Two-dimensional C/SiC composites have attracted increasing interests in recent years due to their low densities, high specific strengths, 1 elevated specific module, 2 and noncatastrophic mode of failure, 3 which made them promising thermal structural materials for applications in aerospace, aircraft braking, and space detection. 1,4,5 However, these harsh environments require them possessing not only thermal structural performances like load resistance, 2 but also functional properties such as high thermal conductivity, especially in thickness direction of the composites (about 5-12 W•m −1 •K −1 for now). 6-9 Therefore, C/SiC composites cannot serve as a functional materials for aerospace vehicle thermal discharge