Výsledky vyhledávání - "大型宇宙構造物"

Plasma and solar array arcing caused by space debris impact

Autor: Cho, Mengu, Fukushige, Shinya, Akahoshi, Yasuhiro, Watanabe, Keiko, Nagasaki, Toshikazu, Sugawara, Kensho, Kora, Takao

Publikováno v: 宇宙航空研究開発機構特別資料: 第4回宇宙環境シンポジウム講演論文集 = JAXA Special Publication: Proceedings of the 4th Spacecraft Environment Symposium. :113-116

There is high possibility that space debris impacts to a solar array paddle in spacecraft parts, because the solar array paddle has large area. Space debris impact to the solar array causes not only mechanical damage but also electrical damage such a

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::884b52f7b3aa32f47466dca3772c30d7
http://id.nii.ac.jp/1696/00005501/

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再構成型宇宙構造物の制御へのパラメータ推定の適用

Autor: Sawayama, Keita, Machida, Kazuo, Matsuzawa, Takashi, Iwata, Toshiaki, Tsutsumi, Yosuke

Publikováno v: 第17回アストロダイナミクスシンポジウム講演後刷り集 2007 = Proceedings of 17th Workshop on JAXA Astrodynamics and Flight Mechanics. :356-361

筆者らは、太陽発電衛星などの大型宇宙構造物の構築に再構成型宇宙構造物を利用することを提案してきた。本稿では、再構成型宇宙構造物の制御手法について考察し、再構成型宇宙構�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::19d8730ff0318636150852e1ce7106cc
http://id.nii.ac.jp/1696/00007490/

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Static deployment of large membrane using a balloon

Autor: Mori, Osamu, Nishimaki, Shuhei, Matsumoto, Michihiro, Iwakura, Atsushi, Arakawa, Masataka, Shibasaki, Yusuke, Hanaoka, Fuminori, Sugita, Masayuki, Shida, Maki, Kawaguchi, Junichiro

Publikováno v: 宇宙航空研究開発機構研究開発報告: 大気球研究報告 = JAXA Research and Development Report: Research Reports on High Altitude Balloons. :35-66

ISAS/JAXAが提案しているソーラー電力セイル計画では、φ50m程度の膜面を遠心力で展開・展張することが重要な技術課題となっている。一般に、大型膜面を動的に展開する場合、膜面がね�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::972f5351a7720a3e29312416cf7ad5aa
http://id.nii.ac.jp/1696/00002162/

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Possibility of sustained arc on solar array through plasma created by space debris impact

Autor: Cho, Mengu, Fukushige, Shinya, Akahoshi, Yasuhiro, Watanabe, Keiko, Furusawa, Naomi, Kusunoki, Shuhei, Kora, Takao, Hosoda, Satoshi, Harada, Shoji, Fujita, Tatsuhito

Publikováno v: 宇宙航空研究開発機構特別資料: 第3回宇宙環境シンポジウム講演論文集 = JAXA Special Publication: Proceedings of the 3rd Spacecraft Environment Symposium. :127-130

In recent years, a solar array of a spacecraft has become larger with the voltage higher. Therefore, the risk of debris impact and discharge on the solar array is increasing. There is danger that discharge through the plasma created by debris impact

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::433304f28fab05620ecaf697379c8fe0
http://id.nii.ac.jp/1696/00005705/

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テザーを伴う柔軟構造物の制御特性に関する解析

Autor: Watanabe, Takeo, Kusagaya, Tairo, Fujii, Hironori A., Koga, Yusuke, Tanemura, Motoki, Fukudome, Hiroyuki, Mori, Takeshi, Anma, Kenichi, Niitsu, Mayuki

Publikováno v: 第16回アストロダイナミクスシンポジウム講演後刷り集 2006 = Proceedings of 16th Workshop on JAXA Astrodynamics and Flight Mechanics. :303-307

テザー型太陽発電衛星(SSPS: Space Solar Power Systems)など、テザーを伴う大型柔軟構造物において、テザーを制御アクチュエータとして用いる案が検討されているが、テザーの非線形性が柔軟�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::11bb5496ed62199977c2435e693e17e5
http://id.nii.ac.jp/1696/00007547/

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Construction of a model of solar radiation pressure for ASTRO-G satellite

Autor: Kubooka, Toshihiro, Otsubo, Toshimichi, Yoshikawa, Makoto

Publikováno v: 第7回宇宙科学シンポジウム = Proceedings of the 7th Space Science Symposium. :727-731

資料番号: AA0063354022

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::b244a5d6d7ef62504e3d9521c46df806
http://id.nii.ac.jp/1696/00011167/

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Space applicability study on carbon reinforced shape memory polymer

Autor: Ishizawa, Junichiro, Minami, Shintaro, Shimamura, Hiroyuki

Publikováno v: 宇宙航空研究開発機構特別資料: 平成18年度宇宙航空研究開発機構総合技術研究本部宇宙科学研究本部研究成果報告書 = JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency. :53-56

Carbon fiber reinforced shape memory polymer (FR-SMP) has been developed for space deployable structures as solar paddles, antennas, etc. This material is lightweight, low-cost, and has high workability. We have experimentally proved enough tolerance

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::7d8fcf80a060878f665d14834335ef05
http://id.nii.ac.jp/1696/00005988/

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On-orbit attitude control experiments of ETS-8

Autor: Otani, Takashi, Mitani, Shinji, Hamada, Yoshiro, Yamaguchi, Isao, Kasai, Tokio, Igawa, Hirotaka

A case study on advanced attitude control experiments of ETS-8 is reported in this paper. ETS-8 is scheduled to be launched on a H2A launch vehicle in 2006. In this experiment, spacecraft attitude control techniques for MIMO (Multi Input Multi Output

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::6645b8777bda45202b4cc9d22048e4f8
http://id.nii.ac.jp/1696/00006058/

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On-orbit system identification experiments of ETS-8

Autor: Yamaguchi, Isao, Kasai, Tokio, Igawa, Hirotaka, Hamada, Yoshiro, Mitani, Shinji, Otani, Takashi, Ikeda, Masafumi, Usui, Motofumi, Sunagawa, Kei

This report describes the studies on the on-orbit system identification experiments using ETS-8 (Engineering Test Satellite 8). ETS-8 will be launched by H-2A launch vehicle in fiscal year 2006. ETS-8 has large-scale, flexible Large Deployable Reflec

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::d7351fe2caba5bbfcf2bde30250f9448
http://id.nii.ac.jp/1696/00006031/

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ソーラーセイル薄膜展開実験について

Autor: Shimose, Shigeru

Solar Sail move by receiving momentum of photons in sunlight. This paper presents results of some Spin-Stabilized Solar Sail deployment experiment. ISAS has successfully deployed, for the first time in the world, the polyimide Solar Sail taking advan

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::4eab068bc5aa8f9e5e4b3c4a56935be2
http://id.nii.ac.jp/1696/00006030/

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