Carbon Fiber Plate - Quasi-Iso - Standard Modulus - Matte - 48" x 48" x 1/4"
Carbon Fiber Plate - Quasi-Iso - Standard Modulus - Matte - 48" x 48" x 1/4"
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$2,027.99
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$1,926.79
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 Quasi-Iso Resin Infused Carbon Fiber Matte/Matte Plate
- Quasi-isotropic layup
- Both sides are a matte textured surface
- 0.055 lbs / in^3 OR 1.52 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
| Materials | Standard Modulus Carbon |
|---|---|
| Pattern | 3k 2X2 Twill Weave |
| Color | Black |
| Finish | Matte / Matte |
| Panel Thickness | 0.250000 |
| Plate / Panel Size | 48" x 48" / 1219.2mm x 1219.2mm |
| Width | 48.0 |
| Thickness | 0.25 |
| Length | 48 |
| Length (max continuous) | 48.0 |
| Areal Density | 1.98 |
| Volumetric Density | 0.055 |
| Weight | 31.68 |
| Primary Fiber | Toray T700S |
| Primary Resin / Hardener | Rhino 1411/4111 |
| Temperature Rating (F) | 194.0 |
| Max Operating Temp- (Tg) | 175F to 199F |
| Resin / Chemistry / Polymer Type | Epoxy |
| HTS - Harmonized Tariff Code | 6815.13.0000 |
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 | 6664000.0 |
|---|---|
| Avg EY Young's Modulus | 6664000.0 |
| GXY Shear Modulus | 2546000.0 |
| X Tensile Yield Strength | 62320.0 |
| X Compressive Yield Strength | 55760.0 |
| Y Tensile Yield Strength | 62320.0 |
| Y Compressive Yield Strength | 55760.0 |
| XY Shear Strength | 30452.0 |
| CTEX | 2.00E-06 |
| CTEY | 2.00E-06 |
| Poisson's Ratio vXY | 0.309 |
| Poisson's Ratio vYX | 0.309 |
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
208-44 Rev NC
| Ply # | Orientation (degrees) | Location |
|---|---|---|
| 1 | 0/90 | Inside |
| 2 | ±45 | ↓ |
| 3 | ±45 | |
| 4 | 0/90 | |
| 5 | 0/90 | |
| 6 | 0/90 | |
| 7 | ±45 | |
| 8 | ±45 | |
| 9 | 0/90 | Outside |
- 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.