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Finite Element Analysis of Vibration Amplification Distribution in Lean Satellites
http://hdl.handle.net/10228/00007238
http://hdl.handle.net/10228/0000723863cf5ac3-e724-4251-a63c-06853091baa6
名前 / ファイル | ライセンス | アクション |
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LaSEINE-2016_08.pdf (1.5 MB)
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Item type | 会議発表論文 = Conference Paper(1) | |||||||||||||||||
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公開日 | 2019-06-24 | |||||||||||||||||
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 | |||||||||||||||||
タイトル | ||||||||||||||||||
言語 | en | |||||||||||||||||
タイトル | Finite Element Analysis of Vibration Amplification Distribution in Lean Satellites | |||||||||||||||||
言語 | ||||||||||||||||||
言語 | eng | |||||||||||||||||
著者 |
Batsuren, Amgalanbat
× Batsuren, Amgalanbat× Hatamura, Toru× 増井, 博一
WEKO
17583
× 趙, 孟佑
WEKO
754
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抄録 | ||||||||||||||||||
内容記述タイプ | Abstract | |||||||||||||||||
内容記述 | This paper presents a part of the basic research for establishing the unit Qualification Test (QT) conditions within the framework of an international project to make ISO standard, namely, "Space Systems—Design Qualification and Acceptance Tests for Small-Scale Satellites and Units Requiring Low Costs and Fast Delivery". A laboratory test is conducted to study how vibration acceleration is distributed in a satellite body, so as to define the unit QT random vibration test level. The range of natural frequency and the amplification of acceleration are identified through statistical analysis of the test results. Finite element analysis is carried out to extend the findings to other structural types of micro/nanosatellites. Three structural types are analyzed, i.e., Yojo han, T-type and Pi-type. Based on the results, a unit QT vibration level that provides the minimum reliability assurance for use in space is proposed. | |||||||||||||||||
言語 | en | |||||||||||||||||
備考 | ||||||||||||||||||
内容記述タイプ | Other | |||||||||||||||||
内容記述 | 6th Nano-satellite Symposium (NSAT), July 4th-July 10th, 2015, Kobe-Hyogo, Japan | |||||||||||||||||
書誌情報 |
en : Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan 巻 14, 号 ists30, p. Pf_51-Pf_60, 発行日 2015-07-10 |
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言語 | ja | |||||||||||||||||
出版社 | 日本航空宇宙学会 | |||||||||||||||||
DOI | ||||||||||||||||||
関連タイプ | isIdenticalTo | |||||||||||||||||
識別子タイプ | DOI | |||||||||||||||||
関連識別子 | https://doi.org/10.2322/tastj.14.Pf_51 | |||||||||||||||||
CRID | ||||||||||||||||||
関連タイプ | isIdenticalTo | |||||||||||||||||
識別子タイプ | URI | |||||||||||||||||
関連識別子 | https://cir.nii.ac.jp/crid/1390282680296025472 | |||||||||||||||||
ISSN | ||||||||||||||||||
収録物識別子タイプ | EISSN | |||||||||||||||||
収録物識別子 | 1884-0485 | |||||||||||||||||
著作権関連情報 | ||||||||||||||||||
権利情報 | Copyright (c) 2016 by the Japan Society for Aeronautical and Space Sciences and ISTS. | |||||||||||||||||
キーワード | ||||||||||||||||||
主題Scheme | Other | |||||||||||||||||
主題 | Finite Element Analysis | |||||||||||||||||
キーワード | ||||||||||||||||||
主題Scheme | Other | |||||||||||||||||
主題 | Small Satellites | |||||||||||||||||
キーワード | ||||||||||||||||||
主題Scheme | Other | |||||||||||||||||
主題 | Random Vibration Test | |||||||||||||||||
キーワード | ||||||||||||||||||
主題Scheme | Other | |||||||||||||||||
主題 | International Standards | |||||||||||||||||
出版タイプ | ||||||||||||||||||
出版タイプ | VoR | |||||||||||||||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||||||||||||||
査読の有無 | ||||||||||||||||||
値 | yes | |||||||||||||||||
連携ID | ||||||||||||||||||
7711 |