Unlike metals which have similar properties in all directions (isotropic), the properties of composites are varying, dependent on the orientation of the fibers in each layer.
*This diagram illustrates a "generic" layup. The SKU being viewed may not have the layup schedule shown in this diagram. To view this SKU's particular layup please check out the "LAYUP ORIENTATION" tab.
P/N | 25483-UHM-BLOWOUT |
---|---|
Application | Space & Stable Structures |
Clearance | Yes |
ECCN | EAR99 |
Finish | Cello Wrap Gloss |
Height | 0.825 |
HTS - Harmonized Tariff Code | 6815.13.0000 |
Inside Dimension | 0.75 |
Length | 66 |
Major ID | 0.75 |
Major OD | 0.825 |
Materials | Ultra High Modulus Carbon |
Minor ID | 0.75 |
Minor OD | 0.825 |
Outside Dimension | 0.825 |
REACH | SCHV JUN-2022 |
RoHS | 2015/863/EU |
Shape | Square |
Tensile Modulus, msi | 36.9 |
Thickness | 0.0375 |
USMCA Criterion | D |
Wall Thickness | 0.0375 |
Weight | 0.4 |
Width | 0.825 |
The inner and external corner radii are measured by hand with a radius gauge with no tolerance called out.
Estimated Laminate Stiffness Properties (psi)
EX | EY | GXY | EXB | EYB |
3.696E+07 | 2.708E+06 |
2.508E+06 |
5.198E+07 |
9.598E+05 |
Estimated Laminate CTE Properties (ppm/°F)
CTE-X | CTE-Y | CTE-XY |
-6.37E-07 |
5.98E-06 |
7.34E-22 |
Estimated Laminate Strength Properties (psi)
X-Axis Tension |
X-Axis Compression |
Y-Axis Tension |
Y-Axis Compression |
XY-Shear |
1.398E+05 |
-4.288E+04 |
1.472E+04 |
-1.664E+04 |
1.607E+04 |