electrons is one of the important mechanisms that cause the surface charging of the material. As the spacecraft surface contains materials with different secondary electron emission coefficients, there is a risk of electrostatic discharge between materials as a result of differential charging, so it is necessary to study the relationship between secondary electron emission and spacecraft surface charging. This paper introduces a measurement method of secondary electron emission coefficient of dielectric materials, using pulsed electron beam together with ultraviolet lamp to neutralize the charged surface during the measurement, and combines the results of secondary electron emission coefficient of typical aerospace materials (Gold, Aluminum, Single-sided Aluminum Plated Kapton™, Double-sided Aluminum Plated F46, Carburized Kapton™, and Polyester Film) to study the impact of secondary electron emission on the surface charging level of spacecraft, laying the foundation for carrying out spacecraft electrostatic protection.
AB - When charged particles incident on the material surface, they will excite secondary electrons and backscattered electrons from the material surface. For low conductivity dielectric materials, the emission of secondary electrons is one of the important mechanisms that cause the surface charging of the material. As the spacecraft surface contains materials with different secondary electron emission coefficients, there is a risk of electrostatic discharge between materials as a result of differential charging, so it is necessary to study the relationship between secondary electron emission and spacecraft surface charging. This paper introduces a measurement method of secondary electron emission coefficient of dielectric materials, using pulsed electron beam together with ultraviolet lamp to neutralize the charged surface during the measurement, and combines the results of secondary electron emission coefficient of typical aerospace materials (Gold, Aluminum, Single-sided Aluminum Plated Kapton™, Double-sided Aluminum Plated F46, Carburized Kapton™, and Polyester Film) to study the impact of secondary electron emission on the surface charging level of spacecraft, laying the foundation for carrying out spacecraft electrostatic protection.
KW - plasma formatting
KW - secondary electron
KW - spacecraft surface charging
UR - https://www.scopus.com/pages/publications/85205732146
U2 - 10.1109/ICEICT61637.2024.10671164
DO - 10.1109/ICEICT61637.2024.10671164
M3 - 会议稿件
AN - SCOPUS:85205732146
T3 - 2024 IEEE 7th International Conference on Electronic Information and Communication Technology, ICEICT 2024
SP - 587
EP - 592
BT - 2024 IEEE 7th International Conference on Electronic Information and Communication Technology, ICEICT 2024
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 7th IEEE International Conference on Electronic Information and Communication Technology, ICEICT 2024
Y2 - 31 July 2024 through 2 August 2024
ER -