Study on Liquid Management Technology in Water Tank for Propulsion System Utilizing Aluminum and Water Reaction
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- IMAMURA Takuya
- Course of Aerospace System Engineering, Muroran Institute of Technology
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- SUGIOKA Masatoshi
- space Plane Research Center, Muroran Institute of Technology
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- HIGASHINO Kazuyuki
- space Plane Research Center, Muroran Institute of Technology
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- IMAI Ryoji
- Course of Aerospace System Engineering, Muroran Institute of Technology
書誌事項
- タイトル別名
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- (Improvement of Liquid Acquisition Performance by Hydrophilic Coating in Metallic Tank)
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説明
In order to use hydrogen as a fuel for spacecraft propulsion system, utilization of aluminum and water reaction system is considered. Liquid-gas separation is necessary for water tank in this propulsion system. The purpose of this study is to confirm the applicability of water to the surface tension liquid acquisition mechanism in tank by improving wettability using a silica coating. It was demonstrated that silica coating could improve the wettability of water against metallic material applied to practical tanks. By the microgravity experiment using drop tower facility, it was confirmed that water in tank could be acquired on the liquid outlet by vane device with silica coating.
収録刊行物
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- International Journal of Microgravity Science and Application
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International Journal of Microgravity Science and Application 35 (1), 350103-, 2018-01-31
日本マイクログラビティ応用学会
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詳細情報 詳細情報について
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- CRID
- 1390283659832346624
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- NII論文ID
- 130007771221
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- NII書誌ID
- AN10537663
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- ISSN
- 21889783
- 09153616
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- HANDLE
- 10258/00009659
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- 本文言語コード
- en
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- 資料種別
- journal article
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- データソース種別
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- JaLC
- IRDB
- CiNii Articles
- KAKEN
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- 抄録ライセンスフラグ
- 使用不可