Carbon Fiber Plate - QISO Tri-Axial - Standard Modulus - Gloss / Matte - 24" x 24" x 3/64"
Carbon Fiber Plate - QISO Tri-Axial - Standard Modulus - Gloss / Matte - 24" x 24" x 3/64"
1
-
19
$194.99
20
+
$193.79
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
Each layer of QISO® quasi-isotropic fabric is a balanced braid with fibers running 0°, + 60° and -60°. In this configuration, our QISO plate will exhibit similar properties in all directions of the laminate. A thicker laminate is not needed with QISO, so we offer it in a two-ply layup. Stronger, lighter and more efficient, QISO® enables superior performance when loads come from multiple directions.
Additional Information
| Application | Multi-Rotor / Drone / UAV |
|---|---|
| Materials | Standard Modulus Carbon |
| Pattern | Tri-Axial Weave |
| Color | Black |
| Finish | Gloss / Matte |
| Panel Thickness | 0.050000 |
| Plate / Panel Size | 24" x 24" / 609.6mm x 609.6mm |
| Width | 24.0 |
| Thickness | 0.05 |
| Length | 24 |
| Length (max continuous) | 24.0 |
| Areal Density | 0.396 |
| Volumetric Density | 0.055 |
| Weight | 1.584 |
| Primary Fiber | Hexcel AS4 |
| 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 | 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 | 30442.0 |
| 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
202-22 Rev C
| Ply # | Orientation (degrees) | Location |
|---|---|---|
| 1 | All 0/60/-60 (Triaxial) | 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.