2009 Fiscal Year Final Research Report
Development of Mitigation Method of GEO Spacecraft Charging using a passive field-electron emitter
Project/Area Number |
19206090
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Research Category |
Grant-in-Aid for Scientific Research (A)
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Allocation Type | Single-year Grants |
Section | 一般 |
Research Field |
Aerospace engineering
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Research Institution | Kyushu Institute of Technology |
Principal Investigator |
CHO Mengu Kyushu Institute of Technology, 工学研究院, 教授 (60243333)
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Co-Investigator(Kenkyū-buntansha) |
TOYODA Kazuhiro 九州工業大学, 工学研究院・電気電子工学研究系, 准教授 (10361411)
IWATA Minoru 九州工業大学, 工学研究院・先端機能システム工学研究系, 助教 (80396762)
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Project Period (FY) |
2007 – 2009
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Keywords | 航空宇宙流体 / 構造 / 航法 / 制御 / 推進 / 衛星帯電 |
Research Abstract |
Passive electron emission device that can emit electrons automatically from a satellite to prevent accident due to charging and arcing in Geosynchronous Orbit. Prototypes were made via micro-etching of laminar film made by copper and polyimide. Design modification and evaluation were repeated. It was confirmed that the emitter has a sufficient electron emission performance and strength against long-time exposure to space environment. Physical mechanism of electron emission was studied. Computer simulation showed that the emitter could mitigate the charging in orbit.
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[Journal Article] Development of Electron-emitting Film for Spacecraft Charging Mitigation: Observation, Endurance and Simulations2009
Author(s)
M. Cho, T. Okumura, M. Iwata, K. Toyoda, H. Igawa, Y. Fujiwara, S. Hatta, T. Satou, T. Fujita
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Journal Title
AIAA-2009-560, 47th AIAA Aerospace Science Meeting 20090100
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[Journal Article] Development of Electron Emitting Film for Spacecraft Charging Mitigation2007
Author(s)
Minoru IWATA, Hideyuki IGAWA, Takayuki OSE, Yuki HARAGUCHI, Yuya SANMARU, Hirokazu MASUI, Satoshi HOSODA, Kazuhiro TOYODA, Mengu CHO, Tatsuhiro FUJITA
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Journal Title
58th International Astronautical Congress, Hyderabad
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