The toughness of ceramic matrix composites is contributed by crack bri
dging, matrix crack deflection, fiber debonding and pull-out and other
minor effects. Crack bridging relies on fibers being intact close to
the crack tip, while pull-out toughening relies on the debonding and f
rictional characteristics of the fiber-matrix interface. The interface
friction depends on the interface pressure (i.e., on misfit strains)
and interface roughness. In this paper, a calculational model for post
irradiation fiber debonding and pull-out toughness in SiC-SiC composit
es is presented. It is shown that fiber debonding and pull-out toughne
ss in SiC-SiC composites vary significantly with neutron fluence and i
rradiation temperature, which is a direct consequence of the dependenc
e of the misfit strain on these irradiation variables.