Oxidation studies of SiC are reviewed and analyzed in terms of thermodynamics by crossing
the high temperature behavior of the SiC material-mainly the activities of its components …

The reentry conditions endured by a vehicle entering the atmosphere from an Earth orbit or
from an interplanetary trajectory are the most critical phases for materials used as Thermal …

Abstract Plasma-sprayed La 2 O 3-modified HfC-SiC (HSL) coating was prepared on SiC-
coated carbon/carbon composites to obtain an elevated ablation resistance under a heat …

An experimental campaign has been carried out to characterize a new class of Ultra-High-
Temperature Ceramic Matrix Composites for near-zero ablation Thermal Protection …

Abstract Two samples of Ultra-High-Temperature Ceramic Matrix Composites, with carbon
fibers in a ZrB 2-SiC matrix, were exposed to supersonic dissociated air flow, simulating the …

In this work, the microstructure, failure behavior and interfacial properties with respective to
the interfacial domain in SiC f/BN/SiC and C f/PyC/SiC composites were studied via the fiber …

To improve the ablation resistance of carbon/carbon (C/C) composites at ultra-high
temperature, La-modified ZrC coating was prepared on SiC-coated C/C composites by …

The effects of SiC content on aero-thermal resistance capabilities of ZrB 2-xSiC-5Y 2 O 3
ceramics (x= 5, 10, 15, 18.5 vol%) in atmospheric re-entry environment were investigated …

Long time oxidation protection at ultra-high temperatures or ablation protection has been a
choke point for C/C composites. In this study, long time ablation protection of different-La 2 O …

A novel composite reinforcement with horizontal multilayer" Spider web like" SiC nanowire
networks and vertical interconnected" Z-pins like" SiC rods was designed and prepared by …