WEKO3
アイテム
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異なる温度環境条件下における絶縁体宇宙材料の二次電子放出係数および抵抗値の測定
https://jaxa.repo.nii.ac.jp/records/3801
https://jaxa.repo.nii.ac.jp/records/3801f2257165-d63a-4483-a2bb-6afe8d1919ae
名前 / ファイル | ライセンス | アクション |
---|---|---|
AA1530019016.pdf (1.2 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-05-08 | |||||
タイトル | ||||||
タイトル | 異なる温度環境条件下における絶縁体宇宙材料の二次電子放出係数および抵抗値の測定 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Total Electron Emission Yield | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Insulator | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Charging | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Temperature | |||||
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 | Total Electron Emission Yield and Resistance Measurement of Polyimide Film Due to Different Temperatures | |||||
著者 |
宮原, 信
× 宮原, 信× 川﨑, 和貴× Wu, Jiang× Khan, Arifur Rahman× 豊田, 和弘× 趙, 孟佑× Miyahara, Akira× Kawasaki, Kazutaka× Wu, Jiang× Khan, Arifur Rahman× Toyoda, Kazuhiro× Cho, Mengu |
|||||
著者所属 | ||||||
九州工業大学 | ||||||
著者所属 | ||||||
九州工業大学 | ||||||
著者所属 | ||||||
西安交通大学 | ||||||
著者所属 | ||||||
九州工業大学 | ||||||
著者所属 | ||||||
九州工業大学 | ||||||
著者所属 | ||||||
九州工業大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Xi'an Jiaotong University | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料: 第11回宇宙環境シンポジウム講演論文集 en : JAXA Special Publication: Proceedings of the 11th Spacecraft Environment Symposium 巻 JAXA-SP-14-012, p. 113-119, 発行日 2015-03-20 |
|||||
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11回宇宙環境シンポジウム (2014年12月10日-11日. 大阪府立大学 I-siteなんば), 大阪 | |||||
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 | 11th Spacecraft Environment Symposium (December 10-11, 2014, I-site Namba, Osaka Prefecture University), Osaka, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Electron induced secondary electron emission from space insulator is a very important factor in understanding spacecraft charging behavior. Due to the injection of primary electrons and the emission of secondary electrons in the surface layer of insulator, the target surface will be negatively or positively charged. Additionally, the electron emission yield of the spacecraft surface materials is highly dependent on space environments, such as the temperature variation. In our tests, we chose the polyimide film (Kapton 100H) and the cover glass (CMG) the research object, and used a single short, low-density pulsed beam, and also developed a scanning method for the total electron emission yield (TEEY) measurement, which can avoid surface potential influence for insulating materials. Moreover for the TEEY system, we installed a heater for high temperature (around 100 C) and the shroud by using liquid nitrogen for low temperature (around -50 C). Under this experimental situation, TEEY of polyimide films of room, high and low temperature was tested respectively. The conductivity variation of the polyimide film and the cover glass due to the different temperatures was considered to influence TEEY. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 著者名の誤記: Cho, Mungu | |||||
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 | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The clerical error of an author's name: Cho, Mungu | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA1530019016 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-14-012 |