1. Glass D. E., Ceramic Matrix Composite (CMC) Thermal Protection Systems (TPS) and Hot Structures for Hypersonic Vehicles, Proc. of 15th AIAA Space Planes and Hypersonic Systems and Technologies Conference, Dayton, OH, USA, 2008.
2. Pichon T., Barreteau R., Thermal Protections Systems : Heritage – Development Status – Perspectives, Proc. of 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, Tours, France, 2012.
3. Lange H., et al., Advanced CMC TPS Design Concepts for Re-usable Re-entry Vehicles, Proc. of 5th European Workshop on thermal Protection System and Hot Structures, Noordwijk, The Netherland, 2006.
4. Pichon T., et al., C/SiC based Rigid External Thermal Protection System for Future Reusable Launch Vehicles: Generic Shingle, Pre-X/FLPP Anticipated Development Test Studies, Proc. of 5th European Workshop on thermal Protection System and Hot Structures, Noordwijk, The Netherland, 2006.
5. Brach Prever E., et al., TPS Design, Development and Verification Approach for IXV Program, Proc. of 7th European Workshop on thermal Protection System and Hot Structures, Noordwijk, The Netherland, 2013.