Zobrazeno 1 - 9 of 9 pro vyhledávání: '"ラジエータ"'
1
Thermal Design of Spacecraft and Thermophysical Properties
Autor: Tachikawa, Sumitaka
Publikováno v: 計測と制御 = Journal of The Society of Instrument and Control Engineers. 54(5):315-320
資料番号: SA1150252000
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::1c2e85dba1747a374d3e84e8c3a019dc
http://id.nii.ac.jp/1696/00028924/
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2
高Ohnesorge数領域における液滴流の捕集と飛散を分ける閾値
Autor: Totani, Tsuyoshi, Nanbu, Kota, Kawakami, Akihito, Yuri, Yasufumi, Nagata, Harunori
Publikováno v: 宇宙利用シンポジウム 第24回 平成19年度 = Space Utilization Research: Proceedings of the Twenty-fourth Space Utilization Symposium. :117-120
This research has aimed to prevent the working fluid from dispersing at the droplet collector of liquid droplet radiators by specifying the threshold in which splashing and spreading of droplets in space are divided. The following results have been a
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::a83414679d83fc49049352e647103468
http://id.nii.ac.jp/1696/00013398/
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3
A proposal of boiling and two-phase flow experiments utilizing a long-term microgravity environment
Autor: Ota, Haruhiko
Publikováno v: 宇宙利用シンポジウム 第24回 平成19年度 = Space Utilization Research: Proceedings of the Twenty-fourth Space Utilization Symposium. :127-130
Development of thermal management systems handling a large amount of waste heat and its long distance transportation becomes a key technology required for the long-term operation of large space platforms and of manned spacecraft systems. Boiling and
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::8c542382f5d0ee3dec694ada2674f0bb
http://id.nii.ac.jp/1696/00013400/
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4
技術試験衛星8型展開ラジエータ(DPR)の地上特性評価試験結果報告
Autor: Kawasaki, Haruo, Yabe, Takahiro, Okamoto, Atsushi, Noda, Hiroyuki
Publikováno v: 宇宙航空研究開発機構特別資料: 平成16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:人工衛星系基盤技術 = JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Satellite Systems. :11-16
The Deployable Radiator (DPR) with looped heat pipe is planed in Engineering Test Satellite. The loop heat pipes are able to transport heat over long distances in satellite. The thermal control systems such as the loop heat pipes are demanded with pr
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::8808469b5135524a36c33b2a60d48c22
http://id.nii.ac.jp/1696/00006253/
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5
Next generation heat pipe, Loop Heat Pipe
Autor: Ueno, Shiro, Nagai, Hiroki
Publikováno v: 第5回宇宙科学シンポジウム = Proceedings of the 5th Space Science Symposium. :509-512
ループ状に閉じたヒートパイプ「Loop Heat Pipe (LHP)」の利用が米国で主流になりつつある。2004年に打ち上げられた地球科学衛星Auraと、宇宙科学衛星SwiftにもLHPが搭載されている。一方日本
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::bdeccb88d36266c3485505da12cd9972
http://id.nii.ac.jp/1696/00011370/
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8
Design and analysis of a space deployment-type ultralight radiator
Autor: Kotani, Masaki, Uchida, Hideki, Tsukahara, Aiichiro
Publikováno v: 第19回宇宙構造・材料シンポジウム = 19th Symposium on Aerospace Structure and Materials. :12-15
宇宙機の熱制御サブシステムとして従来の排熱性能を上回るラジエータについて、設計技術を確立するための初期検討を行った。冷媒配管(フィーダ)と熱拡散面(フィン)からなる放熱面単
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::8fab29450ab8777ab7a3b676154df3f6
http://id.nii.ac.jp/1696/00015214/
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