研究者詳細 - 趙　孟佑

論文 - 趙　孟佑

分割表示643 件中 301 - 320 件目／全件表示 >>

Effect of Energetic Electron and Proton Irradiation on Electron Emission Yield of Polyimide Induced by Electron and Photon"（共著）査読有り

Jiang Wu, Akira Miyahara, Minoru Iwata, Kazuhiro Toyoda, Mengu Cho, Xiaoquan Zheng

29th International Symposium on Space Technology and Science 2013年06月

Comparison of Thermal Distribution within a 50 cm class satellite in Vacuum and Atmosphere Environment（共著）査読有り

Hirokazu Masui, Yuki Seri, Toru Hatamura, Mengu Cho

29th International Symposium on Space Technology and Science 2013年06月

Basic Research on Vibration Test Level for Nanosatellite Components（共著）査読有り

Kenta Tomida, Amgalanbat Batsuren, Toru Hatamura, Hirokazu Masui, Mengu Cho

29th International Symposium on Space Technology and Science 2013年06月

Development of a shock test method suitable for nano-satellites; basic study（共著）査読有り

Toru Hatamura, Shingo Kimoto, Hirokazu Masui, Mengu Cho, Kazuo Maeno

29th International Symposium on Space Technology and Science 2013年06月

Effects of Energetic Electron and Proton Irradiation on Electron Emission Yield of Polyimide Induced by Electron and Photon（共著）査読有り

J. Wu, A. Miyahara, A. R. Khan, M. Iwata, K. Toyoda, M. Cho, X. Q. Zheng

29th International Symposium on Space Technology and Science 2013年06月

Time and Space Redundancy Fault Tolerance Trade-offs for FPGA Based Single and Multicore Designs（共著）査読有り

Mohamed Mahmoud Ibrahim, Kenichi Asami, Mengu Cho

29th International Symposium on Space Technology and Science 2013年06月

LEO Single Event Upset Emulator for Validation of FPGA Based Avionics Systems（共著）査読有り

Mohamed Mahmoud Ibrahim, Kenichi Asami, Mengu Cho

29th International Symposium on Space Technology and Science 2013年06月

Laboratory Test of Vibration of Micro/Nano Satellite for Environment Test Standardization(共著）査読有り

Amgalanbat Batsuren, Toru Hatamura, Hirokazu Masui, Mengu Cho

29th International Symposium on Space Technology and Science 2013年06月

Results of 300V Photovoltaic Power generation Mission Onboard Horyu-2（共著）査読有り

Shunsuke Iwai, Kyutech Satellite Project, Hirokazu Masui, Minoru Iwata,Kazuhiro Toyoda, Mengu Cho

29th International Symposium on Space Technology and Science 2013年06月

Total Electron Emission Yield Measurement of Polyimide Due to Different Temperatures（共著）査読有り

Akira Miyahara, Wu Jiang, Kazuhiro Toyoda, Mengu Cho

29th International Symposium on Space Technology and Science , Nagoya, Japan 2013年06月

On-orbit results of the power system on-board Nano-satellite Horyu-II（共著）査読有り

Kazuya OKADA, Yuki SERI, Ryunosuke Shibagaki, Kyutech Satellite Project, Hirokazu MASUI, Mengu CHO

29th International Symposium on Space Technology and Science, Nagoya, Japan 2013年06月

Charging/Discharging Test of Lithium-Ion Battery using a Nano-Satellite Power System Made for Nickel-Metal Hydride Battery（共著）査読有り

Takuya Motohata, Kazuya Okada, Hirokazu Masui, Yasuhiro Akahoshi, Mengu Cho

29th International Symposium on Space Technology and Science 2013年06月

In-orbit demonstration of spacecraft charging mitigation of passive electron-emitting film（共著）査読有り

Naoki Matsumoto, Atomu Tanaka, Arifur R Khan, Minoru Iwata, Kazuhiro Toyoda, Mengu Cho

International Symposium on Space Technology and Science 2013年06月

Development of Vacuum Arc Thruster for Nano-Satellite in Low Earth Orbit Plasma　Environment（共著）査読有り

Shingo Fuchikami, Masayoshi Nakamoto, Kazuhiro Toyoda, Mengu Cho

29th International Symposium on Space Technology and Science 2013年06月

Evaluation of SRAM based FPGA Performance by Simulating SEU through Fault Injection（共著）査読有り

Mohamed Mahmoud Ibrahim, Kenichi Asami, Mengu Cho

RAST-2013 2013年06月

Selection of the Commercial-Off-the-Shelf Antistatic Coating and Its Applicability for Space-Use Solar Array（共著）査読有り

Minoru Iwata, Akitoshi Takahashi, Musashi Sakamoto, Mengu Cho, Ryo Muraguchi

Transactions of The Japan Society for Aeronautical and Space Sciences 57 ( 3 ) 153 - 159 2013年04月

In-orbit Demonstration of Newly Developed Passive Electron-emitting Film for Spacecraft Charging Mitigation（共著）査読有り

Arifur R. Khan, Minoru Iwata, Kazuhiro Toyoda, Mengu Cho, Yuta Takaki

Journal of Spacecraft and Rockets 50 ( 4 ) 853 - 859 2013年03月

Investigation on Space Environmental Degradation Effects of Solar Cell Coverglass（共著）査読有り

Yu Chen, Jiang Wu, Teppei Okumura, Masato Takahashi, Taishi Endo, Minoru Iwata, Kazuhiro Toyoda, Mengu Cho

IEEE Transactions on Plasma Science 41 ( 12 ) 3471 - 3476 2013年03月

Special issue on spacecraft charging technology 2013

Cho M., Cooke D., Ferguson D., Garrett H., Hilgers A., Lai S., Roussel J., Toyoda K., Wheelock A.

IEEE Transactions on Plasma Science ( IEEE Transactions on Plasma Science ) 41 ( 12 ) 2013年01月

Mitigation method of preventing secondary arcing on solar array by using capacitor and inductor 査読有り

Haruta I., Shimizu T., Toyoda K., Cho M.

Proceedings of the International Astronautical Congress, IAC 12 9397 - 9403 2013年01月

記述言語：英語掲載種別：研究論文（国際会議プロシーディングス）

Recently, the trend of spacecraft designers has led to the tendency of making larger and multifunctional satellites. In order to achieve the growing demands, the development of a large satellite bus is indispensable. However, electrical discharge accidents have increasingly come to occur on the solar arrays due to the higher bus voltage of any satellite. An electrical discharge on the solar array not only decreases the generating power but also can even halt operation of the satellite entirely. During electrical discharges, various arcing are possible, among which sustained arc is the most detrimental to the satellite. At present, grouting (adhesive is buried between solar cells to which high voltage is applied) is practiced as a mitigation method of sustained arc. However, this method has several disadvantages. Therefore, the development of a new mitigation method is requested. In this paper, we report the effect of mitigation method for sustained arc on solar array, by inserting capacitor and inductor into sustained arc circuit. It is confirmed that sustained arcs were oscillated by the capacitor (i.e. several hundred nF). Therefore, if the oscillation is sufficiently big, sustained arcs can be mitigated. In addition, this paper discusses a relation between flashover current and secondary arc. From the experimental results, when flashover is short, arc current to vibrate and it is suppressed. When flashover is long, arc current can't cut and it isn't suppressed. But, by increasing the capacitance of the capacitor, it was possible to accommodate long flashover discharge. Copyright ©2013 by the International Astronautical Federation.

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