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アイテム
Solar Module Integrated Converters as Power Generator in Small Spacecrafts: Design and Verification Approach
http://hdl.handle.net/10228/00007358
http://hdl.handle.net/10228/00007358276bf5c3-bfb1-4992-8648-084eff202f1f
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
aerospace-06-00061.pdf (4.2 MB)
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| アイテムタイプ | 学術雑誌論文 = Journal Article(1) | |||||
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| 公開日 | 2019-08-30 | |||||
| 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 | |||||
| タイトル | ||||||
| タイトル | Solar Module Integrated Converters as Power Generator in Small Spacecrafts: Design and Verification Approach | |||||
| 言語 | en | |||||
| 言語 | ||||||
| 言語 | eng | |||||
| 著者 |
Gonzalez-Llorente, Jesus
× Gonzalez-Llorente, Jesus× Lidtke, Aleksander A.× Hatanaka, Ken× Kawauchi, Ryo× Okuyama, Kei-Ichi |
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| 抄録 | ||||||
| 内容記述タイプ | Abstract | |||||
| 内容記述 | As small satellites are becoming more widespread for new businesses and applications, the development time, failure rate and cost of the spacecraft must be reduced. One of the systems with the highest cost and the most frequent failure in the satellite is the Electrical Power System (EPS). One approach to achieve rapid development times while reducing the cost and failure rate is using scalable modules. We propose a solar module integrated converter (SMIC) and its verification process as a key component for power generation in EPS. SMIC integrates the solar array, its regulators and the telemetry acquisition unit. This paper details the design and verification process of the SMIC and presents the in-orbit results of 12 SMICs used in Ten-Koh satellite, which was developed in less than 1.5 years. The in-orbit data received since the launch reveal that solar module withstands not only the launching environment of H-IIA rocket but also more than 1500 orbits in LEO. The modular approach allowed the design, implementation and qualification of only one module, followed by manufacturing and integration of 12 subsequent flight units. The approach with the solar module can be followed in other components of the EPS such as battery and power regulators. | |||||
| 言語 | en | |||||
| 書誌情報 |
en : Aerospace 巻 6, 号 5, p. 61, 発行日 2019-05-27 |
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| 出版社 | ||||||
| 出版者 | MDPI | |||||
| DOI | ||||||
| 関連タイプ | isIdenticalTo | |||||
| 識別子タイプ | DOI | |||||
| 関連識別子 | https://doi.org/10.3390/aerospace6050061 | |||||
| ISSN | ||||||
| 収録物識別子タイプ | EISSN | |||||
| 収録物識別子 | 2226-4310 | |||||
| 著作権関連情報 | ||||||
| 権利情報Resource | http://creativecommons.org/licenses/by/4.0/ | |||||
| 権利情報 | Copyright (c) 2019 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (http://creativecommons.org/licenses/by/4.0/). | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | small satellite | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | electrical power system | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | modular design | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | spacecraft testing | |||||
| 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 | ||||||
| 値 | 7856 | |||||
