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アイテム
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パラフィン駆動式ヒートスイッチの熱伝導性能評価
https://jaxa.repo.nii.ac.jp/records/38684
https://jaxa.repo.nii.ac.jp/records/38684226f14bb-c5f2-48a3-87c3-5830b1bf2ffa
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-10-16 | |||||
タイトル | ||||||
タイトル | パラフィン駆動式ヒートスイッチの熱伝導性能評価 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Heat switch | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Paraffin | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Gold coating | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Evaluation of Thermal Performance of Paraffin-actuated Heat Switch | |||||
著者 |
安藤, 麻紀子
× 安藤, 麻紀子× 篠崎, 慶亮× 岡本, 篤× 杉田, 寛之× Ando, Makiko× Shinozaki, Keisuke× Okamoto, Atsushi× Sugita, Hiroyuki |
|||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
出版者 | ||||||
出版者 | 日本航空宇宙学会(JSASS) | |||||
出版者(英) | ||||||
出版者 | The Japan Society for Aeronautical and Space Sciences (JSASS) | |||||
書誌情報 |
第58回宇宙科学技術連合講演会講演集 en : Proceedings of 58th Space Sciences and Technology Conference 発行日 2014-11 |
|||||
会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 第58回宇宙科学技術連合講演会(2014年11月12日-14日. 長崎ブリックホール), 長崎市, 長崎県 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A heat switch provides appropriate thermal switching (high or low thermal conductance) depending on the thermal environment around spacecraft. It has an advantage in terms of thermal control of spacecraft such as a lunar rover and planetary exploration spacecraft which have difficulty securing sufficient heater power to keep the spacecraft within its allowable temperature range. The authors have developed a paraffin-actuated heat switch. The required thermal performance is 1W/K as ON thermal conductance and 100 as ON/OFF thermal conductance ratio. The bread board model was fabricated and its performance was evaluated. Consequently, BBM achieved 1.6W/K as ON thermal conductance and 123 as ON/OFF ratio. The long-term thermal performance was also evaluated, and the results showed the consistent thermal performance for one month. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AC1500044000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JSASS-2014-4408 |