Plate - Carbon Fiber - QISO Tri-Axial - Gloss/Matte - 24 x 48 x 0.050" / 1.2mm thick
Discontinuing This Length x Width Option ◾ 24" x 48" ◾ 609mm x 1219mm
1
-
10
$321.99
11
-
49
$297.79
50
+
$272.59
Estimated lead time for quantities greater than what is Available Now is expected to be between 2 and 4 weeks.
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 | 0.05 |
| Plate / Panel Size | 24" x 48" / 609.6mm x 1219.2mm |
| Width | 24.0 |
| Thickness | 0.05 |
| Length | 48 |
| Length (max continuous) | 48.0 |
| Areal Density | 0.396 |
| Volumetric Density | 0.055 |
| Weight | 3.168 |
| Primary Fiber | Hexcel AS4 |
| Primary Resin / Hardener | Rhino 1411/4111 |
| 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 | 30441.0 |
| 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
202-24 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.