High Closed Porosity Structural Foam Sheets 71HF
Recommended PMI foam for radar and radome:
- XK52, XK75, XK110 in medium temperature PMI foam;
- FXK52 and FXK75, FXK110 in PMI medium temperature foam;
PMI has been designed for use primarily in aerospace applications.
Its outstanding properties make it an ideal material solution for
aircraft components, including stringer structures in pressure
bulkheads. This structural foam is also suitable for helicopter
applications and is frequently used in the main and tail rotor
blades, as well as fuselage panels.
PMI Foam core spec.:
| Model | XK32 | XK52 | XK75 | XK110 | XK200 | CK52 | CK72 | CX52 | CX75 | CX110 |
| Density kg/m3 | 32 | 52 | 75 | 110 | 205 | 52 | 72 | 52 | 75 | 110 |
| Compression strength MPa | 0.4 | 0.9 | 1.8 | 2.9 | 7.5 | 0.8 | 1.6 | 0.9 | 1.8 | 2.9 |
Tensile strength MPa | 0.6 | 1.6 | 2.6 | 4.2 | 8.3 | 1.1 | 2.1 | 1.9 | 2.2 | 2.8 |
Tensile modulus MPa | 28 | 72 | 120 | 220 | 443 | 62 | 108 | 70 | 106 | 130 |
Shear strength MPa | 0.3 | 0.8 | 1.3 | 1.9 | 7.0 | 0.7 | 1.2 | 1.0 | 1.2 | 1.6 |
Shear elasticity MPa | 12 | 25 | 48 | 60 | 168 | 32 | 42 | 37 | 27 | 66 |
130℃ Compression strength MPa | 0.3 | 0.7 | 1.1 | 1.6 | 3.6 | 0.6 | 1.1 | 0.72 | 1.2 | 1.4 |
Dielectric constant | 1.06 | 1.08 | 1.10 | 1.15 | 1.27 | 1.08 | 1.10 | 1.08 | 1.10 | 1.15 |
Dielectric loss angle tangent | 0.005 | 0.0052 | 0.0054 | 0.0057 | 0.0065 | 0.0052 | 0.0054 | 0.0052 | 0.0054 | 0.0057 |
Detailed photo of PMI foam:
CNC machining and custom size is available
FAQ:
1. How can I get the reasonable price efficiently?
-Quantity, specification and 3D drawing will be helpful.
2. What file format are available for you to open?
-DWG, DXF, STP, IGS are available.
3. What is your payment term?
-T/T and Paypal are common, other methods could be discussed.
*Reminder: All prices on the website are for reference only, and
the actual prices are subject to specific communication.
