Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Fukushige, Shinya"'
Publikováno v:
Advanced Composite Materials; Aug2024, Vol. 33 Issue 4, p581-602, 22p
Publikováno v:
In Additive Manufacturing January 2020 31
Autor:
DAIBO, Soya, AKAHOSHI, Yasuhiro, UCHIDA, Takeshi, KITAGURO, Yuma, FUJII, Masanori, KOURA, Takao, KAWAMOTO, Satomi, JOUDOI, Daisuke, KIMOTO, Yugo, NAGAOKA, Nobuaki, HARADA, Ryusuke, IZUMIYAMA, Taku, FUKUSHIGE, Shinya, KITAZAWA, Yukihito
第10回スペースデブリワークショップ (2022年11月28-30日. 主催: 宇宙航空研究開発機構研究開発部門(JAXA), 宇宙航空研究開発機構調布航空宇宙センター(JAXA)(CAC)), 調布市, 東京
The 10th Space
The 10th Space
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::018f0bf8e02109681bfbdbccf99fac83
http://id.nii.ac.jp/1696/00049216/
http://id.nii.ac.jp/1696/00049216/
Autor:
Cho, Mengu, Nagasaki, Toshikazu, Fukushige, Shinya, Akahoshi, Yasuhiro, Watanabe, Keiko, Sugahara, Kensho, Kora, Takao, Harada, Shoji
Publikováno v:
第27回宇宙エネルギーシンポジウム 平成19年度 = The Twenty-seventh Space Energy Symposium. :54-58
In recent years, space debris increases because many rockets and satellites have been launched. A solar array of a spacecraft has become larger with the higher voltage and electrical power. Therefore, the risk of debris impact and possibility of disc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::55236e26798d27b2f66ac37c62cc99e7
http://id.nii.ac.jp/1696/00008018/
http://id.nii.ac.jp/1696/00008018/
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/
http://id.nii.ac.jp/1696/00005501/
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. :117-122
Space agencies of some countries have space debris environment model for design of spacecrafts. These models can estimate debris flux as a function of the size, relative impact velocity, and impact angle in a spacecraft orbit. However, it is known ca
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::d92d826cb5b55368fbcaa7fd1bc12c4e
http://id.nii.ac.jp/1696/00005703/
http://id.nii.ac.jp/1696/00005703/
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/
http://id.nii.ac.jp/1696/00005705/
Autor:
Fukushige, Shinya, Akahoshi, Yasuhiro, Watanabe, Keiko, Furusawa, Naomi, Kusunoki, Shuhei, Koura, Takao, Hosoda, Satoshi, Cho, Mengu, Fujita, Tatsuhito
Publikováno v:
第26回宇宙エネルギーシンポジウム 平成18年度 = The Twenty-sixth Space Energy Synmposium. :31-35
第26回宇宙エネルギーシンポジウム 平成18年度（2007年3月12日. 宇宙航空研究開発機構宇宙科学研究本部 (JAXA)(ISAS)）, 相模原市, 神奈川県
The Twenty-sixth Space Energy Synmposium (March 12, 2007. Insti
The Twenty-sixth Space Energy Synmposium (March 12, 2007. Insti
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::9f5e5c8d95739370e94ac5dca88510b1
http://id.nii.ac.jp/1696/00008043/
http://id.nii.ac.jp/1696/00008043/
Autor:
Cho, Mengu, Akahoshi, Yasuhiro, Harano, Takayuki, Machida, Yu, Fukushige, Shinya, Kora, Takao, Hosoda, Satoshi
Publikováno v:
宇宙航空研究開発機構特別資料 = JAXA Special Publication: 9th Spacecraft Charging Technology Conference. :697-702
Recently solar array has become higher in potential and larger in capacitance. Therefore, possibility of collision between space debris and enlarged solar array has been pointed out. Actually, a lot of debris and dust impacts were confirmed on fusela
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::8acf888905786bb4af541812f05c6a69
http://id.nii.ac.jp/1696/00006387/
http://id.nii.ac.jp/1696/00006387/
Autor:
Fukushige, Shinya1 shinyafk@yahoo.co.jp, Akahoshi, Yasuhiro1 akaho@mech.kyutech.ac.jp, Watanabe, Keiko2 keikow@me.es.osaka-u.ac.jp, Nagasaki, Toshikazu1, Sugawara, Kenshou1, Koura, Takao1, Mengu Cho3
Publikováno v:
IEEE Transactions on Plasma Science. Oct2008 Part 2 of 4, Vol. 36 Issue 5, p2434-2439. 6p. 2 Black and White Photographs, 1 Diagram, 2 Charts, 7 Graphs.