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- W4361763714 abstract "As an advanced propulsion technology, electric propulsion has been widely used in foreign aerospace fields, but its application in China has just started. Due to the high voltage and high power characteristics of the PPU supplied by the electric propulsion system, the on-orbit work is prone to high voltage discharge, which has become the main mode of the on-orbit effective of PPU and the key factor affecting the promotion and application of electric propulsion in China. In this paper, the high voltage discharge occurred in electric propulsion PPU of an in-orbit test satellite in China is analyzed through ground verification test, and the technical method of high voltage insulation protection design for aerospace application is put forward, which provides an important technical guarantee for the high reliable electric propulsion aerospace application in China." @default.
- W4361763714 created "2023-04-04" @default.
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- W4361763714 date "2023-01-01" @default.
- W4361763714 modified "2023-09-27" @default.
- W4361763714 title "High Voltage Discharge and Insulation Design for Aerospace Applications" @default.
- W4361763714 cites W2312395837 @default.
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- W4361763714 doi "https://doi.org/10.1007/978-981-99-0357-3_11" @default.
- W4361763714 hasPublicationYear "2023" @default.
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