Carbon fiber reinforced carbon matrix (carbon/carbon, C/C) composites have become the
promising candidates for high‐temperature thermal structure materials in aerospace fields …

Carbon fiber reinforced carbon composites (C/Cs), are the most promising high-temperature
materials and could be widely applied in aerospace and nucleation fields, owing to their …

As nanotechnology rapidly advanced over the past decades, a variety of nanomaterials
have been developed and studied. Among them, SiC nanomaterials have recently attracted …

Silicon Carbide as an inorganic material possesses properties like high thermochemical
stability, high hardness and fracture toughness, low thermal expansion coefficient etc. It is …

A dense double layer ZrB 2-SiC-Si/SiC-Si coating with high content of ZrB 2 was designed
and fabricated by dipping-carbonization joint gaseous silicon infiltration. This coating can …

A joint chemical vapor infiltration-precursor infiltration and pyrolysis (CVI-PIP) process was
used to fabricate C/C-SiC-ZrC composites with different volume ratio of CVI-derived C-SiC …

A thick SiC coating was prepared on graphite by chemical vapor reaction. The coating
reveals a typical crystalline structure with limited porosity and combines well with the …

To reduce the influence of coating preparation on the mechanical properties of
carbon/carbon composites and further improve the antioxidant properties of the coating, a …

With the rapid development of space technology, multi-functional materials with advantages
such as heat insulation, lightweight, and electromagnetic (EM) wave absorption have gained …

To enhance the bonding strength and oxyacetylene ablation resistance of the ZrB 2–ZrC
coated C/C–ZrB 2–ZrC–SiC composites obtained by the combination of supersonic …