Zobrazeno 1 - 10
of 22
pro vyhledávání: '"Taniguchi, Hirofumi"'
Publikováno v:
In Acta Astronautica 2007 60(1):1-6
Publikováno v:
In Solid State Ionics October 2005 176(31-34):2367-2370
Publikováno v:
In Studies in Surface Science and Catalysis 2001 132:259-262
Autor:
Onodera, Takuo, Sakamoto, Hiroshi, Takahashi, Mamoru, Sasaki, Masaki, Tamura, Hiroshi, Kimura, Toshiya, Taniguchi, Hirofumi
Publikováno v:
日本航空宇宙学会北部支部2006年講演会および第7回再使用型宇宙推進系シンポジウム講演論文集 = Proceedings of the Annual Meeting and the Seventh Symposiun on Propulsion System for Reusable Launch Vehicles. :195-199
日本航空宇宙学会北部支部2006年講演会および第7回再使用型宇宙推進系シンポジウム(2006年3月9-10日), 仙台
資料番号: ARDS05503000
レポート番号: G-19
資料番号: ARDS05503000
レポート番号: G-19
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::47e9c81e3812230c98e95ba5a606a1f1
http://id.nii.ac.jp/1696/00039324/
http://id.nii.ac.jp/1696/00039324/
Autor:
Taniguchi, Hirofumi, Aoki, Hiroshi
Publikováno v:
宇宙航空研究開発機構研究開発資料: 平成15年度総合技術研究本部宇宙領域研究成果報告書:先行研究等 = JAXA Research and Development Memorandum: FY15 Annual Report of Research & Development on Space Technology in the Institute of Space Technology and Aeronautics: Advanced Technology. :31-34
To built the 10 Mkg class SSPS, the launch capability of over 20 Mkg to LEO is required. To satisfy these requirements for every year, standard transportation model is suggested. Low-cost reusable launch system has to be accomplished. In this study,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::df8349f602706738b00181c8b8bf077e
http://id.nii.ac.jp/1696/00002665/
http://id.nii.ac.jp/1696/00002665/
Publikováno v:
宇宙輸送シンポジウム 平成15年度 = Proceedings of Space Transportation Symposium FY2003. :158-161
A baseline configuration of the reusable rocket demonstration vehicle is presented. The vehicle adopts a vertical take-off and vertical landing (VTVL) system to minimize ground support equipments (GSE) and turn-around time. The integrated propulsion
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::1130ea1d03b7fde36e64dabd26832a9b
http://id.nii.ac.jp/1696/00017264/
http://id.nii.ac.jp/1696/00017264/
Autor:
Taniguchi, Hirofumi
Publikováno v:
宇宙輸送シンポジウム 平成14年度 = Proceedings of Space Transportation Symposium FY2002. :111-116
資料番号: AA0045426028
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::eab306f3478302463fe4d6718c6b5484
http://id.nii.ac.jp/1696/00017358/
http://id.nii.ac.jp/1696/00017358/
Akademický článek
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Autor:
Onodera, Takuo, Sakamoto, Hiroshi, Takahashi, Mamoru, Sasaki, Masaki, Tamura, Hiroshi, Kimura, Toshiya, Taniguchi, Hirofumi
Publikováno v:
総合技術研究本部・航空プログラムグループ 公開研究発表会前刷集.
総合技術研究本部・航空プログラムグループ 公開研究発表会(2005年12月7日)
資料番号: ARDS05480000
資料番号: ARDS05480000
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::b25c8eb749907e1208d0d83fd57d6219
http://id.nii.ac.jp/1696/00039309/
http://id.nii.ac.jp/1696/00039309/
Autor:
Onodera, Takuo, Sakamoto, Hiroshi, Takahashi, Mamoru, Sasaki, Masaki, Tamura, Hiroshi, Kimura, Toshiya, Taniguchi, Hirofumi
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. :41-42
Effects of liquid hydrogen mixer configurations on its downstream flow field were investigated. Cryogenic tests with different mixer configurations of eight patterns and CFD analysis were conducted. It was found that mixer configurations have strong
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::94340fc6a310c2617d3564b951580652
http://id.nii.ac.jp/1696/00006233/
http://id.nii.ac.jp/1696/00006233/