Zobrazeno 1 - 10 of 58 pro vyhledávání: '"極低温"'
1
Dissertation/ Thesis
Characterization and Compact Modeling of Silicon-Germanium Heterojunction Bipolar Transistors from Room to Cryogenic Temperatures
Autor: Jin, Xiaodi
SiGe HBTs are preferred for quantum computing (QC) readout circuits due to their high gain and speed as well as the integration with complementary metal-oxide-semiconductor (CMOS) technology. The device physics of SiGe HBTs at cryogenic temperatures
Externí odkaz: https://tud.qucosa.de/id/qucosa%3A93416
https://tud.qucosa.de/api/qucosa%3A93416/attachment/ATT-0/
Zobrazit plný text záznamu
2
Dissertation/ Thesis
Modeling of Heat Generation in Cryogenic Turbopump Bearing
Autor: Kakudo, Hiromitsu
甲第24845号
工博第5162号
新制||工||1986(附属図書館)
学位規則第4条第1項該当
Doctor of Philosophy (Engineering)
Kyoto University
DFAM
Externí odkaz: http://hdl.handle.net/2433/284778
Zobrazit plný text záznamu
3
Study status of the low-temperature two-liquid propulsion system
Autor: Habu, Hiroto, Mori, Osamu
Publikováno v: 第4回宇宙科学シンポジウム = Proceedings of the 4th Space Science Symposium. :199-202
資料番号: AA0047899046
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::bb73ff56d8d1ca796f6f2946216d8c6d
http://id.nii.ac.jp/1696/00011476/
Zobrazit plný text záznamu
5
Pressurized tests of a fuel-filled cryogenic propellant tank made of composite materials
Autor: Higuchi, Ken, Goto, Ken, Naruo, Yoshihiro, Namiki, Fumiharu
Publikováno v: 宇宙輸送シンポジウム 平成13年度 = Proceedings of Space Transportation Symposium FY2001. :131-134
近い将来に期待されるロケットの再使用化や軽量化に向けた重要な課題のひとつである極低温推進剤タンクの複合材化について、その材料特性の取得、タンクの設計・製作・試験に関す
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::f444c106e488e3082d7eb480e1544ab4
http://id.nii.ac.jp/1696/00017455/
Zobrazit plný text záznamu
6
Numerical simulation of sub-cooled liquid N2 nozzle flow with cavitation
Autor: Ito, Yutaka, Nagashima, Toshio
Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 46:221-226
航空宇宙技術研究所 7-9 Jun. 2000 東京 日本
National Aerospace Laboratory 7-9 Jun. 2000 Tokyo Japan
航空宇宙分野では、ロケットエンジンターボポンプの例に代表されるように高速流動を伴う極
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::ca7da16e4c45823500452279672c01bc
http://id.nii.ac.jp/1696/00041335/
Zobrazit plný text záznamu
7
Development of continuous ADR system for weak gravity missions
Autor: Shirron, Peter, Numazawa, Takenori, Kamiya, Koji, Mitsuda, Kazuhisa
Publikováno v: 宇宙利用シンポジウム 第24回 平成19年度 = Space Utilization Research: Proceedings of the Twenty-fourth Space Utilization Symposium. :133-135
A new continuous Adiabatic Demagnetization Refrigeration (ADR) system has been developed to provide the cooling temperatures between 0.06 K and 4 K. The system will consists of multi-stages of magnetic materials and magnets cascaded with heat switche
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::4ffaafd0615dcd5a39af6bfaa460870d
http://id.nii.ac.jp/1696/00013402/
Zobrazit plný text záznamu
9
Development of continuous ADR system for weak gravity missions
Autor: Shirron, Peter, Wegel, Don, Numazawa, Takenori, Kamiya, Koji, Mitsuda, Kazuhisa
Publikováno v: 宇宙利用シンポジウム 第23回 平成18年度 = Space Utilization Research: Proceedings of the Twenty-third Space Utilization Symposium. :205-208
Adiabatic Demagnetization Refrigeration (ADR) does not use working fluids contrary to conventional refrigerators that make use of the fluid density difference, which leads to superiority of the ADR under the weak gravity condition. We have been devel
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::75200170762ff3eb96b84fd29f6e728b
http://id.nii.ac.jp/1696/00013547/
Zobrazit plný text záznamu

Vyhledávací nástroje:

Upřesnit hledání

Omezení vyhledávání
Plný text Recenzováno Digitální knihovna AV ČR
Zdroje