CORE MATERIALS
HyboFOAM® C PMI Foam
HyboFOAM® C PMI Foam; closed-cell structural core defined for 32, 52, 75, 110, 150 ve 200…
Product Code: SDF-COR-013
ATA-NH aramid honeycomb is considered for aerospace, defence, UAV, radome and rail applications requiring high sandwich-panel stiffness at very low weight.
The product name alone is not sufficient. Cell size, density, thickness and L/W shear properties must be used together in panel design.
See the Nomex honeycomb selection guide for comparison.
The TDS lists 3.2, 4.8 and 9.5 mm cell options and product codes from 29 to 144 kg/m³. Mechanical data are stated as guaranteed values from 12.7 mm specimens tested at room temperature.
| Material | Phenolic-coated meta-aramid paper |
|---|---|
| Product family | ATA-NH aerospace grade |
| Cell sizes | 3.2 / 4.8 / 9.5 mm |
| Nominal density range | 29–144 kg/m³ (depending on grade) |
| Thickness tolerance | 2–50 mm: ±0.2 mm; 50.01–100 mm: ±0.5 mm; >100 mm: ±3 mm |
| Density tolerance | ±10% |
| Cell-size tolerance | ±5% |
| Mechanical directions | L and W directions |
Aerospace interior and structural panels
Defence and UAVs
Radome and antenna structures
Rail interior panels
Advanced industrial sandwich structures
Very low core weight
High sandwich-panel stiffness
Broad cell and density range
Defined L/W mechanical data
Traceable TDS product coding
CORE MATERIALS
HyboFOAM® C PMI Foam; closed-cell structural core defined for 32, 52, 75, 110, 150 ve 200…
CORE MATERIALS
HyboFOAM® E PMI Foam; closed-cell structural core defined for 52, 75 ve 110 kg/m³, maximum…
CORE MATERIALS
HyboFOAM® RF PMI Foam; closed-cell structural core defined for RF52, RF72, RF110 ve RF200,…
CORE MATERIALS
HyboFOAM® CRH PMI Foam; closed-cell structural core defined for CRH52, CRH75 ve CRH110, ma…