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Material Name:
BMS8-124 CL1 TYI G5.5 .308" X 36" X 96"
Description:
Honeycomb Sheet
Details:
Non-metallic para-aramid honeycomb core sheet designed for sandwich composite construction in aerospace structures. This hexagonal-cell core material offers high strength-to-weight ratio, excellent shear properties, and inherent fire resistance. The material is commonly integrated with facing skins to create lightweight structural panels for aircraft fuselages, wings, control surfaces, and interior components where weight reduction and structural efficiency are critical.
Status:
In-stock |
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