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Thermo-mechanical performance of an ablative/ceramic composite hybrid thermal protection structure for re-entry applications

  • Published:2015-12 Issue: Volume:82 Page:159-165
  • ISSN:1359-8368
  • Container-title:Composites Part B: Engineering
  • language:en
  • Short-container-title:Composites Part B: Engineering

Author:

Triantou K.,Mergia K.,Florez S.,Perez B.ORCID,Barcena J.,Rotärmel W.,Pinaud G.,Fischer W.P.P.

Funder

European Commission

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

Reference18 articles.

1. European atmospheric re-entry activities status and perspectives;Caporicci,2011

2. TPS architecture on ARV;Salmon,2011

3. Ongoing European developments on entry heatshields and TPS materials;Ritter,2011

4. FP7/space project “HYDRA” hybrid ablative development for re-entry in planetary atmospheric thermal protection;Barcena,2013

5. Novel hybrid ablative/ceramic heatshield for earth atmospheric re-entry;Barcena,2014
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