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 |
We use cookies to improve the operation of our websites. By using our websites you agree that we may store cookies on your device. You can learn more about how we use cookies by reviewing our Privacy Policy.