Zobrazeno 1 - 10
of 22
pro vyhledávání: '"部品信頼性"'
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. :369-374
Japan Aerospace Exploration Agency (JAXA) developed Tuned Dry Gyroscope (TDG), as supreme precision rate sensor for satellite attitude control. JAXA also developed Inertial Reference Unit (IRU) using TDG. This IRU is used on every JAXA satellite. It
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. :395-400
A remote terminal converts signal protocols and relays housekeeping telemetry and command data between onboard data handling system and each non-intelligent sub-system. However, existing remote terminals cannot judge the contents of telemetry and gen
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. :303-306
The cause of a spacecraft check valve cracking pressure failure in a spacecraft SFT (System Firing Test) model was found deformation of the valve poppet by the failure analysis. This test was performed for investigation the cause of the deformation.
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:人工衛星系基盤技術 = 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 Satellite Systems. :193-196
It outlines the LSI-process diagnosis technology which screens the commercial components for high-reliability space applications. The inspection of the failure-included lot was performed, and the validity of this technique was examined recursively. A
Autor:
Sato, Makoto, Kawai, 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:人工衛星系基盤技術 = 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 Satellite Systems. :253-256
Japan Aerospace Exploration Agency (JAXA), formerly named as National Space Development Agency (NASDA), developed Tuned Dry Gyroscope (TDG), as supreme precision rate sensor for satellite attitude control. JAXA also developed Inertial Reference Unit
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:人工衛星系基盤技術 = 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 Satellite Systems. :207-210
A Committee for space part/component technologies has been set up since 2002 in JAXA (NASDA in those days). The committee was established to discuss about how we can acquire and maintain the world's most advanced technology with independence and flex
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:人工衛星系基盤技術 = 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 Satellite Systems. :201-206
Several failures of a new generation of Antifuse type FPGAs (RTSX-S, SX-A) were reported subsequent to successful programming in the U.S. in 2003. It was inferred that the degradation of Antifuses causes the signal delay after the investigations and
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:人工衛星系基盤技術 = 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 Satellite Systems. :237-240
We started developing an advanced reaction wheel based on a study for a reaction wheel with high torque and low disturbance characteristics since FY13. The advanced reaction wheel is characterized by small and high performance in comparison with a cu
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:人工衛星系基盤技術 = 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 Satellite Systems. :241-246
A spaceborne GPS receiver is a very useful component which enhances the autonomy of a next generation spacecraft; consequently the requirements for receivers are getting more advanced. Moreover, because of GPS modernization, new civil signals on L2 a
Autor:
Furukawa, Takashi, Shiwa, Mitsuharu, Sato, Akiyoshi, Yamazoe, Satoshi, Shinagawa, Yoshio, Ida, Takashi, Sato, Eiichi
Publikováno v:
第18回宇宙構造・材料シンポジウム = 18th Symposium on Aerospace Structure and Materials. :53-56
資料番号: AA0045440015