Carbon Fiber Plate - Twill Weave - Standard Modulus - Matte - 48" x 48" x 13/64"
Carbon Fiber Plate - Twill Weave - Standard Modulus - Matte - 48" x 48" x 13/64"
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$1,528.99
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$1,452.79
Estimated lead time for quantities greater than what is Available Now is expected to be between 2 and 4 weeks.
If there is an Available Now quantity listed above, it indicates our quantity in stock. Orders placed today for this quantity or less are expected to ship the next business day.
This plate is fabricated via resin infusion and deploys a T700 (or equivalent) carbon fiber. In addition to being stiffer than aluminum carbon fiber plate this thicker version can be machined quite easily and shaped to yield a very interesting aesthetic often seen in knife handles or other products. Other manufacturers have dubbed this plate or ones similar "Artisan". Both sides have a peel ply finish which is matte / textured by default and with a quick cleaning can be bond ready.
Additional Information
| Application | Tooling Plates / Support Structures |
|---|---|
| Materials | Standard Modulus Carbon |
| Pattern | 3k 2X2 Twill Weave |
| Color | Black |
| Finish | Matte / Matte |
| Panel Thickness | 0.210000 |
| Plate / Panel Size | 48" x 48" / 1219.2mm x 1219.2mm |
| Width | 48.0 |
| Thickness | 0.21 |
| Length | 48 |
| Length (max continuous) | 48.0 |
| Areal Density | 1.663 |
| Volumetric Density | 0.055 |
| Weight | 26.611 |
| Primary Fiber | Toray T700S |
| Primary Resin / Hardener | Rhino 1411/4111 |
Engineering Properties
All laminate properties and mechanical calculations are based on Classical Lamination Theory and should be used as a reference only. Rock West Composites does not guarantee these properties or calculations.
| Avg EX Young's Modulus | 9300000.0 |
|---|---|
| Avg EY Young's Modulus | 9300000.0 |
| GXY Shear Modulus | 600000.0 |
| X Tensile Yield Strength | 103000.0 |
| X Compressive Yield Strength | 89000.0 |
| Y Tensile Yield Strength | 103000.0 |
| Y Compressive Yield Strength | 89000.0 |
| XY Shear Strength | 10625.0 |
| CTEX | 2.00E-06 |
| CTEY | 2.00E-06 |
| Poisson's Ratio vXY | 0.035 |
| Poisson's Ratio vYX | 0.035 |
Note:
- "X" is along the length of a tube, rod, plate, or panel.
- "Y" is around the perimeter of a tube, perpendicular to the length of pultruded parts, or along the width of a plate or panel.
Layup Orientation
408-44 Rev A
| Ply # | Orientation (degrees) | Location |
|---|---|---|
| 1 | All 0/90 | Inside |
- 0° fibers maximize bending stiffness and run along the length of the part. Consider bending a tube over your knee.
- 45° fibers maximize torsional stiffness and are typically plied together in an opposing manner, i.e. ±45°. Consider twisting a tube like a vehicle's driveshaft.
- 90° (or "hoop") fibers maximize crushing stiffness and generally assist in overall durability. Consider laying a tube on the ground and stepping on it.