DMS 1928 CL1 52"

Description: Fabric

Details: Glass filament fabric woven from continuous glass fibers, meeting Boeing-Douglas DMS aerospace specifications. This material is engineered for structural reinforcement in composite layup processes for aircraft fuselage, control surfaces, and interior structural components. The fabric provides tensile strength, impact resistance, and compressive properties essential for primary and secondary aircraft structures. Available in 52-inch width for efficient composite manufacturing and integration into laminate systems.

Status: In-stock