Due to its excellent mechanical properties, favorable damage tolerance and comparatively low density, continuous carbon fiber reinforced carbon silicon carbide (C/C-SiC) composite fabricated by Liquid Silicon Infiltration (LSI) process has been successfully used in aerospace, energy, and transport technology. [1][2][3][4][5][6][7][8] The preliminary investigation of siliconization in German Aerospace Center Stuttgart started in the late 1980s and the manufacturing process of LSI-based C/C-SiC was developed in the beginning of 2000s. 9 Since then, material properties of the composite have been characterized intensively. The in-plane and out-of-plane mechanical properties under different loads, thermal properties and the effect of high temperature were investigated and summarized in Ref. [10] The strength ratio between bending and tensile load was approx. 1.7-2.0 depending on the different loading directions. 11 The acoustic emission (AE) technique has been used for the determining the relationship between its tensile strength and damage-related AE energy. 12 Based on the statistical analysis, strength values under tensile, compression and bending loads can be described using normal or Weibull