Carbon Fiber Plate - Twill Weave - Standard Modulus - Gloss / Matte - 12" x 6" x 3/32"
Carbon Fiber Plate - Twill Weave - Standard Modulus - Gloss / Matte - 12" x 6" x 3/32"
$46.99
Estimated lead time for quantities greater than what is Available Now is expected to be between 2 and 4 weeks.
Click to view and choose plate sizes available
Quick Facts for our Resin Infused Carbon Fiber Gloss/Matte Plate
- Top side near glass reflective gloss surface
- Bottom side matte textured surface
- Comprised of 3 plies of 670 GSM 12k twill fabric.
- 0.052 lbs / in^3 OR 1.45 grams / cm^3
- Ready for machining or waterjet cutting
- Minimal to zero fatigue failures
- Structurally sound and cosmetically stunning
- Ideal for RC models including multi-rotor airframes
- Glass Transition Temperature (Tg) is 194°F
- Shore D hardness ~90D
Manufactured using resin infusion to achieve near perfection, porous free laminates!
Special Return Policy - Blowout/Blemished
Rock West Composites will NOT return or refund blowout or blemished items. This applies to all materials listed as a -blowout or a -blem.
Additional Information
| Application | Multi-Rotor / Drone / UAV |
|---|---|
| Materials | Standard Modulus Carbon |
| Pattern | 3k 2X2 Twill Weave |
| Color | Black |
| Finish | Gloss / Matte |
| Panel Thickness | 0.090000 |
| Plate / Panel Size | 6" x 12" / 152.4mm x 304.8mm |
| Width | 6.0 |
| Thickness | 0.09 |
| Length | 12 |
| Length (max continuous) | 12.0 |
| Areal Density | 0.713 |
| Volumetric Density | 0.055 |
| Weight | 0.356 |
| 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 | 10614.0 |
| 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
403-612 Rev NC
| 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.