Evaluation of Spaceborne SiC Mirror Materials Using Samples Cut from the Periphery of a Mirror Body

被引:4
|
作者
Kotani, Masaki [1 ]
Muta, Yoshikazu [2 ]
Yoshimura, Akinori [1 ]
Ogihara, Shinji [2 ]
Imai, Tadashi [3 ]
Katayama, Haruyoshi [3 ]
Yui, Yukari [3 ]
Tange, Yoshio [3 ]
Enya, Keigo [4 ]
Kaneda, Hidehiro [5 ]
Nakagawa, Takao [4 ]
机构
[1] Japan Aerosp Explorat Agcy, Aerosp Res & Dev Directorate, Mitaka, Tokyo 1810015, Japan
[2] Tokyo Univ Sci, Fac Sci & Technol, Noda, Chiba 2788510, Japan
[3] Japan Aerosp Explorat Agcy, Space Applicat Mission Directorate, Tsukuba, Ibaraki 3058505, Japan
[4] Japan Aerosp Explorat Agcy, Inst Space & Astronaut Sci, Chuo Ku, Sagamihara, Kanagawa 2525210, Japan
[5] Nagoya Univ, Grad Sch Sci, Chikusa Ku, Nagoya, Aichi 4648602, Japan
关键词
coefficient of thermal expansion; material evaluation; microstructure; spaceborne SiC mirror; stiffness; C/SIC COMPOSITE; TELESCOPES; SURFACE;
D O I
10.1007/s11665-013-0827-1
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The Japan Aerospace Exploration Agency has studied large-scale, lightweight mirrors constructed of SiC-based materials as a key technology for future earth observations and astronomical missions. One of the most important technical issues for large-scale ceramic components is their quality stability (viz., differences in material properties depending on the part and the processing), which might influence the structural and/or thermal reliability through unforeseen deformation and breakage. In this study, the authors used a simple, low-cost method for evaluating the properties of SiC mirror materials. Using mechanical testing, thermodilatometry, and microstructural analysis on samples cut from the periphery of a prototype 800-mm-diameter mirror body, the overall quality of the mirror body material was determined.
引用
收藏
页码:850 / 858
页数:9
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