Development of MoSi<sub>2</sub>-SiC Component for Satellite Launch Vehicle

<table>XRD pattern of MoSi<sub>2</sub>-SiC composite specimen, vacuum hot pressed at (a) 1500°C and (b) 1600°C.</table>

International Scholarly Research Notices

Figure 6: Development of MoSi<sub>2</sub>-SiC Component for Satellite Launch Vehicle 