热膨胀
航天器
材料科学
校准
机械工程
热的
球(数学)
望远镜
复合材料
计算机科学
航空航天工程
工程类
光学
物理
几何学
气象学
量子力学
数学
作者
Ralph Renz,Bernhard Heidenreich,Walter Krenkel,A. Schöppach,Frank M. Richter
标识
DOI:10.1002/3527605622.ch128
摘要
Carbon fibre reinforced CMC materials, originally developed for the thermal protection of reusable spacecrafts, offer a great applicability for extreme lightweight and thin walled structures combining an excellent strength to density ratio with a close to zero thermal expansion behaviour. These outstanding properties and a cost efficient manufacturing route, predestine these C/C-SiC materials for a variety of low CTE applications e.g. for telescopes or calibration artefacts. This paper deals with principal correlations between the thermal expansion of different C/C-SiC materials as well as their microstructural characterisation. Additionally, two special applications designed, manufactured and tested successfully in collaboration with industrial partners will be described exemplarily. One is a telescope structure for the data link between satellites based on an optical concept. The other application is a new calibration ball plate for coordinate measuring machines.
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