Author:
Helber Bernd,Chazot Olivier,Hubin Annick,Magin Thierry E.
Funder
Mersen Scotland Holytown Ltd.
Agency for Innovation by Science and Technology
European Research Council
Subject
Mechanics of Materials,Ceramics and Composites
Reference56 articles.
1. The initial development of ablation heat protection: an historical perspective;Sutton;J Spacecraft Rock,1982
2. Degradation behaviour of a composite material for thermal protection systems Part I – experimental characterization;Torre;J Mater Sci,1998
3. Laub B, Venkatapathy E. Thermal protection system technology and facility needs for demanding future planetary missions. In: International workshop on planetary probe atmospheric entry and descent trajectory analysis and science, Lisbon (Portugal), ESA SP-544; October, 2003. p. 239–47.
4. Duffa G. Ablative thermal protection systems modeling. AIAA Education Series; 2013.
5. Tran HK. Development of lightweight ceramic ablators and arc jet test results. Tech Rep TM-108798. NASA Ames Research Center; 1994.
Cited by
58 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献