Study on a smart thermal control method under periodic heating environment
| Project/Area Number |
20560741
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| Research Category |
Grant-in-Aid for Scientific Research (C)
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| Allocation Type | Single-year Grants |
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| Section | 一般 |
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| Research Field |
Aerospace engineering
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| Research Institution | Japan Aerospace Exploration Agency |
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Principal Investigator |
OGAWA Hiroyuki Japan Aerospace Exploration Agency, 宇宙科学研究所, 准教授 (60311172)
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| Co-Investigator(Kenkyū-buntansha) |
NAGANO Hosei 名古屋大学, 大学院・工学研究科, 講師 (10435810)
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| Project Period (FY) |
2008 – 2010
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| Project Status |
Completed (Fiscal Year 2010)
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| Budget Amount *help |
¥4,290,000 (Direct Cost: ¥3,300,000、Indirect Cost: ¥990,000)
Fiscal Year 2010: ¥910,000 (Direct Cost: ¥700,000、Indirect Cost: ¥210,000)
Fiscal Year 2009: ¥1,300,000 (Direct Cost: ¥1,000,000、Indirect Cost: ¥300,000)
Fiscal Year 2008: ¥2,080,000 (Direct Cost: ¥1,600,000、Indirect Cost: ¥480,000)
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| Keywords | 宇宙機熱制御 / 宇宙科学 / 環境対応 / 熱工学 / 省エネルギー / 月面長期滞在 / 放熱制御 / 航空宇 / 航空宇宙工学 |
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| Research Abstract |
The purpose of this study is to propose a new thermal control method under periodic heating environment and to demonstrate its feasibility. A new small loop heat pipe was developed as a heat transport device for this method, and thermal controllability against large heat load change and environmental change was evaluated under both atmospheric and vacuum conditions. A new instrument to simulate lunar thermal environment was fabricated. A thermal model for periodic heating environment was also developed based on the evaluation of thermophysical properties of the lunar regolith stimulant.
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Report
(4 results)
Research Products
(17 results)
