WEKO3
アイテム
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宇宙用汎用連続型ADR超低温冷凍システムの開発
https://jaxa.repo.nii.ac.jp/records/13353
https://jaxa.repo.nii.ac.jp/records/13353e2e1221c-4578-4b80-a309-fbc2098a9907
名前 / ファイル | ライセンス | アクション |
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64297109.pdf (2.5 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 宇宙用汎用連続型ADR超低温冷凍システムの開発 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ADR, Cryocooler | |||||
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 | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Development of continuous ADR system for weak gravity missions | |||||
著者 |
沼澤, 健則
× 沼澤, 健則× 神谷, 宏治× 満田, 和久× Numazawa, Takenori× Kamiya, Koji× Shirron, Peter× Mitsuda, Kazuhisa |
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著者所属 | ||||||
物質・材料研究機構 | ||||||
著者所属 | ||||||
物質・材料研究機構 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
National Institute for Materials Science (NIMS) | ||||||
著者所属(英) | ||||||
en | ||||||
National Institute for Materials Science (NIMS) | ||||||
著者所属(英) | ||||||
en | ||||||
Goddard Space Flight Center, National Aeronautics and Space Administration (GSFC/NASA) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (ISAS)(JAXA) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究本部 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙利用シンポジウム en : Space Utilization Research: Proceedings of Space Utilization Symposium 巻 25, 発行日 2009-03 |
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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25回宇宙利用シンポジウム(2009年1月14日-15日, 宇宙航空研究開発機構宇宙科学研究本部相模原キャンパス) | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The Twenty-fifth Space Utilization Symposium (January 14-15, 2009: ISAS/JAXA Sagamihara, Japan) | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Adiabatic Demagnetization Refrigeration (ADR) does not use working fluids contrary to conventional refrigerators that make use of the fluid density difference, which leads to superiority of the ADR under the weak gravity condition. In this study, we developed a continuous ADR system to provide constant cooling temperatures ca. 0.1 K. The system consists of four stages of magnetic materials and magnets cascaded with heat switches. The magnetic materials CPA and GdLiF(sub 4) are used for 3 stages between 0.1 K and 1.4 K, and single stage between 1.4 K and 4 K, respectively. Passive heat switches are used for the stages > 0.3 K and a superconducting heat switch is used for the continuous stage at ca. 0.1 K. A G-M cycle cooler with a 100 V compressor unit is used to cool the ADR and cryostat shieldings. Total mass of flight model is less than 60 kg. Cooling tests with Transition Edge Sensor on the ground showed that the ADR provided continuous cooling temperatures between 105 mK and 120 mK and it successfully operated the TES. Airborne flight experiments confirmed the ability of the cooling system under the mili-gravity condition. The experimental results showed that the ADR could provide stable temperature under the weak gravity, however, strong vibrations coming from turbulence or takeoff affected to the stability of ADR cycle. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10324210 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0064297109 |