Microfabrication of mega-pixcel micro-plasmajets and their potentials for medical applications
Project/Area Number |
15K14256
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Research Category |
Grant-in-Aid for Challenging Exploratory Research
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Allocation Type | Multi-year Fund |
Research Field |
Aerospace engineering
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Research Institution | Tokai University |
Principal Investigator |
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Co-Investigator(Kenkyū-buntansha) |
山口 滋 東海大学, 理学部, 教授 (40297205)
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Project Period (FY) |
2015-04-01 – 2018-03-31
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Project Status |
Completed (Fiscal Year 2017)
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Budget Amount *help |
¥3,900,000 (Direct Cost: ¥3,000,000、Indirect Cost: ¥900,000)
Fiscal Year 2017: ¥910,000 (Direct Cost: ¥700,000、Indirect Cost: ¥210,000)
Fiscal Year 2016: ¥1,300,000 (Direct Cost: ¥1,000,000、Indirect Cost: ¥300,000)
Fiscal Year 2015: ¥1,690,000 (Direct Cost: ¥1,300,000、Indirect Cost: ¥390,000)
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Keywords | 推進・エンジン / 電気推進 / 微細加工 / 表面加工 / マイクロマルチプラズマジェットアレイ,プラズマ源 / マルチ噴流効果 / プラズマ除去加工 / マイクロマルチプラズマジェットアレイ / プラズマ源 / プラズマ推進機 / プラズマ除去加工機 / プラズマ生体薄膜除去 |
Outline of Final Research Achievements |
The objective of this study is to investigate primary subjects for development and improvement of thin, small or large DC plasmajet-array. Firstly, micro-fabrication and demonstration of micro-plasmajet-array were conducted. It was shown that multi-nozzle configuration of thin nozzle elements was appropriate for large thrusters rather than small thrusters, and that thrust performance was higher than single nozzles with the same sizes. Secondly, development of a novel laser-thermal micro-plasmajet employing a laser-diode coupled fiber-tip heat source was conducted for a potential candidate of innovative micro-nozzle elements. In addition, to employ and enhance chemical energy required for low-power plasma sources, development of novel, safe, non-toxic liquid propellant was conducted. Some potential liquids were extracted.
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Report
(4 results)
Research Products
(38 results)
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[Journal Article] Chemically Augmented Laser Microthrusters2017
Author(s)
Mitsutoshi Tsuchiya, Shoko Shaibagaki, Kai Wada, Souto Komine, Miya Isoda, Yuka Arai, Tomoyuki Ikeda, Hideyuki Horisawa
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Journal Title
Proceedings of the 35th International Electric Propulsion Conference
Volume: IEPC2017-408
Pages: 1-6
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[Presentation] Chemically Augmented Arcjet Thrusters2017
Author(s)
Yuka Arai, Shoko Shaibagaki, Kai Wada, Mitsutoshi Tsuchiya, Tomoyuki Ikeda, Hideyuki Horisawa
Organizer
Joint Conference: 31st ISTS (International Symposium on Space Technology and Science), 26th ISSFD (International Symposium on Space Flight Dynamics) & 8th NSAT (Nano-Satellite Symposium)
Related Report
Int'l Joint Research
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[Presentation] Chemically Augmented Laser-thermal Thrusters2017
Author(s)
Mitsutoshi Tsuchiya, Yuka Arai, Kai Wada, Miya Isoda, Shoko Shibagaki, Tomoyuki Ikeda, Hideyuki Horisawa
Organizer
Joint Conference: 31st ISTS (International Symposium on Space Technology and Science), 26th ISSFD (International Symposium on Space Flight Dynamics) & 8th NSAT (Nano-Satellite Symposium)
Related Report
Int'l Joint Research
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[Presentation] Development of Chemically Augmented Electrothermal Thrusters2017
Author(s)
Shoko Shibagaki, Kai Wada, Mitsutoshi Tsuchiya, Yuka Arai, Tomoyuki Ikeda, Hideyuki Horisawa
Organizer
Joint Conference: 31st ISTS (International Symposium on Space Technology and Science), 26th ISSFD (International Symposium on Space Flight Dynamics) & 8th NSAT (Nano-Satellite Symposium)
Related Report
Int'l Joint Research
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[Presentation] High-Temperature Generation of a Diode-Laser Coupled Fiber-Tip Heat Source2015
Author(s)
Kai Wada, Shoko Shibagaki, Yoshiki Fukuda, Keisuke Kondo, Hideyuki Horisawa
Organizer
Joint Conference of 30th ISTS(International Symposium on Space Technology and Science), 34th IEPC(International Electric Propulsion Conference) & 6th NSAT(Nano-satellite Symposium)
Place of Presentation
Kobe International Conference Center (兵庫県・神戸市)
Year and Date
2015-07-04
Related Report
Int'l Joint Research