Nelcote® E-765 Structural Composite Material - Park Electrochemical Corp - #1
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| Nelcote Advanced Composite Materials | ||||||||||||||||||
| E-765 Epoxy Prepregs Nelcote® E-765 is tough 250°F cure prepreg system designed to replace 350°F cure systems in aircraft structural applications. FAA-approved Design Allowable Databases are available upon request. | ||||||||||||||||||
| Applications / Qualifications - Primary Aircraft Structures • Fuselage • Wing • Control Surfaces - Secondary Aircraft Structures • Aircraft Frames • Doors • Shelves • Bulkheads Design Allowable Database B Basis Lamina Allowables • 3KPW T-300 Carbon - 195gsm • 6K5HS T-300 Carbon - 370gsm • 7781 Fiberglass - 295gsm • T-700 Uni-directional Tape -150-300gsm Laminate (notched) Allowables • 3KPW T-300 Carbon - 195gsm • 6K5HS T-300 Carbon - 370gsm • T-700 Uni-directional Tape -150- 300gsm | ||||||||||||||||||
| y Features & Benefits Designed to replace first generation 350°F (176°C) cure systems. Wide cure temperature process window of 250°F to 350°F Exhibits very low void content, i.e., <2% after vacuum cure. Superior fiber property translation. 180°F Wet service temperature after ~250°F cure Good tack and drape characteristics for 3 weeks at room temperature | ||||||||||||||||||
| Product Forms - Available on a wide variety of reinforcements including fiberglass and carbon - Carbon and glass broadgoods up to 60 inches wide - Available as unidirectional carbon tape - Compatible with autoclave, vacuum bag/oven or press cure processes | ||||||||||||||||||
| Global Availability For Information about Nelcote® materials: North America +1.203.755.1344 Asia Pacific +656.861.7117 Europe +33-562-985290 nelcote@parkelectro.com www.parkelectro.com | ||||||||||||||||||
| PARK Page1of5 ^ELECTROCHEMICAL CORP. Rev.3_08 Advanced Material Technologies | ||||||||||||||||||