L-929
Solution Coated Epoxy Prepreg
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Cure Cycles
  • 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

PROPERTY

50 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

 
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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 correctly stated. Data of this type may be 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 with his or her specific application and process.

 
       
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