2 Layers of A&P's QISO® quasi-isotropic fabric. Each layer is a balanced braid with fibers running 0°, + 60° and -60°. In this configuration, laminate stiffness is mostly similar in any bending scenario. Stronger, lighter and more efficient, QISO® enables superior performance when loads come from multiple directions.
P/N | 202-11 | 202-12 | 202-22 | 202-44 | 202-410 | 202-24 |
---|---|---|---|---|---|---|
Application | Multi-Rotor / Drone / UAV | Multi-Rotor / Drone / UAV | Multi-Rotor / Drone / UAV | Multi-Rotor / Drone / UAV | Multi-Rotor / Drone / UAV | Multi-Rotor / Drone / UAV |
Materials | Standard Modulus Carbon | Standard Modulus Carbon | Standard Modulus Carbon | Standard Modulus Carbon | Standard Modulus Carbon | Standard Modulus Carbon |
Pattern | Tri-Axial Weave | Tri-Axial Weave | Tri-Axial Weave | Tri-Axial Weave | Tri-Axial Weave | Tri-Axial Weave |
Color | Black | Black | Black | Black | Black | Black |
Finish | Gloss / Matte | Gloss / Matte | Gloss / Matte | Gloss / Matte | Gloss / Matte | Gloss / Matte |
Panel Thickness | 0.050000 | 0.050000 | 0.050000 | 0.050000 | 0.050000 | 0.05 |
Plate / Panel Size | 12" x 12" / 304.8mm x 304.8 mm | 12" x 24" / 304.8mm x 609.6mm | 24" x 24" / 609.6mm x 609.6mm | 48" x 48" / 1219.2mm x 1219.2mm | 48" x 120" / 1219.2mm x 3048mm | 24" x 48" / 609.6mm x 1219.2mm |
Width | 12.0 | 12.0 | 24.0 | 48.0 | 48.0 | 24.0 |
Thickness | 0.05 | 0.05 | 0.05 | 0.05 | 0.05 | 0.05 |
Length | 12 | 24 | 24 | 48 | 120 | 48 |
Length (max continuous) | 12.0 | 24.0 | 24.0 | 48.0 | 120.0 | 48.0 |
Areal Density | 0.396 | 0.396 | 0.396 | 0.396 | 0.396 | 0.396 |
Volumetric Density | 0.055 | 0.055 | 0.055 | 0.055 | 0.055 | 0.055 |
Weight | 0.396 | 0.792 | 1.584 | 6.336 | 15.84 | 3.168 |
Primary Fiber | Hexcel AS4 | Hexcel AS4 | Hexcel AS4 | Hexcel AS4 | Hexcel AS4 | Hexcel AS4 |
Primary Resin / Hardener | Rhino 1411/4111 | Rhino 1411/4111 | Rhino 1411/4111 | Rhino 1411/4111 | Rhino 1411/4111 | Rhino 1411/4111 |
HTS - Harmonized Tariff Code | 6815.13.0000 |
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.
P/N | 202-11 | 202-12 | 202-22 | 202-44 | 202-410 | 202-24 |
---|---|---|---|---|---|---|
Avg EX Young's Modulus | 6664000.0 | 6664000.0 | 6664000.0 | 6664000.0 | 6664000.0 | 6664000.0 |
Avg EY Young's Modulus | 6664000.0 | 6664000.0 | 6664000.0 | 6664000.0 | 6664000.0 | 6664000.0 |
GXY Shear Modulus | 2546000.0 | 2546000.0 | 2546000.0 | 2546000.0 | 2546000.0 | 2546000.0 |
X Tensile Yield Strength | 62320.0 | 62320.0 | 62320.0 | 62320.0 | 62320.0 | 62320.0 |
X Compressive Yield Strength | 55760.0 | 55760.0 | 55760.0 | 55760.0 | 55760.0 | 55760.0 |
Y Tensile Yield Strength | 62320.0 | 62320.0 | 62320.0 | 62320.0 | 62320.0 | 62320.0 |
Y Compressive Yield Strength | 55760.0 | 55760.0 | 55760.0 | 55760.0 | 55760.0 | 55760.0 |
XY Shear Strength | 30444.0 | 30443.0 | 30442.0 | 30440.0 | 30440.0 | 30441.0 |
CTEX | 2.00E-06 | 2.00E-06 | 2.00E-06 | 2.00E-06 | 2.00E-06 | 2.00E-06 |
CTEY | 2.00E-06 | 2.00E-06 | 2.00E-06 | 2.00E-06 | 2.00E-06 | 2.00E-06 |
Poisson's Ratio vXY | 0.309 | 0.309 | 0.309 | 0.309 | 0.309 | 0.309 |
Poisson's Ratio vYX | 0.309 | 0.309 | 0.309 | 0.309 | 0.309 | 0.309 |