Coupled ablation and thermal behavior of an all-composite structurally integrated thermal protection system: Fabrication and modeling

2020 ◽  
Vol 251 ◽  
pp. 112623 ◽  
Author(s):  
Shengbo Shi ◽  
Yifan Wang ◽  
Li Yan ◽  
Peijie Sun ◽  
Maoyuan Li ◽  
...  
AIAA Journal ◽  
2010 ◽  
Vol 48 (1) ◽  
pp. 119-128 ◽  
Author(s):  
Oscar A. Martinez ◽  
Anurag Sharma ◽  
Bhavani V. Sankar ◽  
Raphael T. Haftka ◽  
Max L. Blosser

2009 ◽  
Vol 46 (3) ◽  
pp. 501-513 ◽  
Author(s):  
Christian Gogu ◽  
Satish K. Bapanapalli ◽  
Raphael T. Haftka ◽  
Bhavani V. Sankar

Author(s):  
D. I. Aronov ◽  
V. V. Klyagin

On the basis of analytical and experimental data, this paper presents possible levels of thermal loading of reusable hypersonic aircrafts. Methods for ensuring the thermal regime of such aircrafts using various passive and active thermal protection technologies are considered. The conducted analysis of the scientific and technical background in terms of the practical implementation of these technologies allowed the authors to draw the conclusion about the relevance and expediency of creating an integrated thermal protection system for reusable high-speed aircrafts.


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