| Project/Area Number |
13555267
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| Research Category |
Grant-in-Aid for Scientific Research (B)
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| Allocation Type | Single-year Grants |
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| Section | 展開研究 |
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| Research Field |
Aerospace engineering
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| Research Institution | Kyushu University |
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Principal Investigator |
TAKAHASHI Koji Kyushu University, Faculty of Engineering, Associate Professor, 大学院・工学研究院, 助教授 (10243924)
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| Co-Investigator(Kenkyū-buntansha) |
ASANO Tanemasa Kyushu Inst.Tech., Center for Micro Systems, Professor, マイクロ化総合技術センター, 教授 (50126306)
YASAKA Tetsuo Kyushu University, Faculty of Engineering, Professor, 大学院・工学研究院, 教授 (80261238)
NAGAYAMA Kunihito Kyushu University, Faculty of Engineering, Professor, 大学院・工学研究院, 教授 (20040446)
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| Project Period (FY) |
2001 – 2003
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| Project Status |
Completed (Fiscal Year 2003)
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| Budget Amount *help |
¥13,800,000 (Direct Cost: ¥13,800,000)
Fiscal Year 2003: ¥1,000,000 (Direct Cost: ¥1,000,000)
Fiscal Year 2002: ¥2,500,000 (Direct Cost: ¥2,500,000)
Fiscal Year 2001: ¥10,300,000 (Direct Cost: ¥10,300,000)
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| Keywords | MEMS / Microchannel / Hydrogen Peroxide / Porous Silicon / Platinum Catalyst / 推力測定 / 気液相変化 / マイクロヒータ / マイクロタンクアレイ / マイクロヒーター |
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| Research Abstract |
In order to control the position and attitude of micro aerospace systems represented by the pico satellite of less than 1kg, liquid-propellent microthrusters are fabricated and tested. At first, two fuel supply systems are developed, one of which is a novel micro tank array and the other is piezoelectric diaphragm pump. All systems are based on MEMS technology especially, considering the microscale fluid and thermal phenomena. Because the size is extremely reduced, the increased surface/volume ratio makes the two-phase flow critically dependent on the wettability. In order to control the bubbly flow, super-hydrophobic surface is successfully obtained by electrochemical etching of silicon substrate. The obtained porous surface is found applicable to catalyst bed. Platinum particle is deposited there and compared its performance with the film configurations. Though the obtained ISP is not so high because of the low concentration of Hydrogen peroxide fuel, it can be concluded that the MEMS fabrication process for high-performance liquid-propellant thruster is achieved in this development study.
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