High-precision CTE measurement of hybrid C/SiC composite for cryogenic space telescopes
K. Enya, N. Yamada, T. Imai, Y. Tange, H. Kaneda, H. Katayama, M., Kotani, K. Maruyama, M. Naitoh, T. Nakagawa, T. Onaka, M. Suganuma, T. Ozaki,, M. Kume, M. R. Krodel

TL;DR
This study precisely measures the thermal expansion of a hybrid C/SiC composite for cryogenic space telescopes, demonstrating significantly reduced anisotropy and providing detailed temperature-dependent data.
Contribution
It introduces a new hybrid C/SiC composite with reduced anisotropy and provides high-precision thermal expansion data across cryogenic temperatures.
Findings
Anisotropy reduced to 4% in the hybrid composite.
CTE values are approximately 0.805 and 0.837×10^{-6} K^{-1} for XY and Z directions.
Measurement accuracy better than 0.01×10^{-6} K^{-1}.
Abstract
This paper presents highly precise measurements of thermal expansion of a "hybrid" carbon-fiber reinforced silicon carbide composite, HB-Cesic\textregistered - a trademark of ECM, in the temperature region of \sim310-10K. Whilst C/SiC composites have been considered to be promising for the mirrors and other structures of space-borne cryogenic telescopes, the anisotropic thermal expansion has been a potential disadvantage of this material. HB-Cesic\textregistered is a newly developed composite using a mixture of different types of chopped, short carbon-fiber, in which one of the important aims of the development was to reduce the anisotropy. The measurements indicate that the anisotropy was much reduced down to 4% as a result of hybridization. The thermal expansion data obtained are presented as functions of temperature using eighth-order polynomials separately for the horizontal (XY-)…
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