COI Ceramics Sylramic™ S300 Silicon Carbide Ceramic Matrix Composite, SiC

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COI Ceramics Sylramic™ S300 Silicon Carbide Ceramic Matrix Composite, SiC
Categories:	Ceramic; Carbide; Ceramic Matrix Composite
Material Notes:	Engineered ceramic composite structures for a broad range of industries and applications. Reinforcing Fiber Flexibility: S300 - Sylramic SiC Preceramic Polymer Matrix Precursors: S300 - Crystalline (SiC + Si3N4) or SiC Physical Attributes: Dense Matrix (<5%), High Temperature Capability, Good Matrix Dominated Properties and Wear Resistance Typical Applications: Commercial Aviation Exhaust, Military Aircraft Propulsion Exhaust, Industrial Produced using the Polymer Impregnation & Pyrolysis (PIP) process. This versatile and robust process is well suited for the fabrication of complex components. The PIP process utilizes a combination of polymeric and ceramic processes, combining a variety of ceramic fibers, fillers and pre-ceramic polymer resins to produce engineered ceramic composite structures for a broad range of industries and applications. Process temperatures referenced in property table: T1< T2 < T3 < T4. Information from COI Ceramics, Inc.
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Available Properties

Tensile Stress at Strain, Process Temperature T4
Tensile Stress at Strain, Process Temperature T1
Tensile Stress at Strain, Process Temperature T2
Tensile Stress at Strain, Process Temperature T3
Tensile Stress at Strain, Process Temperature T4
Tensile Stress at Strain, Process Temperature T1
Tensile Stress at Strain, Process Temperature T2
Tensile Stress at Strain, Process Temperature T3
Tensile Stress at Strain, Process Temperature T4
Tensile Stress at Strain, Process Temperature T1
Tensile Stress at Strain, Process Temperature T2
Tensile Stress at Strain, Process Temperature T3
Tensile Stress at Strain, Process Temperature T4
Tensile Stress at Strain, Process Temperature T1
Tensile Stress at Strain, Process Temperature T2
Tensile Stress at Strain, Process Temperature T3

Property Data

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