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Hexcel® Fibrelam® 2000 Grade 1 Panels for Aircraft Flooring

Category Other Engineering Material , Polymer , Thermoset , Carbon Fiber/Thermoset Composite
Manufacturer Hexcel
Trade Name Fibrelam®
Port Shanghai port,China
Trade Terms FOB, CFR, CIF
Payment Terms L/C, T/T, Western Union
Download PDF Hexcel® Fibrelam® 2000 Grade 1 Panels for Aircraft Flooring.pdf
Price EMAIL US    sales@lookpolymers.com
  Online Service   lookpolymers   27660005
Material Notes:
Designed for aircraft use where weight is critical, Fibrelam® 2000 structural sandwich panels utilize ultra light weight woven carbon prepreg skins bonded to high-strength aramid honeycomb to reduce weight without sacrificing performance. In addition to offering outstanding mechanical and physical properties, Fibrelam® 2000 panels are easy to install, and can be easily cut and machined on equipment normally found in airline maintenance shops. Fibrelam® 2000 panels are approved and qualified for use as flooring by major aircraft manufacturers and airlines worldwide.Information provided by Hexcel
Descriptive Properties Value Comments
Burn Length (mm) 99
BSS 7230; Flammability: 60 Second Vertical Ignition
Drip Extinguish Time (sec) 0
BSS 7230; Flammability: 60 Second Vertical Ignition
Glow Time (sec) 0
BSS 7230; Flammability: 45 Degree Test
Impact Resistance (N-m) 1.4
In-Plane Shear (N/mm) 61
Insert Shear (N) 4500
Long Beam Bending Deflection (mm) 12
MIL-STD-401B; At 445N (100lb)
Long Beam Bending Load (N) 1290
BSS 7250 Humidity; Humidity Resistance Load (100% at 60°C (140°F) for 30 days)
1330
MIL-STD-401B; Core Ribbon, Transverse
Panel Shear Strength (N) 3220
MIL-STD-401B 3 point loading; Load on Splice
3560
MIL-STD-401B 3 point loading;
Sandwich Peel (N/76 mm) 427
MIL-STD-401B 3 point loading; Core Ribbon, Transverse
Self-Extinguish Time (sec) 0
BSS 7230; Flammability: 60 Second Vertical Ignition
1.2
BSS 7230; Flammability: 45 Degree Test
Stabilized Core Compression (N/mm2) 13.8
Warpage (mm/m), max 0.8
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