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月軌道から帰還する超小型プローブの熱防御システム
https://jaxa.repo.nii.ac.jp/records/3691
https://jaxa.repo.nii.ac.jp/records/3691a96ee208-c8a7-448c-892b-cafbf24aabb0
名前 / ファイル | ライセンス | アクション |
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AA1630004036.pdf (554.8 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2016-05-02 | |||||
タイトル | ||||||
タイトル | 月軌道から帰還する超小型プローブの熱防御システム | |||||
言語 | ||||||
言語 | jpn | |||||
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 | |||||
その他のタイトル(英) | ||||||
その他のタイトル | A Heat Shield System of a Nano-Sized Space Probe Returning from a Lunar Orbit | |||||
著者 |
吉尾, 颯
× 吉尾, 颯× 奥山, 圭一× 下田, 孝幸× Szasz, Bianca× 加藤, 純郎× Yoshio, Hayato× Okuyama, Keiichi× Shimoda, Kazuyuki× Szasz, Bianca× Kato, Sumio |
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著者所属 | ||||||
九州工業大学 | ||||||
著者所属 | ||||||
九州工業大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
琉球大学 | ||||||
著者所属 | ||||||
琉球大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
University of the Ryukyus | ||||||
著者所属(英) | ||||||
en | ||||||
University of the Ryukyus | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料: 第12回宇宙環境シンポジウム講演論文集 en : JAXA Special Publication: Proceedings of the 12th Spacecraft Environment Symposium 巻 JAXA-SP-15-012, p. 347-349, 発行日 2016-03-11 |
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会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 第12回 宇宙環境シンポジウム(2015年11月16日-18日. 北九州国際会議場 国際会議室), 北九州市, 福岡県 | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The 12th Spacecraft Environment Symposium (November 16-18, 2015. International Conference Room, Kitakyushu International Conference Center), Kitakyushu, Fukuoka, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The LATS (Lightweight Ablator series for Transfer vehicle) is a porous CFRP composite material and it can endure from heat flux bunch of approximately 15 MW/sq m, m2. After a Nano probe finish collecting samples of lunar, they make a reentry into the earth's atmosphere with the speed of 11 km/s without slowdown. This report shows a heat shield system using this LATS. Specifically, this report shows about the heat shield constitution and a necessary thickness, an in-depth temperature history during a re-entry flight. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA1630004036 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-15-012 |