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Rulon Bearings
Toray 2511 Prepreg Laminate with P6111-200 (M46J UD) Fiber
Categories: Polymer; Thermoset; Carbon Fiber/Thermoset Composite; Epoxy; Epoxy/Carbon Fiber Composite

Material Notes: This semi-toughened epoxy prepreg system was formulated for better oven cure processing than the #2510 general aviation (AGATE) prepreg system. #2511 provides excellent all-around structural properties with a high wet and dry TG while offering a flexible cure temperature (250°F to 350°F, 121°C to 177°C) with a very low void content. This prepreg system also can be used in industrial and recreational applications.

Information provided by Toray Composite Materials America, Inc.

Available Properties
  • Density, ASTM D792, Laminate
  • Filler Content, ASTM D3171, Fiber Volume
  • Tensile Strength, ASTM D3039, 90° (F2t), RTA
  • Tensile Strength, ASTM D3039, 0° (F1t), RTA
  • Tensile Modulus, ASTM D3039, 90° (E2t), RTA
  • Tensile Modulus, ASTM D3039, 0° (E1t), RTA
  • Compressive Strength, ASTM D6484, Open Hole, (QI:25/50/25), RTA
  • Compressive Strength, ASTM D6641, 90° (F2C), RTA
  • Compressive Strength, ASTM D6641, 0° (F1C), RTA
  • Compressive Modulus, ASTM D6641, 90° (E2C), RTA
  • Compressive Modulus, ASTM D6641, 0° (E1C), RTA
  • Shear Modulus, ASTM D5379, In-Plane (G12), RTA
  • Shear Strength, ASTM D2344, Short Beam, RTA
  • Shear Strength, ASTM D5379, In-Plane Shear (F12) Strength @ 5%, RTA
  • Processing Temperature, Cure Temp.
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