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Cure Cycle

60 minutes at 250-275°F (121-135°C)

Typical Applications

Aircraft panel facings Auto racing components Aircraft detail part lay-up Sporting goods Marine panels

Mechanical Data

PROPERTY50 PSI (0.34 MPa) CURE TEST METHOD ULTIMATE TENSILE STRENGTH Room Temperature (RT) 99 KSI (683 MPa)ASTM D638 TENSILE MODULUS Room Temperature (RT) 10.0 MSI (69 GPa)ASTM D638 ULTIMATE FLEXURAL STRENGTH Room Temperature (RT) 125 KSI (862 MPa)ASTM D790 FLEXURAL MODULUS Room Temperature (RT) 11.0 MSI (76 GPa)ASTM D790
NOTICE: Product data and parameters cited in this publication have been obtained in J.D. Lincoln, Inc. laboratories using the materials under carefully controlled conditions. The information, therefore, is believed to be accurate and correctlystated. Data of this type maybe considered to be indicative of representative properties obtainable. J.D. Lincoln, Inc. cannot accept responsibility for the misapplication of these products, nor for their use under uncontrolled conditions. Numerical values resulting from the application of this material are dependant on processing details. It is recommended that the user develop his or her own application techniques and generate data consistent withhis or her specific application and process. L-929