L-951
Laminating Woven Graphite Prepreg
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 Flammability
  • Self Extinguishing per FAR part 25.853
Sandwich Properties*
Core: ¼” cell x 0.004” (6.35 mm cell, x 0.10 mm) Aluminum Foil
Facings: 2 plies L-951-3K70P each side
  • RT Flatwise Tensile Strength: 900 PSI (6.2 MPa)
  • RT Sandwich Peel Strength: 6 in lb/in (27 N/25 mm)
  • *Sandwich peel strength varies with the orientation of the fibers directly against the core and the test direction.
  • Fibers laid up parallel with the test direction produce minimum strengths.
  • Fibers laid up perpendicular to the test direction produce maximum strengths.
  • L-951-(7 mil) sandwich peel strength ranges from 5-7 in lb/in (22-31 N/25 mm).
Mechanical Data

 

LAMINATE PROPERTIES

PROPERTY

85 PSI (0.59 MPa) CURE

VACUUM BAG CURE

TEST METHOD

ULTIMATE TENSILE STRENGTH

 

 

 

Room Temperature (RT)

91 KSI (628 MPa)

87 KSI (600 MPa)

ASTM D638

250°F (121°C)

80 KSI (552 MPa)

78 KSI (538 MPa)

ASTM D638

TENSILE MODULUS

 

 

 

Room Temperature (RT)

10.1 MSI (70 GPa)

9.9 MSI (68 GPa)

ASTM D638

250°F (121°C)

8.9 MSI (61 GPa)

8.8 MSI (61 GPa)

ASTM D638

ULTIMATE COMPRESSION STRENGTH

 

 

 

Room Temperature (RT)

78 KSI (538 MPa)

72 KSI (497 MPa)

ASTM D695

250°F (121°C)

52 KSI (359 MPa)

-

ASTM D695

COMPRESSION MODULUS

 

 

 

Room Temperature (RT)

8.9 MSI (61 GPa)

8.7 MSI (60 GPa)

ASTM D695

250°F (121°C)

8.0 MSI (55 GPa)

-

ASTM D695

ULTIMATE FLEXURAL STRENGTH

 

 

 

Room Temperature (RT)

112 KSI (772 MPa)

107 KSI (738 MPa)

ASTM D790

250°F (121°C)

88 KSI (607 MPa)

-

ASTM D790

FLEXURAL MODULUS

 

 

 

Room Temperature (RT)

9.4 MSI (65 GPa)

9.2 MSI (63 GPa)

ASTM D790

250°F (121°C)

8.7 MSI (60 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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