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SAE AMS 3970/2A:2016-12-06

Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 2 - Qualification Program for Fiber, Fabric, Carbon Prepreg, Film Adhesive and Non-Structural Glass Prepreg

Summary

AMS3970/2 gives specific information about the qualification program for carbon fiber reinforced epoxy structural repair prepreg systems, applicable for 120 °C (250 °F) vacuum curing. The prepreg system may include an epoxy film adhesive to be applied in a co-curing process with the prepreg for joint and sandwich bonding. The need for a film adhesive shall be established during screening tests.

Notes

/ Note: Revision A

Technical characteristics

Publisher SAE International
Publication Date 12/06/2016
Confirmation Date 12/06/2016
Page Count 16
Themes Aerospace
EAN ---
ISBN ---
Weight (in grams) ---
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