Thermal Ablation Experiments of Carbon Phenolic and SiC-Coated Carbon Composite Materials Using a High-Velocity Oxygen-Fuel Torch

For future spacecraft TPS (heat shield) applications, ablation experiments of carbon phenolic material specimens with two lamination angles (0° and 30°) and two specially designed SiC-coated carbon–carbon composite specimens (with either cork or graphite base) were conducted using an HVOF material a...

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Detalles Bibliográficos
Autores principales: Chinnaraj, Rajesh Kumar, Kim, Young Chan, Choi, Seong Man
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2023
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC10003895/
https://www.ncbi.nlm.nih.gov/pubmed/36903009
http://dx.doi.org/10.3390/ma16051895

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC10003895/
https://www.ncbi.nlm.nih.gov/pubmed/36903009
http://dx.doi.org/10.3390/ma16051895

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