A lightweight sandwich composite consisting of thin T300 carbon fiber/epoxy skins (0° and ±45° plies) bonded to a Nomex honeycomb core, manufactured via co-cure autoclave process. This architecture delivers high bending stiffness and strength with minimal weight, making it ideal for applications where rigidity and damage tolerance are critical. CFRP/Nomex sandwich panels are widely used in aerospace primary and secondary structures, marine hulls, and high-performance sporting goods where the material's exceptional stiffness-to-weight ratio and impact-resistant core outweigh the cost of solid laminates or foam-core alternatives.
Compliance & Regulations
Fiber Direction
Ply Schedule
Laminate Code
[0/45/0/45/0]T
Fiber angles relative to the 0° reference direction (red arrow in 3D view). 0° = longitudinal, 90° = transverse, ±45° = shear paths.
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Compressive Strength(σc) | 3.500 | MPa | — | ||
Young's Modulus(E) | 25.00 | GPa | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Maximum Service Temperature(Tmax) | 453 | K | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 320 | kg/m³ | — |