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Preliminary structural design and key technology demonstration of cryogenic assembly in the next-generation infrared space telescope SPICA
https://jaxa.repo.nii.ac.jp/records/22538
https://jaxa.repo.nii.ac.jp/records/22538b09f69a2-1172-4d4c-93bf-4be12c3924e1
Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2015-08-24 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Preliminary structural design and key technology demonstration of cryogenic assembly in the next-generation infrared space telescope SPICA | |||||
言語 | ||||||
言語 | eng | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | journal article | |||||
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 | |||||
著者 |
水谷, 忠均
× 水谷, 忠均× 山脇, 敏彦× 小松, 敬治× 後藤, 健× 竹内, 伸介× 篠崎, 慶亮× 松原, 英雄× 中川, 貴雄× Mizutani, Tadahito× Yamawaki, Toshihiko× Komatsu, Keiji× Goto, Ken× Takeuchi, Shinsuke× Shinozaki, Keisuke× Matsuhara, Hideo× Nakagawa, Takao |
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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) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
出版者 | ||||||
出版者 | 国際光工学会(SPIE) | |||||
出版者(英) | ||||||
出版者 | The International Society for Optical Engineering(SPIE) | |||||
書誌情報 |
en : Journal of Astronomical Telescopes, Instruments, and Systems 巻 1, 号 2, 発行日 2015-04-15 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The infrared space telescope SPICA (Space Infrared Telescope for Cosmology and Astrophysics) is a next-generation astronomical project of the Japan Aerospace Exploration Agency, which features a 3 m class and 6 K cryogenically cooled space telescope. This paper outlines the current status for the preliminary structural design of the SPICA payload module. Dedicated studies were conducted for key technologies to enhance the design accuracy of the SPICA cryogenic assembly and mitigate the development risk. One of the results is described for the concept of the on-orbit truss separation mechanisms, which aim to both reduce the heat load from the main truss assembly and isolate the microvibration by changing the natural frequency of the spacecraft. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 2329-4124 | |||||
DOI | ||||||
識別子タイプ | DOI | |||||
関連識別子 | http://dx.doi.org/10.1117/1.JATIS.1.2.027001 | |||||
関連名称 | info:doi/10.1117/1.JATIS.1.2.027001 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: PA1510037000 |