Nelcote® E-765 Structural Composite Material
250°F cure aerospace grade epoxy resin thermoset composite system. FAA accepted AGATE Design Allowables databases available. Wide processing window. Wet service temperature up to 180°F.
 

The largest single regulatory obstacle to using advanced thermoset composite materials in certified aircraft and general aviation applications has been the generation of design allowables that will satisfy FAR 23.613 Material Strength Properties and Design Values.

Until recently, individual airframe manufacturers generated design allowable databases as a routine part of their certification effort. However, with expensive qualification costs and long timelines, this approach has proved unfeasible for smaller manufacturers, and has often led larger manufacturers with established databases to continue to use “old” composite material systems.

Key Nelcote materials participate in design allowable databases that are accepted by the FAA for a family of materials based on E-765 - a tough, shop-friendly, 180°F(82°C) Wet service epoxy composite material system that cures at temperatures as low as 250°F(120°C). Designed specifically for aerospace and critical aircraft structures and based on the latest developments in epoxy resin technology, Nelcote E-765 demonstrates good toughness, outstanding fiber property translation and is suitable for vacuum bag, autoclave, or compression molding processes.

Password Access:
Several documents listed on this page require a password to access. If you are not registered with Park Electrochemical Corp., please visit our registration page to apply.

 





 

E-765 Material Information and Resources

E-765 Datasheet

E-765 Datasheet  (A4 metric)

Material and Process Specifications (password)

Qualifications and Test Plans (password)

Material Equivalence (password)

MSDS (password)

FAA Approval Documentation (password)

Flamability Reports (password)

Electrical Characteristics (password)

Space Flight Approval (password)

DOT/FAA/AR-00-47

DOT/FAA/AR-03-19

SAMPE Agate Paper

 

 

 

 

 

 

 

 

 

 

 

Material Summary Tables
Click here to access specific documents listed below
(password required)

 
Full AGATE Reports
FAA Approved Lamina Design Allowables Laminate Design Allowables Other Information
E765 / T700 24K UniTape Oven Cure
Oven Cure (Metric)
Autoclave Cure
Autoclave Cure (Metric)
Damage Tolerance Summary
Mode 1 Fracture Toughness
Mode 2 Fracture Toughness
Mixed Mode Fracture Toughness
AGATE W3.3-033051-104 (Rev 1)
AGATE W3.3-033051-108
E765 / 3KPW Oven Cure
Oven Cure (Metric)
Autoclave Cure
Autoclave Cure (Metric)

Sandwich Properties Summary

AGATE WP3.3-033051-103
AGATE WP3.3-033051-109
E765 / 6K5HS Autoclave Cure
Autoclave Cure (Metric)
Autoclave Cure
Autoclave Cure (Metric)
-- NIAR Report 02-2
AGATE WP3.3-033051-110
E765 / 7781 Oven Cure
Oven Cure (Metric)
-- -- AGATE W3.3-033051-105

E765 / 12K 2x2 Twill
-- -- Screening Data --

E765 / IM7 6K4HS
-- -- Screening Data --

E765 / 3K8HS
-- -- Screening Data --

E765 M40J UniTape
-- -- Screening Data --

E765/ 285 4HS Kevlar
-- -- Screening Data --
E765 / T700 100EPI Hybor -- -- Screening Data --
  Nelco®, Nelcote®, Neltec®, CoreFix® and PeelCote™ are trademarks of Park Electrochemical Corporation

Kevlar® is a registered trademark of E.I. du Pont de Nemours and Company. Spectra® is a registered trademark of Honeywell Performance Fibers.
 
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