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赤外線天文衛星「SPICA」ペイロードモジュールの構造検討
https://jaxa.repo.nii.ac.jp/records/38797
https://jaxa.repo.nii.ac.jp/records/3879789a835f1-2be7-4777-9589-c9f12b8710f4
Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2016-09-21 | |||||
タイトル | ||||||
タイトル | 赤外線天文衛星「SPICA」ペイロードモジュールの構造検討 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Infrared Telescope | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Structural Design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | analysis | |||||
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 | SPICA Payload Module Structure Consideration | |||||
著者 |
間澤, 朋哉
× 間澤, 朋哉× 東海林, 和典× 岡田, 康彦× 飯田, 浩× 中川, 貴雄× 小川, 博之× 後藤, 健× 竹内, 伸介× 山脇, 敏彦× 水谷, 忠均× 松原, 英雄× Mazawa, Tomoya× Shoji, Kazunori× Okada× Iida, Hiroshi× Nakagawa, Takao× Ogawa, Hiroyuki× Goto, Ken× Takeuchi, Shinsuke× Yamawaki, Toshihiko× Mizutani, Tadahito× Matsuhara, Hideo |
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著者所属 | ||||||
日本電気株式会社 | ||||||
著者所属 | ||||||
日本電気株式会社 | ||||||
著者所属 | ||||||
日本電気株式会社 | ||||||
著者所属 | ||||||
日本電気株式会社 | ||||||
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 | ||||||
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 | ||||||
NEC Corporation | ||||||
著者所属(英) | ||||||
en | ||||||
NEC Corporation | ||||||
著者所属(英) | ||||||
en | ||||||
NEC Corporation | ||||||
著者所属(英) | ||||||
en | ||||||
NEC Corporation | ||||||
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) | ||||||
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 | Japan Society for Aeronautical and Space Sciences (JSASS) | |||||
書誌情報 |
第47期年会講演会講演集 en : Proceedings of the 47th JSASS Annual Meeting 巻 47, 発行日 2016-04-14 |
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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47期定時社員総会および年会講演会(2016年4月14日-15日. 東京大学 山上会館 ), 文京区, 東京 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | SPICA is the next-generation infrared space telescope cooled to very low temperature on orbit to achieve extremely high sensitivity for astronomical observations in the infrared. The scientific instrument assembly is supported by the structure of the payload module using an on-orbit thermal insulation mechanism. The structure of payload module consists of CFRP, which is chosen from the requirement of thermal design. It is confirmed that the payload module has enough stiffness by structure analysis. | |||||
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 | Physical characteristics: Original contains color illustrations | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA12394237 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AC1600066000 | |||||
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-2016-1089 |