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Flame-retardant, unfilled amber epoxy laminating system for the manufacture and repair of composite structures.
Unit of Measure

Typical Properties

Original Equipment Manufacturer (OEM) Specifications

N/A Boeing BMS 8-201, Ty 4, REV F / Embraer MEP 22-011, REV C

Suggested Cure Schedule Fahrenheit (ºF)

N/A 5 days at 77 ºF or 2 hrs at 170º-200 ºF

Packaging

N/A Working packs

Mix Ratio Ritt by Weight

N/A 100:15

Mixed Viscosity at 77 Fahrenheit (ºF) Temperature

N/A 2400 cP

Minimum Gel Time/Pot Life at 77 Fahrenheit (ºF) Temperature

N/A 20 (100 gram mass)

Nominal Service Temperature

N/A Not Determined

Laminate Compressive Strength at 77 Fahrenheit (ºF) Temperature

N/A >45,000 psi

Specifications

Color

N/A Amber