2018
DOI: 10.1016/j.actamat.2018.03.042
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Understanding the oxidation behavior of a ZrB2–MoSi2 composite at ultra-high temperatures

Abstract: This basic research investigates the microstructure evolution of a composite based on ZrB 2-MoSi 2 from the as-sintered features to the changes occurring upon oxidation at ultra-high temperatures, 1650 and 1800°C, in a bottom-up loading furnace for 15 minutes. Scanning and transmission electron microscopy evidenced the formation of a matrix typified by ZrB 2-cores surrounded by (Zr,Mo)B 2-rims with dispersed MoSi 2 particles and SiO 2 glass trapped at the triple junctions. The oxidation at 1650°C induced the m… Show more

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Cited by 103 publications
(47 citation statements)
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“…For the silicide-containing composites, independent of the MeSi 2 used, the original ZrB 2 grains of the matrix were surrounded by a solid solution with general formula (Zr,Me)B 2 , in agreement with previous studies [25,27,28] and as a consequence of the densification process involving a transient liquid phase formed by partial dissociation of the silicide [25]. This feature is particularly visible in ZBH, Figure 2c, owing to a higher amount of Me, in this case Hf, being dissolved in the ZrB 2 lattice.…”
Section: Microstructure and Properties Of As-sintered Materialssupporting
confidence: 89%
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“…For the silicide-containing composites, independent of the MeSi 2 used, the original ZrB 2 grains of the matrix were surrounded by a solid solution with general formula (Zr,Me)B 2 , in agreement with previous studies [25,27,28] and as a consequence of the densification process involving a transient liquid phase formed by partial dissociation of the silicide [25]. This feature is particularly visible in ZBH, Figure 2c, owing to a higher amount of Me, in this case Hf, being dissolved in the ZrB 2 lattice.…”
Section: Microstructure and Properties Of As-sintered Materialssupporting
confidence: 89%
“…For the materials containing MeSi 2 , the (Zr,Me)B 2 solid solutions of the matrices oxidized following the typical oxidation behavior recently outlined in dedicated studies [27,28]…”
Section: Microstructure Of Oxidized Composites and Evolution Mechanismmentioning
confidence: 99%
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“…The pursuit of commercial hypersonic flights and space travel for the mission to Mars relies on innovative reusable materials with improved thermal protection systems (TPS) . Candidate materials must survive harsh conditions, especially those found upon atmospheric reentry with dissociative oxidation at surfaces, extreme heat fluxes, temperatures soaring over 3000°C and vibrational and stagnation pressure loads, in key components of the hypersonic vehicles and aircrafts . These key components are traditionally leading edges, combustors and insulation components .…”
Section: Introductionmentioning
confidence: 99%