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Design and verification of the TPS of the circumlunar free return and reentry flight vehicle for the 3rd phase of Chinese lunar exploration program
The thermal protection system (TPS) of the high speed reentry vehicle is confronted with sever challenges, for the reentry environment has the characteristics such as high enthapy, twice rentry, the coupling of high heat flux and long time heating. This paper brings forward a design of the TPS, develops a …