2017
DOI: 10.1134/s107042721707014x
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Functionally graded ceramic material prepared by spark plasma sintering (SPS)

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Cited by 3 publications
(3 citation statements)
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“…To reduce the density of ultra-high-temperature ceramics (UHTC) for aerospace applications, Kachaev et al [28] fabricated FGCMs with a gradient transition from a UHTC side to a ceramic of lower density. The high-temperature side of the five-layered FGCM was a composite of HfB 2 + SiC, while the low-density side was SiC with 7 wt-% oxide additives (Al 2 O 3 + Y 2 O 3 ).…”
Section: Ceramic-ceramicmentioning
confidence: 99%
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“…To reduce the density of ultra-high-temperature ceramics (UHTC) for aerospace applications, Kachaev et al [28] fabricated FGCMs with a gradient transition from a UHTC side to a ceramic of lower density. The high-temperature side of the five-layered FGCM was a composite of HfB 2 + SiC, while the low-density side was SiC with 7 wt-% oxide additives (Al 2 O 3 + Y 2 O 3 ).…”
Section: Ceramic-ceramicmentioning
confidence: 99%
“…Hypersonic and Supersonic jets generally experience aerodynamic drag and hence are subjected to extreme heat fluxes at their surfaces and therefore these spacecraft components should be able to sustain in ultra-high temperatures over 2000°C and extremely harsh and oxidizing atmospheres. Spark plasma sintered FGCMs such as SiC-HfB 2 [28], ZrB 2 -SiC-CNT [33], Cu-Al 2 O 3 [150] , ZrB 2 -ZrO 2 [263] have shown excellent thermo-mechanical characteristics, with reduced thermal residual stresses and absence of any delaminations or cracks across the sample cross-sections under highly oxidizing atmospheres. These make them very promising candidates for spacecraft body components such as nose covers, engine parts, heat exchange plates, turbine blades, etc.…”
Section: Application Of Fgcmsmentioning
confidence: 99%
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