2010
DOI: 10.1016/j.actaastro.2009.08.008
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Microstructure and evolution of iridium coating on the C/C composites ablated by oxyacetylene torch

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Cited by 39 publications
(12 citation statements)
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“…However, since Ir exceeds its ductile/brittle transition temperature (760°C [35]), it will become plastic and deform under the compressive stress, resulting in a rumpled Ir coating [ Fig. 7bB], which was reported by other researchers [10,13]. The stress relaxation of the Ir coating may occur at 1800°C following Path B-C in Fig.…”
Section: Characterizationmentioning
confidence: 93%
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“…However, since Ir exceeds its ductile/brittle transition temperature (760°C [35]), it will become plastic and deform under the compressive stress, resulting in a rumpled Ir coating [ Fig. 7bB], which was reported by other researchers [10,13]. The stress relaxation of the Ir coating may occur at 1800°C following Path B-C in Fig.…”
Section: Characterizationmentioning
confidence: 93%
“…6d, e, located mainly along the grain boundaries and at the grain boundary junctions. The formation of the voids could be owing to the migration and aggregation of the inner microvoids in Ir coating at high temperatures [10].…”
Section: Characterizationmentioning
confidence: 99%
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“…It is thus one of the most promising candidates for protective coating of either structural carbons or Re-based components for extreme environments. 2,17,18 Iridium-coated Re nozzles are used in aerospace applications for small chemical rockets and resistojet thrusters. 19 A combustion chamber composed of Re substrate and Ir coating has been demonstrated to be stable for extended lifetimes at temperatures as high as 2,200 • C. 20,21 NASA has reported the development of Ircoated Re rocket chamber technology, allowing an increase in satellite life from 12 to 15 years, and gaining 30-60 M$ in the added revenue per satellite.…”
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confidence: 99%