Ablation and Thermal Response Property Model Validation for Phenolic Impregnated Carbon Ablator
By F. Milos, Yih-Kanq Chen. 2009
192 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Applied Mathematics, Materials Chemistry
View Paper: https://www.semanticscholar.org/paper/af969a56d531a2f7046a4cbd6b2557e66f732ced
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In Aerospace Engineering
In Materials Chemistry
Citations in the corpus
- Graphene NanoPlatelets reinforced tantalum carbide consolidated by spark plasma sintering (2013, background): “Hypersonic spacecraft such as Apollo Orbiters and Space Shuttles used ablative materials such as Phenolic Impregnated Carbon Ablator (PICA) [16] which could withstand the high temperatures for a few hundred seconds.”