Výsledky vyhledávání - "再使用型ロケット"

CFD analysis of an aerodynamic body-flap effect for a basic SSTO-rocket configuration

Publikováno v: 宇宙航行の力学シンポジウム平成15年度 = Symposium on Flight Mechanics and Astrodynamics 2003. :63-66

Navier-Stokes simulations are carried out for the investigation of a body-flap effect on the subsonic to supersonic base-entry aerodynamic characteristics for the conical SSTO-rocket configuration. It is clarified that the body-flap effect has strong

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::fb973d8e31fbf9f9d32a5a3fb1621e5d
http://id.nii.ac.jp/1696/00014656/

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Durability tests of OMS subscale engine for H-2 orbiting plane

Autor: Kuroda, Yukio, Tadano, Makoto, Sato, Masahiro, Kusaka, Kazuo, Moro, Akio, Aoki, Yoshio, Miki, Yoichiro

Publikováno v: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory. 1294:1-27

将来の宇宙往還機に対応する再使用型高性能2液式エンジンの要求に応える為、金属とセラミックスの異種材料の組成を変化させた材料を1部に用いた燃焼器を製作し、エンジンの高性能�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::6dc963eb69f79b7d7c832e2be78d24a5
http://id.nii.ac.jp/1696/00039790/

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Research of reusable transportation system: Study of VTOL (Vertical Takeoff and Landing) experiment

Autor: Aoki, Hiroshi, Takano, Yutaka, Wada, Shigeaki, Iwanaga, Noriki, Ginoza, Akira

Publikováno v: 宇宙開発事業団技術報告 = NASDA Technical Memorandum. :1-221

現在｢再使用型のロケット｣の帰還形態として有翼型と垂直軟着陸型の2つが考えられている。前者の有翼型はH-2ロケット打上げ型有翼回収機(HOPE)実験による検討が進んでいる。後者の｢

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::97af056e1f9ca5ea44d3fbaf0b72c00c
http://id.nii.ac.jp/1696/00041106/

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Endurance test for the injector elements of reusable LOX/LH2 engine

Autor: Yagishita, Tsuyoshi, Tokudome, Shinichiro

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. :59-60

In the Institute of Space and Astronautical Science (ISAS), a flight test campaign for studying reusable space transportation system has been performed with a small vehicle having a 10 kN class LOX/LH2 propulsion system. As a part of this study, we a

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::871128036b3cafedc3974a4437827894
http://id.nii.ac.jp/1696/00006237/

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