Výsledky vyhledávání - "Kanmuri, Akio"

Three-Center coordinated core research and development project for rocket engines

Autor: Kanmuri, Akio

Publikováno v: 宇宙輸送シンポジウム平成13年度 = Proceedings of Space Transportation Symposium FY2001. :139-142

プロジェクト推進会議による運営の下(共通の場)で、H-2Aロケットエンジンに係わる技術課題を中心に3機関連携による研究が進められ、新しい連携の形が実現された。プロジェクト推進会

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::f23fa1c93d3b67c5cbc27475056e1293
http://id.nii.ac.jp/1696/00017457/

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再生冷却が液体ロケットエンジンの比推力に及ぼす効果

Autor: Kanda, Takeshi, Masuya, Goro, Wakamatsu, Yoshio, Kanmuri, Akio, Chinzei, Nobuo, Niino, Masayuki

Publikováno v: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory. :1-9

再生冷却が液体ロケットエンジンの比推力に及ぼす効果について、準1次元シミュレーションモデルを用いて検討した。ロケットエンジンのノズルスカートの再生冷却は、エンジン比推力

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::29be18f589f3f89d50c98e170d543c2a
http://id.nii.ac.jp/1696/00041178/

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Transient simulation of LOX/LH2 rocket engine, LE-7

Autor: Imoto, takayuki, Sito, Takashi, Kanmuri, Akio, Wakamatsu, Yoshio, Kanda, Takeshi, Torii, Yoshihiro, Nagao, Ryuuji, Kitakura, Kazuhisa, Okada, Masashi, Hasegawa, Keiichi

Publikováno v: Proceedings of the 17th International Symposium on Space Technology and Science. 1:133-138

17th International Symposium on Space Technology and Science (May 20-25, 1990.), Tokyo, Japan
資料番号: AC1000110000

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::e93030d75994308890ccd78a5beb36de
http://id.nii.ac.jp/1696/00038494/

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Performance Analysis of Idealized Scramjet

Autor: Wakamatsu, Yoshio, Masuya, Goro, Kanda, Takeshi, Chinzei, Nobuo, Kanmuri, Akio

Publikováno v: Proceedings of the 17th International Symposium on Space Technology and Science. 1:303-308

17th International Symposium on Space Technology and Science (May 20-25, 1990.), Tokyo, Japan
資料番号: AC1000111000

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::125a2d1507a689da21548c264f56f8b1
http://id.nii.ac.jp/1696/00038495/

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Start Transient Simulation of LOX/LH２ Staged Combustion Cycle Engine

Autor: Wakamatsu, Yoshio, Kanmuri, Akio, Kanda, Takeshi, Torii, Yoshihiro

Publikováno v: Proceedings of the 15th International Symposium on Space Technology and Science. 1:315-320

15th International Symposium on Space Technology and Science (May 19-23, 1986.), Tokyo, Japan
資料番号: AC1000108000

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::9edf587b41a2d04f9fc42147fba05dad
http://id.nii.ac.jp/1696/00038492/

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Start Transient Analysis of LOX/LH２ Rocket Engine(LE-7)

Autor: Kagawa, Eiji, Kanmuri, Akio, Kanda, Takeshi, Wakamatsu, Yoshio, Torii, Yoshihiro, Hasegawa, Keiichi

Publikováno v: Proceedings of the 16st International Symposium on Space Technology and Science. 1:309-314

16st International Symposium on Space Technology and Science (May 22-27, 1988.), Sapporo, Hokkaido, Japan
資料番号: AC1000114000

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::e43689d8296ac34c904d99db11051432
http://id.nii.ac.jp/1696/00038498/

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Transient analysis of LOX/LH2 rocket engine (LE-7)

Autor: Kanmuri, Akio, Kanda, Takeshi, Wakamatsu, Yoshio, Torii, Yoshihiro, Kagawa, Hideshi, Hasegawa, Keiichi

Publikováno v: ASME, SAE, and ASEE, Joint Propulsion Conference, 25th, Monterey, CA, July 10-13, 1989.

ASME, SAE, and ASEE, Joint Propulsion Conference, 25th, Monterey, CA, July 10-13, 1989
資料番号: AC1000090000
レポート番号: AIAA-1989-2736

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2529d2701ef296da5e776679c7f8149a
http://id.nii.ac.jp/1696/00038474/

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スクラムジェット・エンジン特性の検討

Autor: KANDA, Takeshi, MASUYA, Goro, WAKAMATSU, Yoshio, CHINZEI, NOBUO, KANMURI, Akio

Publikováno v: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-1041. 1041:21

In a previous report, we compared scramjet engine characteristics of different propellant feed cycles, and discussed engine performances. In this study, we examined a hydrogen fueled airframe-integrated scramjet, considered the cooling of the airfram

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::8fb410a257fc0d73ac7b6c2469dea26c
http://id.nii.ac.jp/1696/00045294/

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太陽熱を利用した小型液酸/液水ロケットエンジン

Autor: KANDA, Takeshi, WAKAMATSU, Yoshio, KANMURI, Akio

Publikováno v: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-992. 992:12

Solar energy is already used in the form of electric power generated by solar cells in satellites. And a solar thermal propusion system, a kind of gas jet engine, has been studied. Large expansion area engines have been studied to achieve high specif

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::b7b0788618f2fd75d995833d1fa1bf60
http://id.nii.ac.jp/1696/00045245/

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Start Transient Analysis of Turbopump-fed LOX/LH2 Rocket Engine (LE-5)

Autor: KANMURI, Akio, WAKAMATSU, Yoshio, SHIMURA, Takashi, TOKI, Kyoichiro, TORII, Yoshihiro

Publikováno v: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-868. 868:33

The first Japanese LOX/LH2 rocket engine (LE-5) employs a turbopump-fed gas generator cycle system. The LE-5 engine starts up in such an unique method that the power of the turbopump system is at first built up by a coolant bleed cycle followed by a

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::f9e09c3e9b7bd22c6cc7fa4504408e1f
http://id.nii.ac.jp/1696/00045120/

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