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Proposal and Evaluation of High-Heat Insulation System for Spacecraft by Using WPT

Proposal and Evaluation of High-Heat Insulation System for Spacecraft by Using WPT

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カテゴリ: 論文誌(論文単位)

グループ名: 【D】産業応用部門(英文)

発行日: 2023/05/01

タイトル(英語): Proposal and Evaluation of High-Heat Insulation System for Spacecraft by Using WPT

著者名: Sayuri Honda (Research Unit I, R&D Directorate, Japan Aerospace Exploration Agencym), Shuhei Shimada (Research Unit I, R&D Directorate, Japan Aerospace Exploration Agencym), Kosuke Tanaka (Research Unit II, R&D Directorate, Japan Aerospace Exploration Age

著者名(英語): Sayuri Honda (Research Unit I, R&D Directorate, Japan Aerospace Exploration Agencym), Shuhei Shimada (Research Unit I, R&D Directorate, Japan Aerospace Exploration Agencym), Kosuke Tanaka (Research Unit II, R&D Directorate, Japan Aerospace Exploration Agency), Kana Nakamura (Department of Engineering Mechanics and Energy, Graduate School of Science and Technology Degree Programs in Systems and Information Engineering, University of Tsukuba), Takehiro Imura (Department of Electrical Engineering, Faculty of Science and Technology, Tokyo University of Science), Katsuhiro Hata (Department of Informatics and Electronics, Institute of Industrial Science, University of Tokyo), Yoichi Hori (Department of Electrical Engineering, Faculty of Science and Technology, Tokyo University of Science)

キーワード: heat insulation,lunar surface exploration,MLI,wireless power transfer

要約(英語): As a new space station succeeding the International Space Station (ISS), a lunar orbit manned base, called “Gateway,” is considered and manned lunar surface exploration via the Gateway is also studied. To realize manned lunar surface exploration, new technologies are required to overcome the severe condition of the lunar night. As one of these technologies, applying wireless power transfer (WPT) to a spacecraft, such as a rover, is proposed. The WPT system contributes to the improvement of heat insulation performance and is ideal for reducing the weight of the battery of the spacecraft. In addition, magnetic transmissive multi-layer insulation (MT-MLI) is developed to suppress the generation of eddy currents. In WPT experiments with MT-MLI, the power transmission efficiency between coils is 90% or more. Furthermore, thermal vacuum tests demonstrate that the combination of WPT and MT-MLI reduces thermal leakage.

本誌: IEEJ Journal of Industry Applications Vol.12 No.3 (2023) Special Issue on “IPEC-Himeji 2022”

本誌掲載ページ: 467-474 p

原稿種別: 論文/英語

電子版へのリンク: https://www.jstage.jst.go.jp/article/ieejjia/12/3/12_22007943/_article/-char/ja/

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