30th International Symposium on Shock Waves 1 2017
DOI: 10.1007/978-3-319-46213-4_107
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Surface Oxidation Study of ZrB2–SiC Composite for Re-entry Applications Using Free Piston-Driven Shock Tube

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“…18 In another earlier study, Jayaram et al carried out shock tube experiments in oxygen environment with hot pressed ZrB 2 -SiC-MoSi 2 composite and observed the formation of zirconium dioxide and silicon dioxide. 19 Likewise, Monteverde et al reported the oxidation and thermal shock resistance of ZrB 2 -based UHTC under the dissociated flow, simulating the aerothermal heating in hypersonic re-entry conditions and reported the formation of a protective SiO 2 layer at a test temperature of ∼2100 K. This improves the oxidation resistance and thermomechanical properties. 20 In the case of hot pressed and spark plasma sintered TiB 2 -based ceramics, surface oxidation is reported as a result of shock wave exposure.…”
Section: Introductionmentioning
confidence: 97%
“…18 In another earlier study, Jayaram et al carried out shock tube experiments in oxygen environment with hot pressed ZrB 2 -SiC-MoSi 2 composite and observed the formation of zirconium dioxide and silicon dioxide. 19 Likewise, Monteverde et al reported the oxidation and thermal shock resistance of ZrB 2 -based UHTC under the dissociated flow, simulating the aerothermal heating in hypersonic re-entry conditions and reported the formation of a protective SiO 2 layer at a test temperature of ∼2100 K. This improves the oxidation resistance and thermomechanical properties. 20 In the case of hot pressed and spark plasma sintered TiB 2 -based ceramics, surface oxidation is reported as a result of shock wave exposure.…”
Section: Introductionmentioning
confidence: 97%