Carbon Fiber Plate - Twill Weave - Standard Modulus - Gloss / Matte - 24" x 24" x 7/64"
Carbon Fiber Plate - Twill Weave - Standard Modulus - Gloss / Matte - 24" x 24" x 7/64"
1
-
19
$287.99
20
+
$273.79
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.
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 4 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 | 0.115000 |
| Plate / Panel Size | 24" x 24" / 609.6mm x 609.6mm |
| Width | 24.0 |
| Thickness | 0.115 |
| Length | 24 |
| Length (max continuous) | 24.0 |
| Areal Density | 0.911 |
| Volumetric Density | 0.055 |
| Weight | 3.643 |
| 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 | 10618.0 |
| 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
404-22 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.