Zobrazeno 1 - 10
of 126
pro vyhledávání: '"ロケットエンジン"'
Autor:
Kakudo, Hiromitsu
甲第24845号
工博第5162号
新制||工||1986(附属図書館)
学位規則第4条第1項該当
Doctor of Philosophy (Engineering)
Kyoto University
DFAM
工博第5162号
新制||工||1986(附属図書館)
学位規則第4条第1項該当
Doctor of Philosophy (Engineering)
Kyoto University
DFAM
Externí odkaz:
http://hdl.handle.net/2433/284778
Publikováno v:
宇宙航空研究開発機構特別資料: M-V型ロケット:5号機から8号機まで = JAXA Special Publication: The M-V Rockets: From the Fifth to the Eighth Vehicle. :41-78
資料番号: AA0064112005
レポート番号: JAXA-SP-07-023
レポート番号: JAXA-SP-07-023
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::0592d799324631f92a6b58d28f099893
http://id.nii.ac.jp/1696/00005544/
http://id.nii.ac.jp/1696/00005544/
Autor:
Shimada, Toru
Publikováno v:
宇宙航空研究開発機構特別資料: M-V型ロケット:5号機から8号機まで = JAXA Special Publication: The M-V Rockets: From the Fifth to the Eighth Vehicle. :5-10
資料番号: AA0064112002
レポート番号: JAXA-SP-07-023
レポート番号: JAXA-SP-07-023
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::84a38f2dced1b7b55b0e78f1b762331b
http://id.nii.ac.jp/1696/00005541/
http://id.nii.ac.jp/1696/00005541/
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. :93-98
Numerical simulations were conducted to predict the ejector pumping performance of our rocket-ramjet combined-cycle engine under a take-off condition, which will be tested in the Ramjet Engine Test Facility at Fy2006. Our code was verified by compari
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::53661b2cb40ff0a436aa27ec32045f6d
http://id.nii.ac.jp/1696/00005998/
http://id.nii.ac.jp/1696/00005998/
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/
http://id.nii.ac.jp/1696/00005995/
Publikováno v:
宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2005論文集 = JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2005. :215-220
The numerical simulations carried out for the rocket engine development at the Japan Aerospace Exploration Agency is presented. Although numerical simulations played a major role in the return to flight of the H-2A launch vehicle, the basic design of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::6136019d693555623d2829d600cadcaa
http://id.nii.ac.jp/1696/00006163/
http://id.nii.ac.jp/1696/00006163/
Autor:
Aoki, Hiroshi, Taguchi, Hideyuki, Kuratani, Naoshi, Okai, Keiichi, Kojima, Takayuki, Hasegawa, Takuya, Kanda, Takeshi
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. :25-30
In past, the Design for Space Systems has conducted accumulating the optimum design results for each device. 'System Reliability Level' was measured as the results of long time development tests. Recently, the new design method is required. It is nec
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::7b060bedcd042b237dcce7adbde54a66
http://id.nii.ac.jp/1696/00006230/
http://id.nii.ac.jp/1696/00006230/
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:輸送系 = JAXA Research and Development Memorandum: FY15 Annual Report of Research & Development on Space Technology in the Institute of Space Technology and Aeronautics: Space Transportation System. :49-52
This paper describes research and development activities on advanced technologies for liquid rocket engine system. These activities include the following four topics: 1) LOX/LNG engine test bed for low cost propulsion system, 2) Extendible nozzle for
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::a287ddad2a42fbe4f20317370db20904
http://id.nii.ac.jp/1696/00002735/
http://id.nii.ac.jp/1696/00002735/
Publikováno v:
宇宙輸送シンポジウム 平成15年度 = Proceedings of Space Transportation Symposium FY2003. :198-201
資料番号: AA0047118050
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::433fb68e8a5ae58a02b174c2c09eb40e
http://id.nii.ac.jp/1696/00017274/
http://id.nii.ac.jp/1696/00017274/
Autor:
Kimura, Toshiya, Takahashi, Masahiro, Wakamatsu, Yoshio, Hasegawa, Keiichi, Yamanishi, Nobuhiro
Publikováno v:
宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2003論文集 = JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2003. :107-112
The Rocket Engine Dynamic Simulator (REDS) has been developed. REDS is a kind of simulation tool to simulate and examine unsteady behavior of a rocket engine. A rocket engine is modeled as a system of pipes with various hydraulic elements such as tur
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::dba89e51a73c3d0458ab5266388bcbc7
http://id.nii.ac.jp/1696/00006615/
http://id.nii.ac.jp/1696/00006615/