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アイテム
Analysis of Charging of the HTV-4 Based on On-Orbit Data
http://hdl.handle.net/10228/00007897
http://hdl.handle.net/10228/0000789707c5da32-bf50-409d-a5ad-d180bd9f9773
| 名前 / ファイル | ライセンス | アクション |
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LaSEINE-2019_05.pdf (1.3 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 | 2020-09-23 | |||||
| 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 | Analysis of Charging of the HTV-4 Based on On-Orbit Data | |||||
| 言語 | en | |||||
| 言語 | ||||||
| 言語 | eng | |||||
| 著者 |
Tsujita, Daisuke
× Tsujita, Daisuke× Okumura, Teppei× Kobayashi, Yuki× Kasai, Toru× Ohkawa, Yasushi× Koga, Kiyokazu× 趙, 孟佑 |
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| 抄録 | ||||||
| 内容記述タイプ | Abstract | |||||
| 内容記述 | After three H-II transfer vehicles (HTVs) had finished their mission to resupply the International Space Station (ISS), NASA requested data of the HTV's potential to evaluate the charging/discharging process that occurs when the HTV docks to the ISS. To measure these data, a new instrument was installed on the fourth HTV. This instrument allows us to measure the HTV-4 surface potential relative to the surrounding plasma, and is called advanced technology on-orbit test instrument for space environment-mini (ATOTIE-mini). The ATOTIE-mini observed the HTV's local potential in the orbit for more than one month. The measured potential during the HTV solo-flight phase varied between -30 and -60 V in sunlight and was about 0 V in eclipse conditions. The HTV's potential during the time when it was docked to the ISS followed the ISS's potential with an almost constant offset of about 10 V. The data measured by ATOTIE-mini are consistent with those measured by the floating potential measurement unit on the ISS, and thus are considered reliable. The HTV's potential level itself was acceptable for ISS. Note that the solar array panels can generate up to approximately 120 V, which is much larger than the absolute potential range in sunshine. We analyze the potential distribution on the HTV surface by a multi-utility spacecraft charging analysis tool, because ATOTIE-mini can only observe one point on the HTV surface. The analysis results are discussed with respect to the flight attitude. | |||||
| 言語 | en | |||||
| 書誌情報 |
en : IEEE Transactions on Plasma Science 巻 47, 号 8, p. 3905-3914, 発行日 2019-06-19 |
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| 出版社 | ||||||
| 出版者 | IEEE | |||||
| DOI | ||||||
| 関連タイプ | isVersionOf | |||||
| 識別子タイプ | DOI | |||||
| 関連識別子 | https://doi.org/10.1109/TPS.2019.2920153 | |||||
| 日本十進分類法 | ||||||
| 主題Scheme | NDC | |||||
| 主題 | 538 | |||||
| NCID | ||||||
| 収録物識別子タイプ | NCID | |||||
| 収録物識別子 | AA0066803X | |||||
| ISSN | ||||||
| 収録物識別子タイプ | EISSN | |||||
| 収録物識別子 | 1939-9375 | |||||
| ISSN | ||||||
| 収録物識別子タイプ | PISSN | |||||
| 収録物識別子 | 0093-3813 | |||||
| 著作権関連情報 | ||||||
| 権利情報 | Copyright (c) 2019 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works. | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | Charging analysis | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | H-II transfer vehicle (HTV) | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | ionosphere | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | spacecraft charging | |||||
| 出版タイプ | ||||||
| 出版タイプ | AM | |||||
| 出版タイプResource | http://purl.org/coar/version/c_ab4af688f83e57aa | |||||
| 査読の有無 | ||||||
| 値 | yes | |||||
| 連携ID | ||||||
| 値 | 8422 | |||||
