The oxidation behaviour of a 2.5D multi-layered ceramic-matrix composite (S
iC)(f)/C/(SiBC)(m) was investigated in a dry atmosphere O-2 (20 Vo1.%) CO2
(5 vol.%) He and in the presence of water vapour H2O (2.3 vol.%). The matri
x denoted (SIBC)(m) is constituted of three phases: silicon carbide, boron
carbide and a SiBC phase. The aim of boron incorporation is to improve the
oxidation resistance of the composite by boron oxide or borosilicate format
ion. The transformations were followed by thermogravimetry during isotherma
l experiments of 20 h exposure in the range 600-1200 degreesC and the chang
es of the specific area of the samples were measured by krypton adsorption
at 77 K. The results of this study show that effective protection occurs in
the range 650-900 degreesC and is mainly related to the oxidation of boron
carbide. At higher temperatures, boron oxide is no longer protective becau
se of its volatilisation and consumption by reaction with water vapour. How
ever, the two other constituents of the matrix, SiC and SiBC, lead to self-
healing behaviour by both borosilicate and silica formation. (C) 2001 Publi
shed by Elsevier Science Ltd. Ail rights reserved.