The results of propulsion system firing test for HTV

Autor:	Nagata, Taiichi, Kajiwara, Kenichi, Imada, Takane, Sasaki, Hiroshi
Jazyk:	japonština
Rok vydání:	2006
Předmět:	propulsion system configuration reaction control system ISS firing test 宇宙ステーション補給機 H-2 transfer vehicle combustion vibration 燃焼試験 推進システム性能 propulsion system performance spacecraft propulsion 燃焼振動 姿勢制御系 宇宙機推進 推進システム構成
Zdroj:	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
ISSN:	1349-113X
Popis:	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 propellant. 資料番号: AA0049056019 レポート番号: JAXA-SP-05-010
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=jairo_______::ff532a8857bddd3f5f350041748c143d http://id.nii.ac.jp/1696/00006244/ Zobrazit plný text záznamu