WEKO3
アイテム
Ground Tests and In-Orbit Results for the Horyu-II Nanosatellite Power System
http://hdl.handle.net/10228/00007259
http://hdl.handle.net/10228/00007259603a9f25-c7b7-4f93-9a0e-ccd4f521cccd
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
LaSEINE-2013_18.pdf (4.7 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 | 2019-06-28 | |||||||||||
| 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 | Ground Tests and In-Orbit Results for the Horyu-II Nanosatellite Power System | |||||||||||
| 言語 | en | |||||||||||
| その他のタイトル | ||||||||||||
| その他のタイトル | Ground tests and on-orbit results of the power system of nano-satellite Horyu-II | |||||||||||
| 言語 | en | |||||||||||
| 言語 | ||||||||||||
| 言語 | eng | |||||||||||
| 著者 |
Okada, Kazuya
× Okada, Kazuya× Seri, Yuki× Shibagaki, Ryunosuke× Kyutech Satellite Project× 増井, 博一
WEKO
17583
× 趙, 孟佑 |
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| 抄録 | ||||||||||||
| 内容記述タイプ | Abstract | |||||||||||
| 内容記述 | The Kyutech (Kyushu Institute of Technology) Satellite Project developed a high-voltage demonstration satellite called “Horyu-II” between 2010 and 2012. Horyu-II is a nanosatellite 350 mm x 310 mm x 315 mm (X*Y*Z) in size, with a mass of only 7.1 kg. This satellite was launched on May 18, 2012 as a piggy-back payload of the 21st H-IIA launch. Its missions are the demonstration of high-voltage technology in orbit, mitigation of electrostatic discharge (ESD), and so on. In this paper, we describe the design of the power system and its verification through various ground tests. The power system is equipped with a thin-film double-junction GaAs solar cell, with an efficiency of 20%, as the primary power source for the first time in orbit. The satellite also carries Ni-MH batteries for power storage. The power system architecture was simplified as much as possible with failure prevention mechanisms, such as over-current protection and various switches related to safety and debris mitigation. We present the analysis of the telemetry data obtained after the launch and validate the effectiveness of the design and verification processes. | |||||||||||
| 言語 | en | |||||||||||
| 備考 | ||||||||||||
| 内容記述タイプ | Other | |||||||||||
| 内容記述 | 29th International Symposium on Space Technology and Science (ISTS), June 2nd-June 9th, 2013, Nagoya-Aichi, Japan | |||||||||||
| 書誌情報 |
en : Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan 巻 12, 号 ists29, p. Tf_49-Tf_56, 発行日 2013-06 |
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| 出版社 | ||||||||||||
| 出版者 | 日本航空宇宙学会 | |||||||||||
| 言語 | ja | |||||||||||
| 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.12.Tf_49 | |||||||||||
| 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/1390282680295897344 | |||||||||||
| 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) 2014 by the Japan Society for Aeronautical and Space Sciences and ISTS. | |||||||||||
| キーワード | ||||||||||||
| 主題Scheme | Other | |||||||||||
| 主題 | Nanosatellite | |||||||||||
| キーワード | ||||||||||||
| 主題Scheme | Other | |||||||||||
| 主題 | Power System | |||||||||||
| キーワード | ||||||||||||
| 主題Scheme | Other | |||||||||||
| 主題 | In-Orbit Results | |||||||||||
| 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 | 7692 | |||||||||||
