Výsledky vyhledávání

High altitude performance tests of perfect ZrO2/Ni FGM chamber

Autor: Kuroda, Yukio, Sato, Masahiro, Tadano, Makoto, Moriya, Shinichi, Kusaka, Kazuo, Kumagai, Tatsuo, Moro, Akio, Taguchi, Hideyuki, Kawamata, Yoshihiro, Miki, Yoichiro

Publikováno v: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory. 1327:1-18

将来の宇宙往還機用軌道制御システムの実現には、既存の2液式エンジンより高性能で耐久性を有する再使用型エンジンの実用化が不可欠である。この要求に応えるため、エンジンの高性

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::25b31458435d678e180f8e95b8bcb81c
http://id.nii.ac.jp/1696/00039956/

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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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Effect of film cooling/regenerative cooling on scramjet engine performances

Autor: Kanda, Takeshi, Masuya, Goro, Ono, Fumiei, Moro, Akio, Wakamatsu, Yoshio

Publikováno v: Journal of Propulsion and Power. 10(5):618-624

Eleventh International Symposium on Air Breathing Engines (September 20-24, 1993.), Tokyo, Japan
資料番号: AC1000115000
レポート番号: ISABE 93-7036

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::5c9c546f4ac5a36cc719b8506000ebdf
http://id.nii.ac.jp/1696/00021258/

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Theoretical performance of rocket engine for liquid oxygen/high density hydrocarbon/metal system

Autor: Sato, Kazuo, Moro, Akio, Yatsuyanagi, Nobuyuki, Sakamoto, Hiroshi

Publikováno v: 航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory. 659:1-10

液体酸素・炭化水素燃料に金属を添加したロケット推進薬の理論性能計算を1次元化学平衡流の手法を用いて行った。炭化水素には密度ρ=851kg/立方メートルの石油系炭化水素燃料RJ-1Jを用�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::4e2cc6e066e413334c323be7c53442fa
http://id.nii.ac.jp/1696/00041120/

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Application of C/C composites for RCS engines: Evaluation test of S[lc]iC/C-FGM coating chambers

Autor: Sato, Masahiro, Tadano, Makoto, Kusaka, Kazuo, Niino, Masayuki, Moro, Akio

Publikováno v: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory. 1427

近い将来における宇宙輸送系システムの再使用化のため、姿勢制御用(RCS)スラスタにおいても軽量、高耐久性且つ高性能化が課題となる。我々はこの課題達成のため、燃焼室材料に従来�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::af659e4051b0c64170f3fe48b90c2309
http://id.nii.ac.jp/1696/00042414/

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Conference

Impulse generated from laser targets.

Autor: Niino, Masayuki, Kmetik, Viliam, Kumagai, Tatsuo, Moro, Akio, Kibe, Seishiro, Imasaki, Kazuo

Publikováno v: Proceedings of SPIE; Nov2000 Part 2, Issue 1, p370-377, 8p

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傾斜機能材料データベースの作製

Autor: SUDO, Takayuki, KISARA, Katsuto, MORO, Akio, NIINO, Masayuki, ISHIBASHI, KENJI

Publikováno v: 航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory. 621:36

現在,「熱応力緩和のための傾斜機能材料開発の基盤技術に関する研究」が科学技術振興調整費によって進められている。この研究を効率的に推進するためにはデータベースが不可欠であ

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::7399a7de7f936d45400d007a4b4cfba1
http://id.nii.ac.jp/1696/00044198/

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液体酸素・液体水素小型高膨張燃焼器の実験(1)

Autor: MIYAJIMA, Hiroshi, MORO, Akio, KUSAKA, Kazuo, NAKAHASHI, Kazuhiro, KURODA, Yukio, KUMAGAI, Tatsuo, KISARA, Katsuto, KAMATA, Makoto, SATO, Masahiro, ABE, Noboru, KATSUTA, Hideaki

Publikováno v: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-662. 662:26

The performance of a thrust chamber with a nozzle whose nominal expansion area ratio was 140:1 was evaluated under environmental pressure of 8 to 13 torr. The nominal vacuum thrust of the chamber was 400kgf at a chamber pressure of 35.5kg/cm2, abs. M

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::b29df302628d2c5106cd387b3a021078
http://id.nii.ac.jp/1696/00044913/

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An Investigation of the Numerical Methods for the High-Expansion Rocket Nozzle Flow Calculation

Autor: NAKAHASHI, Kazuhiro, MORO, Akio, MIYAJIMA, Hiroshi

Publikováno v: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-634. 634:11

This paper is concerned with an investigation of numerical methods for the inviscid flow calculation of a high-expansion rocket nozzle. A method of characteristics and a space-marching shock capturing finite-difference method are compared for the cal

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::fd124e2a7f945359434318469f8f4890
http://id.nii.ac.jp/1696/00044883/

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液酸・液水ロケットエンジン用点火器の真空着火試験

Autor: KISARA, Katsuto, MIYAJIMA, Hiroshi, ABE, Noboru, SATO, Masahiro, KAMATA, Makoto, SUDO, Takayuki, MORO, Akio, TORII, Yoshihiro

Publikováno v: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-732. 732:22

The LE-5 engine, which will be installed in the second stage of Japan’s next launch vehicle, requires tank head ignition of the main thrust chamber and allows a small pressure budget to the igniter. Vacuum ignition tests of the original igniter rev

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::49e9ece42eeeaa6fb237262279309d54
http://id.nii.ac.jp/1696/00044983/

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