Development of debris removal method using space plasma interaction
| Project/Area Number |
22656195
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| Research Category |
Grant-in-Aid for Challenging Exploratory Research
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| Allocation Type | Single-year Grants |
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| Research Field |
Aerospace engineering
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| Research Institution | Kyushu Institute of Technology |
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Principal Investigator |
TOYODA Kazuhiro 九州工業大学, 大学院・工学研究院, 准教授 (10361411)
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| Project Period (FY) |
2010 – 2011
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| Project Status |
Completed (Fiscal Year 2011)
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| Budget Amount *help |
¥3,410,000 (Direct Cost: ¥3,200,000、Indirect Cost: ¥210,000)
Fiscal Year 2011: ¥910,000 (Direct Cost: ¥700,000、Indirect Cost: ¥210,000)
Fiscal Year 2010: ¥2,500,000 (Direct Cost: ¥2,500,000)
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| Keywords | 航空宇宙環境 / スペースデブリ / プラズマ / 除去技術 |
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| Research Abstract |
The space debris mitigation method was developed using the interaction between space plasma and biased mesh electrode. The pseudo-debris was charged and attracted by electric field from mesh electrode by means of applying voltage on mesh electrode in a vacuum chamber filled with plasma. The electric force measured with pendulum angle was agreed with theoretical one.
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Report
(3 results)
Research Products
(4 results)
