Silicon carbide composites with carbon interfaces have been analyzed b
y thermal gravimetric analysis (TGA) in O-2 and H-2 environments to pr
edict their performance as structural materials in fusion applications
. Conditions for testing included temperatures between 800 and 1200 de
grees C, O-2 concentrations ranging from 100 to 1500 ppm, and H-2 conc
entrations of 0.1 and 1%. Weight losses observed by TGA were determine
d to be primarily due to the oxidation of the carbon interface. Linear
-parabolic kinetics governed the interfacial oxidation for all of the
conditions in O-2. By focusing on the linear region, a simple model es
timated the linear rate dependency on O-2 partial pressure to be on th
e order of 0.911. Weight loss data in H-2 environments yielded activat
ion energies of 18 and 34 kcal/mol for 0.1 and 1%, respectively. The w
eight loss rates in H-2 were 6 to 26 times slower than rates in O-2, w
hen approximations were made assuming linear kinetics.