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An Analytical Approach to the Thermal Design of Spacecrafts
https://jaxa.repo.nii.ac.jp/records/34400
https://jaxa.repo.nii.ac.jp/records/34400dc10cfe7-a690-40c6-862f-5f60b50fbf60
名前 / ファイル | ライセンス | アクション |
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SA2400575.pdf (2.2 MB)
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Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | An Analytical Approach to the Thermal Design of Spacecrafts | |||||
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 | departmental bulletin paper | |||||
著者 |
OSHIMA, Koichi
× OSHIMA, Koichi× OSHIMA, Yuko |
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出版者 | ||||||
出版者 | 東京大学宇宙航空研究所 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Aeronautical Science,University of Tokyo | |||||
書誌情報 |
en : ISAS report/Institute of Space and Aeronautical Science,University of Tokyo 巻 33, 号 1, p. 1-39, 発行日 1968-01 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The linearized thermal balance equations of two-nodes system, in which radiative heat dissipation to outer space from the each node and heat transfer between them are counted, are analytically solved for several special cases which closely relate to the real situations in spacecrafts. And general theorems on n-nodes system are presented with relations to the real spacecraft structure. Based on these discussions, a new method of thermal analysis of spacecrafts is proposed, which is essentially an experimental analysis of simplified thermal model. The construction method of this model and the data reduction process are shown with an illustrative example. Using this method, the thermal character of a spacecraft can be determined with minimum simulator time and without longsome numerical computation. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0372-1418 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA00675986 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: SA2400575000 |