WEKO3
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火星着陸探査に向けた大気突入モジュールのエアロシェル開発
https://jaxa.repo.nii.ac.jp/records/3654
https://jaxa.repo.nii.ac.jp/records/3654baae4e24-f74c-43b1-bab1-9400278fb94d
名前 / ファイル | ライセンス | アクション |
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AA1630005029.pdf (3.7 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2016-04-21 | |||||
タイトル | ||||||
タイトル | 火星着陸探査に向けた大気突入モジュールのエアロシェル開発 | |||||
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 | Development of Aeroshell Module for Mars Exploration Mission | |||||
著者 |
鈴木, 俊之
× 鈴木, 俊之× 滝沢, 直美× 青木, 卓哉× 石田, 雄一× 小笠原, 俊男× 渡邉, 泰秀× 藤田, 和央× Suzuki, Toshiyuki× Takizawa, Naomi× Aoki, Takuya× Ishida, Yuichi× Ogasawara, Toshio× Watanabe, Yasuhide× Fujita, Kazuhisa |
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著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
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47回流体力学講演会/第33回航空宇宙数値シミュレーション技術シンポジウム論文集 en : JAXA Special Publication: Proceedings of the 47th Fluid Dynamics Conference / the 33rd Aerospace Numerical Simulation Symposium 巻 JAXA-SP-15-013, p. 183-188, 発行日 2016-03-08 |
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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47回流体力学講演会/第33回航空宇宙数値シミュレーション技術シンポジウム (2015年7月2日-3日. 東京大学生産技術研究所), 目黒区, 東京 | |||||
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 | 47th Fluid Dynamics Conference /the 33rd Aerospace Numerical Simulation Symposium (July 2-3, 2015. Institute of Industrial Science , the University of Tokyo), Meguro-ku, Tokyo, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Lightweight ablative material has been developed in Japan Aerospace Exploration Agency for Mars rover mission in Japan. Basic thermal characteristics of ablating material are obtained by conducting heating tests in high enthalpy facilities. Thermal conductivity measurements and thermogravimetry analysis are made to develop a numerical analysis code to predict the thermal performance of ablator in flight environments. Tensile strength tests are carried out to examine the mechanical performance of ablator. Effects of Martin dust storm on the surface erosion of ablator are also investigated experimentally. Finally, a breadboard model of the lightweight ablator aeroshell with the diameter of 500mm is developed to examine a manufacturability of proto flight model of aeroshell. The developed BBM is qualified through vibration tests, pyro shock tests, and thermal-vacuum tests at the qualification test level of the mission requirements. | |||||
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: AA1630005029 | |||||
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-15-013 |