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Published in 2020 at "Journal of Thermal Analysis and Calorimetry"
DOI: 10.1007/s10973-020-10343-4
Abstract: During the ballistic atmospheric re-entry, a space vehicle has to withstand huge thermo-mechanical solicitations because of its high velocity and the friction with the atmosphere. According to the kind of the re-entry mission, the heat…
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Keywords:
carbon phenolic;
zro2;
phenolic ablators;
nano zro2 ... See more keywords