WEKO3
アイテム
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Excelを用いた定常温度解析のSLRAへの適用
https://jaxa.repo.nii.ac.jp/records/8039
https://jaxa.repo.nii.ac.jp/records/8039f0b0e76a-3ead-4a8c-a6b4-b5bca185fa4f
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | Excelを用いた定常温度解析のSLRAへの適用 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 計算機プログラム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 計算機プログラミング | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱伝達 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 微分方程式 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ASTRO-G | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 電波天文衛星 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | レーザーリフレクタアレイ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機温度 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 定常状態 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱力学的平衡 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computer program | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computer programming | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | thermal analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | heat transfer | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | differential equation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | thermal design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ASTRO-G | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Radio-Astronomical Satellite | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | laser reflector array | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft temperature | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | steady state | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | thermodynamic equilibrium | |||||
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 | Application of excel static temperature analysis to SLRA | |||||
著者 |
石井, 忠司
× 石井, 忠司× 國森, 裕生× 竹内, 央× 古賀, 茂昭× 洲崎, 保司× Ishii, Tadashi× Kunimori, Hiroo× Takeuchi, Hiroshi× Koga, Shigeaki× Suzaki, Yasuji |
|||||
著者所属 | ||||||
次世代技術 | ||||||
著者所属 | ||||||
情報通信研究機構 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属 | ||||||
翔エンジニアリング | ||||||
著者所属 | ||||||
ユニバース | ||||||
著者所属(英) | ||||||
en | ||||||
Jisedaitech L. P. | ||||||
著者所属(英) | ||||||
en | ||||||
National Institute of Information and Communications Technology (NICT) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Sho Engineering Corp. | ||||||
著者所属(英) | ||||||
en | ||||||
Universe Pty. | ||||||
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/ISAS) | |||||
書誌情報 |
第27回宇宙エネルギーシンポジウム 平成19年度 en : The Twenty-seventh Space Energy Symposium p. 126-130, 発行日 2008-05 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A simplified method to compute static temperature using Microsoft Excel is presented in this report. There are two ways for prediction of temperature. One is transient temperature analysis, and the other is steady state analysis. For the thermal design of spacecrafts, both are important. We ordinarily use the maximum and minimum temperature obtained by the steady-state thermal analysis for the preliminary design. Therefore, although this method cannot treat large models, it is useful for preliminary design level. Because the heat transfer equation is a first-order differential equation, it can be easily solved by using MS (MicroSoft)-Excel. Temperature analysis using Excel are widely performed. But in many cases, they use cells as a meshes of the target's shape. The method that we developed this time simply uses Excel's worksheet as a data of thermal properties, and the calculation is done by Visual Basic for Applications (VBA). The analysis is done by using iterative sequential process and the equilibrium temperature will be calculated. The Excel sheet used for this method has good readability and can be used for a report directly. Because the calculation is coded by VBA, the code is easy to maintain. The calculation is done by VBA interpreter, so it is faster than ordinary Excel process. We applied this method to analyze the temperature of SLRA (Satellite Laser Reflector Array) equipped in ASTRO-G (Radio-Astronomical Satellite), and had a good result that agrees with an analysis using SINDA (System Improved Numerical Differential Analyzer) and detail model. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063965026 |