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 |
