These components can withstand temperatures ranging from 1000°C to 2000°C, typical of re-entry from space missions, hypersonic flight, and propulsion systems. CMC and UHTCMC enable the design of lightweight, rigid structures with significantly better damage tolerance compared to conventional ceramics. For such reasons they can be considered a key enabling technology for the development of reusable spacecraft.
The Italian Space Agency funded AM3aC2A, which brought together a significant partnership including the Department of Aerospace Science and Technology (DAER) at the Politecnico di Milano - the project leader - CIRA (Italian Aerospace Research Centre), ISSMC (Institute of Science, Technology, and Sustainability for Ceramic Materials Development of CNR), and Petroceramics S.p.A, a leader in ceramic matrix composite research and development. Together, they produced, characterized, modelled, and tested a significant number of specimens and structural elements in relevant environments, by exploiting specific facilities at the laboratories of CIRA and the University Federico II of Naples.

