E-752 Structural Composite Material
 Toughened 360°F cure aerospace grade epoxy composite prepreg system.
 

FAA Accepted B-basis Design Allowables
- NCAMP data program  completed for two product forms

Reduced Cost and Lead time for composite Material Qualification
- Significantly reduced material testing
- Known allowables at start of qualification testing
- Reduced program qualification time and total cost

Toughened Structural Epoxy Prepreg
- 360°F cure
- 250°F hot/wet performance
- Self-adhesive in honeycomb sandwich panels

Vacuum, Oven or Autoclave Curing
- Flexible processing
- Reduced operating costs
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-752 Information and Resources

E-752 Datasheet

E-752 Datasheet  (A4 metric)

Material and Process Specifications (password)

Qualifications and Test Plans (password)

Material Equivalence (password)

MSDS (password)

DOT/FAA/AR-00-47

DOT/FAA/AR-03-19
 

 

 

 

 

 

 

 

 

 

 

Material Summary Tables
 Click here to access specific documents listed below
(password required)		 Full NCAMP Reports
FAA Approved Lamina Design Allowables Laminate Design Allowables
E752 / AS7 UniTape Oven Cure Oven Cure Qualification Material Property Data Report
Statistical Analysis Report
E752 / 3KPW Oven Cure Oven Cure Qualification Material Property Data Report
Statistical Analysis Report