Experimental Study of a Laser Micro-Thruster for Precise Attitude Control of Spacecraft
Project/Area Number |
22656196
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Research Category |
Grant-in-Aid for Challenging Exploratory Research
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Allocation Type | Single-year Grants |
Research Field |
Aerospace engineering
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Research Institution | Japan Aerospace Exploration Agency |
Principal Investigator |
FUNAKI Ikkoh 独立行政法人宇宙航空研究開発機構, 宇宙科学研究所, 准教授 (50311171)
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Co-Investigator(Kenkyū-buntansha) |
HORISAWA Hideyuki 東海大学, 工学部, 教授 (30256169)
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Research Collaborator |
SUMIDA Sota 東海大学, 大学院・工学研究科, 大学院生
HAGIWARA Keiji 東海大学, 大学院・工学研究科, 大学院生
YONAMINE Hitoshi 東海大学, 大学院・工学研究科, 大学院生
OSHIO Yuya 総合研究大学院大学, 大学院生
SATO Hiroki 総合研究大学院大学, 大学院生
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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 |
¥3,470,000 (Direct Cost: ¥3,200,000、Indirect Cost: ¥270,000)
Fiscal Year 2011: ¥1,170,000 (Direct Cost: ¥900,000、Indirect Cost: ¥270,000)
Fiscal Year 2010: ¥2,300,000 (Direct Cost: ¥2,300,000)
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Keywords | 航空宇宙工学 / 推進・エンジン / レーザー / マイクロスラスタ |
Research Abstract |
A laser micro-thruster was experimental investigated in a vacuum chamber. In the experiment, 1-20 W continuous wave laser was irradiated on the thruster, consisting of an aluminum target, and thrust force proportional to the laser input power(0.3~0.8μN/W) was obtained. Because the thrust force depends on the pressure in the vacuum chamber, it is expected that a rarefied jet is formed around the aluminum target as a result of laser irradiation.
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Report
(3 results)
Research Products
(16 results)
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[Presentation] 微小推力測定システムの開発2011
Author(s)
萩原啓司,與那嶺仁,大塩祐哉,佐藤博紀,堀澤秀之,船木一幸
Organizer
日本航空宇宙学会第42期年会講演会
Place of Presentation
東京
Year and Date
2011-04-14
Related Report
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[Presentation] Experimental Investigation on CW Laser Microthruster2011
Author(s)
Yonamine, H., Hagiwara, K., Horisawa, H., Oshio, Y., Satou, H., Funaki, I.
Organizer
32nd International Electric Propulsion Conference, IEPC-2011-320
Place of Presentation
ヴィースバーデン(ドイツ)
Related Report
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