Výsledky vyhledávání - "ロケットノズル"

Autor: Hori, Keiichi, Shimada, Toru, Tokudome, Shinichiro, Habu, Hiroto

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

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::0592d799324631f92a6b58d28f099893
http://id.nii.ac.jp/1696/00005544/

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Analytical evaluation of the solid rocket motor nozzle surface recession by the alumina-carbon reaction

Autor: Matsukawa, Yutaka, Sato, Yutaka

Publikováno v: 宇宙航空研究開発機構特別資料 = JAXA Special Publication: Proceedings of Lectures and Workshop International: Recent Advances in Multidisciplinary Technology and Modeling. :168-174

A theoretical model describing the chemical ablation of a solid rocket motor nozzle ablator by the alumina-carbon reaction is presented. An application of it to a typical solid rocket motor with a graphite nozzle ablator indicates a large influence o

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::e3819afaadf4de8a2e5d82196facccad
http://id.nii.ac.jp/1696/00005666/

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Standardization of test methods for evaluating the mechanical properties of 3D-C/C composites utilized for nozzle throats of solid rocket motors

Autor: Aoki, Takuya, Ogasawara, Toshio, Hatta, Hiroshi, Ishikawa, Takashi, Goto, Ken

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. :61-66

Three-dimensionally reinforced carbon-fiber-reinforced carbon matrix (3D-C/C) composites have been applied to the nozzle throats of solid propellant rockets such as SRB-A and M-V due to the excellent heat resistance exceeding 2,273 K. In order to ass

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::c0e515b0ef55976cb833d6cf91057a64
http://id.nii.ac.jp/1696/00005990/

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The development of a Japanese 20N thruster valve for a spacecraft propulsion system

Autor: Nagata, Taiichi, Kushiki, Kenichi, Kajiwara, Kenichi

The Japan Aerospace Exploration Agency (JAXA) is now developing a 20N-class thruster valve for spacecraft propulsion systems. We intend to develop this valve with the high reliability, and a robust and durable design. The suspended armature type was

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::21f9155af422e95da52425f367d01dae
http://id.nii.ac.jp/1696/00006040/

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Development of ceramic thruster

Autor: Nakatsuka, Junichi, Sawai, Shujiro

In recent days, the propulsion subsystem of spacecraft is required to achieve higher reliability and performance simultaneously. The performance of thrusters has a great impact to the weight budget of the propulsion subsystem, because high performanc

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::afc91331a453142b9837fdbed5694976
http://id.nii.ac.jp/1696/00006039/

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Experimental analysis of the effect of side walls of a linear aerospike nozzle on the jet-flow structure

Autor: Mori, Hideo, Taniguchi, Mashio, Nishihira, Ryutaro, Niimi, Tomohide

Publikováno v: 宇宙航行の力学シンポジウム平成16年度 = Symposium on Flight Mechanics and Astrodynamics 2004. :120-123

資料番号: AA0048089031

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::b017d855c26a05231e94c67816638e49
http://id.nii.ac.jp/1696/00014632/

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過膨張時のロケットノズル内部流の数値解析

Autor: Kim, Hyoung Chol, Nakahashi, Kazuhiro, Obayashi, Shigeru

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. :113-118

資料番号: AA0047427021
レポート番号: JAXA-SP-03-002

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::5fbdd27dde44b22dd2348b89f548562a
http://id.nii.ac.jp/1696/00006616/

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Three dimensional numerical analysis on the lateral force generated at a rocket nozzle

Autor: Shimizu, Taro, Miyajima, Hiroshi, Kodera, Masatoshi

Publikováno v: 宇宙輸送シンポジウム平成14年度 = Proceedings of Space Transportation Symposium FY2002. :95-98

資料番号: AA0045426024

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::2d39993ed0e16c0301ef0e0efe745494
http://id.nii.ac.jp/1696/00017354/

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Experimental study on the erosive combustion of practical solid rocket propellants

Autor: Hasegawa, Hiroshi, Hanzawa, Masahisa, Kobayashi, Kiyokazu, Tokudome, Shinichiro, Shimada, Toru, Kono, Masahiro

Publikováno v: 宇宙輸送シンポジウム平成13年度 = Proceedings of Space Transportation Symposium FY2001. :29-32

DSM燃焼試験結果に対して実績のある相関式を用いて、S-310改用推進薬BP-206Jに関してDSMおよび直径80モータ燃焼試験から同相関式を実機侵食燃焼予測に適用する際の妥当性を検討した。結�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::037469e43861c84d6e6b0861add30592
http://id.nii.ac.jp/1696/00017430/

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