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Tensile behavior and microstructural evolution of a carbon/silicon carbide composite in simulated re-entry environments

✍ Scribed by Yani Zhang; Litong Zhang; Laifei Cheng; Yongdong Xu


Publisher
Elsevier Science
Year
2008
Tongue
English
Weight
1000 KB
Volume
473
Category
Article
ISSN
0921-5093

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✦ Synopsis


Carbon fiber reinforced silicon carbide matrix composites with a protective coating were prepared by chemical vapor infiltration. Their tensile strength was about 240-250 MPa at room temperature, and 330-390 MPa in vacuum. Tensile behavior in a simulated re-entry environment was studied and compared with that in vacuum. The microstructural evolution on tensile fracture surfaces were investigated by scanning electron microscopy, and an oxidation damage pattern of fibers on tensile fracture surface was presented and discussed. A significant strength reduction was observed in re-entry environments due to the interaction of load, high temperature, and oxidation. The non-uniform oxidation of fibers weakened the load-carrying ability due to decreasing effective loaded area and hence strength. Finally, a minimum diameter of total fiber cluster embedded in composites is suggested about 220 m for use under high load in re-entry environments at 1800 • C.


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✍ Hui Mei; Laifei Cheng; Qingqing Ke; Litong Zhang 📂 Article 📅 2010 🏛 Elsevier Science 🌐 English ⚖ 616 KB

The tensile properties and oxidation behavior of 2D C/SiC bolts prepared by chemical vapor infiltration were investigated in a simulated re-entry environment. The results showed that all the tensile streng\ths of 2D C/SiC bolts at test temperatures of 1300, 1600 and 1800 °C decreased, respectively,