Výsledky vyhledávání - "推進システム"

The results of propulsion system firing test for HTV

Autor: Nagata, Taiichi, Kajiwara, Kenichi, Imada, Takane, Sasaki, Hiroshi

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:宇宙輸送系基盤技術 = 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 Space Transportation Systems. :93-98

The system firing test for HTV (H-2 Transfer Vehicle) was performed on June thru August, 2004. The result shows that the system provides approximately 50 percent thrust during short impulse RCS firings using four forward thrusters with GHe saturated

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::ff532a8857bddd3f5f350041748c143d
http://id.nii.ac.jp/1696/00006244/

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CFD application to SST propulsion system

Autor: Oba, Yoshinori, Kodama, Hidekazu, Nozaki, Osamu, Kikuchi, Kazuo, Nishizawa, Toshio, Matsuo, Yuichi

Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. :109-114

航空宇宙技術研究所 17-19 Jan. 2000 東京日本
National Aerospace Laboratory 17-19 Jan. 2000 Tokyo Japan
SSTの推進システムは、離陸のときのマッハ3から極超音速輸送のときのマッハ5までの領域で�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::9c5f04a319c121a5435675e2a5e96d5d
http://id.nii.ac.jp/1696/00041424/

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次世代超音速民間輸送機の設計のための数値シミュレーション技術に関する国際ワークショップ

Autor: National Aerospace Laboratory

Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. :1-234

航空宇宙技術研究所 17-19 Jan. 2000 東京日本
National Aerospace Laboratory 17-19 Jan. 2000 Tokyo Japan
ワークショップの各部会における以下の課題について発表された研究が報告されている。(1)�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::8df4a8cf66ad17b33e6315beb245fe95
http://id.nii.ac.jp/1696/00041410/

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Integrated ground test Water-Energy-Cycle Space Propulsion System

Autor: Hashimoto, Yasunari, Tanaka, Koji, Ishii, Tadashi, Fujita, Takashi, Toki, Kyoichiro

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. :112-116

A space propulsion and a power generation system using Water-Energy-Cycle are integrated as a 'Water-Energy-Cycle Space Propulsion System' into a standard rack compatible to the Space Station 'Kibo' cabin. This newly conceptualized system stores hydr

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::e22f10d361a6160b7685ecddfa5c09f0
http://id.nii.ac.jp/1696/00008030/

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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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Integrated design methodology for highly reliable liquid rocket engine: Analytical modeling and experimental investigation of failure mechanism for engine dynamic simulator

Autor: Iwasaki, Fumiya, Kuratani, Naoshi, Aoki, Hiroshi, Yoshida, Makoto, Takada, Hitoshi, Kimura, Toshiya, Osada, Atsushi

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. :81-86

In the past, space propulsion systems were usually composed by accumulating the optimum design results for each component device. Therefore, 'system reliability level' was measured by long-time development tests. Recently, the new design method is re

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::861d66eab22220e8b7bd86d8d6bd7e23
http://id.nii.ac.jp/1696/00005995/

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A study of Water-Energy-Cycle space propulsion system

Autor: Toki, Kyoichiro, Hashimoto, Yasunari, Tanaka, Koji, Fujita, Takashi, Ishii, Tadashi

Publikováno v: 第24回宇宙エネルギーシンポジウム平成16年度 = The Twenty-fourth Space Energy Symposium March 7, 2005. :32-36

第25回宇宙利用シンポジウム(2009年1月14日-15日, 宇宙航空研究開発機構宇宙科学研究本部相模原キャンパス)
The Twenty-fifth Space Utilization Symposium (January 14-15, 2009: ISAS/JAXA Sagamihara, Japan)
A

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::45f0e3f15877582da959591dec4c58a3
http://id.nii.ac.jp/1696/00008087/

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Study status of the low-temperature two-liquid propulsion system

Autor: Habu, Hiroto, Mori, Osamu

Publikováno v: 第4回宇宙科学シンポジウム = Proceedings of the 4th Space Science Symposium. :199-202

資料番号: AA0047899046

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::bb73ff56d8d1ca796f6f2946216d8c6d
http://id.nii.ac.jp/1696/00011476/

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A space propulsion system with water cycles

Autor: Hashimoto, Yasunari, Toki, Kyoichiro, Fujita, Takashi, Ishii, Tadashi

Publikováno v: 宇宙輸送シンポジウム平成13年度 = Proceedings of Space Transportation Symposium FY2001. :91-94

資料番号: AA0033392023

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::21267748eeea8fb811b770fc3341a6de
http://id.nii.ac.jp/1696/00017445/

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Aerodynamic shape design of laminar wings for NAL powered experimental SST

Autor: Matsushima, Kisa, Iwamiya, Toshiyuki

Publikováno v: 航空宇宙技術研究所特別資料: 航空宇宙数値シミュレーション技術シンポジウム2001論文集 = Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2001. 53:221-226

The first stage of aerodynamic design of a main wing for NAL's second scaled experimental SST (Supersonic Transport) is reported. The second model has a propulsion system. The design has been done by using the strategy acquired from the wing design f

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::43e085ac7da7a5d89fa7013ef82adab0
http://id.nii.ac.jp/1696/00038068/

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