WebCYCOM® 2265 is a phenolic prepreg for interior aircraft applications where low flammability and toxicity are required. The prepreg is light in color and exhibits excellent peel strength … WebCarbon Fiber – The Key Building Block of Advanced Composites; HexPly® XF Surfacing Technology Enabling High-Quality Paint-Ready Surfaces for Prepreg and Infused Components
CYCOM 5250-4 PREPREG S - e-aircraftsupply.com
WebFEATURES & BENEFITS • One of a family of compatible products based on second-generation cyanate ester chemistry • Low dielectric constant and loss tangent • Service temperature up to 350⁰F (177⁰C) • Autoclave, vacuum or press curable • Excellent hot/wet mechanical performance • Low moisture uptake, low out-gassing properties • Shelf Life is … WebTensile, flexure, and interlaminar shear data were obtained on specimens removed from the flat panels parallel to the warp fabric direction and at room temperature and 280 deg F 138 degrees C. Single lap shear tests were conducted on specimens removed from the adhesively bonded panels. fly wisconsin passport
Solvay Technical Data Sheets - MatWeb
WebCYCOM® 2265: Self-adhesive • Fiberglass Press (MOP), 250–275 (121–135) Side walls, phenolic system with low tack and Vacuum Bag partitions, drape ceiling panels Interior Applications CYCOM® 6070: Rapid-cure phenolic • Fiberglass Press (MOP, 280–325 (138–163) Stow bins, side system with low tack and drape • Carbon Crushed Core) … WebCYCOM® 114 is a unidirectional glass reinforced epoxy prepreg which cures at 325°F (163°C) and has a 250°F (121°C) service temperature. Applications for CYCOM® 114 include: Primary and secondary structural aircraft parts, Electrical applications, Helicopter rotor blades and Aircraft flooringService Temp: 250 F (121 C) Cure: Autoclave Markets WebMaterial Notes: 60 Volume % IM-7. CYCOM® 5250-4 is a 350°F to 400°F (177°C to 204°C) curing bismaleimide resin with a service temperature range of -75°F to 400°F (-59°C to 204°C). CYCOM 5250-4 is specifically formulated for use in primary aircraft structures. In addition, a variety of secondary structural components can take advantage ... flywise aviation