Novel Hybrid Ablative/Ceramic Layered Composite for Earth Re-entry Thermal Protection: Microstructural and Mechanical Performance

Author:

Triantou K.,Mergia K.,Marinou A.,Vekinis G.,Barcena J.,Florez S.,Perez B.,Pinaud G.,Bouilly J.-M.,Fischer W. P. P.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference14 articles.

1. M. Caporicci, European Atmospheric Re-entry Activities Status and Perspectives”, 3rd International ARA Days, May 2-4, 2011 (Arcachon, France)

2. T. Salmon, X. Vo and M. Bottacini, TPS Architecture on ARV, 7 th European Symposium on Aerothermodynamics, L. Ouwehand, Ed., 2011 (Noordwijk, Netherlands) European Space Agency, id. 120

3. H. Ritter, O. Bayle, Y. Mignot, E. Boulier, J.-M. Bouilly, P. Portela, and R. Sharda, Ongoing European Developments on Entry Heatshields and TPS Materials, 8th International Planetary Probe Workshop, June 6-10, 2011 (Portsmuth, Virginia, USA)

4. G. Vekinis and G. Xanthopoulou, A Hybrid Ceramic—Polymer Composite TPS for Multiple Atmospheric Entry Probes, 3rd International Planetary Probe Workshop, June 27–July 1, 2005 (Anavyssos, Greece)

5. G. Vekinis, Hybrid TPS: A Feasibility and Use Study of a Novel Hybrid Ceramic-Ablator TPS for Probes, ESA/ESTEC-ITI 19981, Final Report, Dec 2007, ESA/ESTEC

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