Ultra High Temperature Composites For Thermal Protection Systems

The objective of this proposed project is to develop a low-cost nanostructured hybrid composites TPS. The proposed new TPS system will consist of porous skeleton based on polymer derived ceramic (PDC) matrix composites and nano-modified ablator (nano-modified phenolic or cyanate ester). Extensive ground-based testing on the composites TPS will be conducted at UCF and FSU FCAAP.


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Filing Info

  • Accession Number: 01678209
  • Record Type: Research project
  • Source Agency: Federal Aviation Administration Center of Excellence for Commercial Space Transportation
  • Files: RIP, USDOT
  • Created Date: Aug 22 2018 1:02PM