Two types of low-density carbon/carbon preforms which had different fiber v
olume fractions and fiber orientations, i.e., a carbon woven fabric (approx
imate to 55 vol%)/carbon and a chopped carbon fiber (approximate to 40 vol%
) /carbon composites, were reaction-bonded with a silicon melt at 1750 degr
ees C in vacuum to fabricate dense carbon fiber/Si/SiC composites. The reac
tion-bonding process increased the density to similar to 2.1 g/cm(3) from 1
.6 and 1.15 g/cm(3) for carbon woven and chopped carbon preforms, respectiv
ely. All of the composites fractured with extensive fiber pullout. The high
er the density, the higher the stiffness and proportional limit stress. The
carbon woven fabric/Si/SiC composites with a density of 2.06 g/cm(3) exhib
ited a similar to 120 MPa ultimate strength and a similar to 80 MPa proport
ional limit in bending test.