Abstract
The development of ceramic matrix composites (CMCs) using 5 harness satin carbon fiber fabric impregnated with commercial polycarbosilane precursor plasticized by siloxane copolymer was investigated aiming to improve wetting behavior and shape conformability. The polycarbosilane precursor and polysiloxane plasticizer were mixed at varying weight ratios to obtain flexible preceramic resin prepreg cloths. 13 plies of preceramic polymer prepreg cloths were stacked in 0/90° layup and cured by compression molding, followed by densified via PIP process. The CMCs were densified with eight PIP cycles followed by final crystallization at 1600 °C. The CMCs made with 10 wt% polysiloxane loading showed lower viscosity of the prepreg resin as well as higher strength and displacement to failure compared to those fabricated from unplasticized polycarbosilane prepolymer. In contrast, at higher concentration of plasticizer, viscosity of the prepreg resin increased, and the CMC became more brittle; however, it exhibited considerably higher thermal conductivity.
| Original language | English |
|---|---|
| Article number | 118277 |
| Journal | Journal of the European Ceramic Society |
| Volume | 46 |
| Issue number | 10 |
| DOIs | |
| State | Published - Aug 2026 |
Funding
This manuscript has been authored by UT-Battelle LLC under Contract No. DE-AC05–00OR22725 with the U.S. Department of Energy. Authors thank Sandia National Laboratories’ Laboratory Directed Research and Development (LDRD) program for funding. Sandia National Laboratories is a multimission laboratory managed and operated by National Technology & Engineering Solutions of Sandia, LLC, a wholly owned subsidiary of Honeywell International Inc., for the U.S. Department of Energy’s National Nuclear Security Administration under contract DE-NA0003525 .
Keywords
- Carbosilane
- Ceramic matrix composites
- Polymer impregnation and pyrolysis (PIP)
- Siloxane
- Thermal conductivity
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