Design, preparation and properties of carbon fiber reinforced ultra-high temperature ceramic composites for aerospace applications: a review

S Tang, C Hu - Journal of Materials Science & Technology, 2017 - Elsevier
Carbon fiber reinforced ultra-high temperature ceramic (UHTC) composites, consisting of
carbon fibers embedded in a UHTC-matrix or a C–SiC–UHTC-matrix, are deemed as the …

Review of research progress in nontraditional machining of ultrahigh-temperature ceramic matrix composites

Y Lu, P Sun, X Yang, X Guo, X Li, W Ming - Coatings, 2023 - mdpi.com
Ultrahigh-temperature ceramic matrix composites are currently among the most promising
high-temperature-resistant materials, owing to their high-temperature strength, high …

[图书][B] Fundamentals of turbulent and multiphase combustion

KK Kuo, R Acharya - 2012 - books.google.com
Detailed coverage of advanced combustion topics from the author of Principles of
combustion, Second Edition Turbulence, turbulent combustion, and multiphase reacting …

Ablation of the carbon/carbon composite nozzle-throats in a small solid rocket motor

KZ Li, XT Shen, HJ Li, SY Zhang, T Feng, LL Zhang - Carbon, 2011 - Elsevier
Ablation of needled carbon/carbon (C/C) composite nozzle-throats was studied by hot-fire
testing in a small solid rocket motor. The composition of the combustion gases was …

Numerical analysis of nozzle material thermochemical erosion in hybrid rocket engines

D Bianchi, F Nasuti - Journal of Propulsion and Power, 2013 - arc.aiaa.org
Ablative materials are commonly used to protect the nozzle metallic housing and to provide
the internal contour to expand the exhaust gases in both solid and hybrid rockets. Because …

Thermochemical erosion analysis for chraphite/carbon-carbon rocket nozzles

D Bianchi, F Nasuti, M Onofri, E Martelli - Journal of Propulsion and …, 2011 - arc.aiaa.org
WITH the development of high-energy solid propellants and harder firing conditions in
advanced solid rocket motors (SRMs), graphite and carbon–carbon composites have found …

[HTML][HTML] Research progress in antioxidation and anti-ablation coatings of carbon-based materials: A review

Y Tian, H Cui, Y Jiang, N Wang - Resources Chemicals and Materials, 2024 - Elsevier
Carbon materials (graphite or C/C composites) are widely used in aerospace applications
due to their unique performance advantages, including low density, high specific strength …

Navier-Stokes simulations of hypersonic flows with coupled graphite ablation

D Bianchi, F Nasuti, E Martelli - Journal of Spacecraft and Rockets, 2010 - arc.aiaa.org
UPON exposure to ballistic reentry environments, ablative thermal protection systems (TPS)
are subjected to severe thermal and mechanical conditions and must be designed to keep …

Chemical erosion of carbon-phenolic rocket nozzles with finite-rate surface chemistry

D Bianchi, A Turchi, F Nasuti, M Onofri - Journal of Propulsion and …, 2013 - arc.aiaa.org
Ablative materials are commonly used to protect the nozzle metallic housing and to provide
the internal contour to expand the exhaust gases in solid rocket motors. Because of the …

Ablation behaviour of C/C–ZrC composites in a solid rocket motor environment

XT Shen, L Liu, W Li, KZ Li - Ceramics International, 2015 - Elsevier
Abstract Ablation of C/C–ZrC composites in a solid rocket motor environment was
investigated. The chemical compositions of the combustion gases were calculated using the …