1. C. Bouquet, P. Soyris, A. Lacombe, S. Cueille, Overview of the current thermal protection technologies and orientation of performance improvements to satisfy RLV needs, Structures and Technologies: Challenges for Future Launchers, Snecma Moteurs, Strasbourg, France, 11–14 December, 2001.
2. H. Copéret, P. Soyris, M. Lacoste, J. Garnett, D. Tidwell, MMOD testing of C–SiC based rigid external insulation of the X-38/CRV thermal protection system, in: Proceedings of the 53rd International Astronautical Congress, The World Space Congress, Snecma Propulsion Solide and Lockheed Martin Astronautics, Houston, TX, USA, 10–19 October, 2002.
3. F. Leleu, P. Watillon, J. Moulin, A. Lacombe, P. Soyris, The thermo-mechanical architecture and TPS configuration of the Pre-X vehicle, in: Proceedings of the 53rd International Astronautical Congress, The World Space Congress, EADS-LV and Snecma Propulsion Solide, Houston, TX, USA, 10–19 October, 2002.
4. T. Salmon, F. Leleu, J. Moulin, P. Tran, Experimentation plan for thermal protections and hot structures on pre-X: current status, in: Proceedings of the Fourth European Workshop on Hot Structures and Thermal Protection Systems for Space Vehicles, EADS-LV, Palermo, Italy, 26–29 November, 2002.
5. P. Soyris, A. Foucault, J.M. Parenteau, T. Pichon, C/SiC based rigid external thermal protection system for future reusable launch vehicles: generic shingle, pre-X/FLPP anticipated development test studies, in: Y. Prel, S. Guédron (Eds.), Proceedings of the 13th International Space Planes and Hypersonic Systems and Technologies Conference, Snecma Propulsion Solide, CNES, Capua, Italy, 16–20 May, 2005.