Study on Impact Resistance of C/SiC Ceramic Matrix Composites for Thermal Protection of the Aerospace Vehicle

Table 3

Maximum tensile load and tensile strength.

	Impact energy	The average maximum tensile load	The average tensile strength	The percentage of residual strength
Nondestructive	0	37.60	273.78	100
Impact	10	24.18	186.57	68.17
	12	18.45	140.90	51.46