The Thermal and Thermo-Mechanical Properties of Carbon Composite Laminate
Carbon Composite raw material property comparison are summarized below:
-Thermal Conductivity – Watts per meter ? Kelvin.
The core material can spread up to 620.0 W/m?K.
-CTE – parts per million per C.
Carbon Composite Laminate has a very low negative CTE,(-1.10 ppm/C) so it contracts very slightly as temperature rises.
Traditional materials expand considerably as temperature rises. When in plane,the user can tailor the surface CTE of a
standard Printed Circuit Board from 3ppm/C to 12 ppm/C,enabling direct die attach and WLP.
-Density – grams per cubic centimeter.
The material density (and therefore weight) is approximately equivalent to fiberglass. Standard FR4 is 1.85g/cm3 carbon
composite is 1.76-2.20g/cm3. No weight premium.
-Tensile modulus of elasticity – MSI (1,000,000 PSI).
The carbon composite is much more rigid than traditional materials. It is 4 to 10 times the rigidity of standard Fr4. Tensile
modulus is 34-130 MSI per layer depending on raw material selected.
-Dielectric constant – r (relative permittivity).
The relative permittivity of the new material is higher than traditional material,however,it is used only as a plane layer
(preferably ground plane) and is isolated from the copper vias. This material can be drilled through easily so that signals pass
through the carbon composite layer,are isolated,and still can be used throughout the entire board. This eliminates the
concerns of the Dielectric constant of the core material and allows users to simply design the PCB as normal concerning
vias.