Silicon oxycarbide coatings are applied to graphite fibers by dip coat
ing tows of fibers into hexane solutions of the silsesquioxane terpoly
mer MeHSiO](0.1)[MeSi(OnPr)O](0.2)[MeSi(O)(1.5)](0.7)- to form silsesq
uioxane coatings typically 0.1 mu m thick. The coatings are then pretr
eated by heating in N-2 to selected temperatures (200 degrees C increm
ents to 1000 degrees C). The amorphous polymeric coatings were shown t
o convert to amorphous silicon oxycarbide coatings on heating to tempe
ratures above 600 degrees C. Single carbon fibers coated with silicon
oxycarbide coatings were pyrolyzed and then encapsulated in a transpar
ent epoxy matrix so that stress could be applied and the adhesion and
fracture behavior of the coatings could be observed. The properties an
d adhesion of the coatings to the carbon fibers change with the degree
of pyrolysis. Initially the adhesion is low and interfacial failure i
s observed. After thermal processing to 800 degrees C and above a sign
ificant increase in adhesion is detected but the failure mode remains
interfacial and circumferential cracks in the coating are detected. A
non-linear axisymmetric finite element model of this single fiber coat
ed with material having properties varying in a manner similar to the
coating was used to gain insight into observed changes.