L-212 is a unidirectional cross-plied carbon fiber prepreg with an epoxy resin matrix. The L-212 system has adhesive film for core side bonding and a fiberglass scrim outer covering. Type: Epoxy | Temp: Cure temperature 225-300 | Process: Press Cure-MOP, Oven Cure, Press Cure-Crushed Core | OSU Heat Release: No | Flamability: Yes | Smoke: No | Toxicity: No | Reinforcements: Cross-plied Carbon | Core Adhesion Level: High


  • Global Business Unit
    Composite Materials


Segments Applications
Airframe Primary structural materials

Chemical categories

Chemical category Chemical family Chemical product
Composites Thermoset Epoxy

Region of commercial availability

  • Asia / Pacific
  • Europe / Middle East / Africa
  • North America
  • Latin America

Download documentation for L-212