Výsledky vyhledávání - "推進システム性能"

The results of propulsion system firing test for HTV

Autor: Nagata, Taiichi, Kajiwara, Kenichi, Imada, Takane, Sasaki, Hiroshi

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. :93-98

The system firing test for HTV (H-2 Transfer Vehicle) was performed on June thru August, 2004. The result shows that the system provides approximately 50 percent thrust during short impulse RCS firings using four forward thrusters with GHe saturated

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::ff532a8857bddd3f5f350041748c143d
http://id.nii.ac.jp/1696/00006244/

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Performance analysis of pre-cooled turbojet engines for space planes

Autor: Taguchi, Hideyuki, Futamura, Hisao, Yanagi, Ryoji, Maita, Masataka

Publikováno v: 宇宙航空研究開発機構研究開発報告 = JAXA Research and Development Report.

宇宙航空機(スペースプレーン)に適用することを想定した予冷ターボエンジンの性能を評価することを目的として、エンジン性能解析、飛行解析、および質量推算を組み合わせたペイロ�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::68ff19ea3cc192cb65c26cd1e0bedd38
http://id.nii.ac.jp/1696/00002333/

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