Solvay CYCOM® 5250-4 BMI Prepreg System with IM7-6K-5HS Woven Carbon Fiber

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Solvay CYCOM® 5250-4 BMI Prepreg System with IM7-6K-5HS Woven Carbon Fiber
Categories:	Polymer; Thermoset; Bismaleimide (BMI); Carbon Fiber/Thermoset Composite
Material Notes:	58 Volume % IM7-6K-5HS. 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 of the increased performance from using high-strain carbon fibers and the improved damage-resistance this system provides. CYCOM 5250-4 is available with either carbon fiber or glass fiber reinforcement in unidirectional tape, woven broadgood and roving forms. Features & Benefits: Short-term service temperature up to 450°F (232°C) Superior hot/wet properties at 220°F to 375°F (104°C to 190°C) Excellent toughness Void-free laminates High temperature resistance Low thermal conductivity Versatile cure Excellent compression strength properties after impact Shop life greater than 28 days at room temperature Fluid/solvent resistant Suggested Applications: Primary and secondary aircraft structure including: Engine nacelles Fuselage skins and stiffeners Wing and stabilizer spars and skins Other critical load-bearing components Mechanical properties are reported for standard cure + standard post-cure Information provided by Cytec, subsequently acquired by Solvay.
Vendors:

Available Properties

Density, QC-PT-55, Neat Resin
Volatiles
Water Absorption, As Tested (Wet)
Tensile Strength, Open Hole, (+,0,0,90,0), IM-7-6K-5HS, Wet
Tensile Strength, Open Hole, (+,0,0,90,0), IM-7-6K-5HS
Tensile Strength, Fill (90°), IM-7-6K-5HS, Wet
Tensile Strength, ASTM D3039, Warp (0°), IM-7-6K-5HS, Wet
Tensile Strength, ASTM D3039, Warp (0°), IM-7-6K-5HS
Tensile Strength, Fill (90°), IM-7-6K-5HS, Wet
Tensile Modulus, Fill (90°), IM-7-6K-5HS, Wet
Tensile Modulus, Warp (0°), IM-7-6K-5HS, Wet
Tensile Modulus, Open Hole, IM-7-6K-5HS
Tensile Modulus, Fill (90°), IM-7-6K-5HS, Wet
Tensile Modulus, Open Hole, IM-7-6K-5HS, Wet
Tensile Modulus, Warp (0°), IM-7-6K-5HS
Flexural Strength, Warp, (0°), IM7-6K-5HS, wet
Flexural Strength, Fill, (0°), IM7-6K-5HS, wet
Flexural Strength, Fill, (0°), IM7-6K-5HS
Flexural Strength, Warp, (0°), IM7-6K-5HS
Flexural Modulus, Fill, (0°), IM7-6K-5HS, wet
Flexural Modulus, Fill, (0°), IM7-6K-5HS
Flexural Modulus, Warp, (0°), IM7-6K-5HS
Flexural Modulus, Warp, (0°), IM7-6K-5HS, wet
Compressive Strength, Open Hole, [+,0,0,90,0] W/D=6, IM7-6K-5HS, wet
Compressive Strength, Open Hole, [+,0,0,90,0] W/D=6, IM7-6K-5HS, wet
Compressive Strength, Open Hole, [+,0,0,90,0] W/D=6, IM7-6K-5HS
Compressive Modulus, Open Hole, IM7-6K-5HS
Compressive Modulus, Open Hole, IM7-6K-5HS, wet
Shear Strength, ASTM D2344, Short Beam Warp (0°), IM7-6K-5HS, wet
Shear Strength, ASTM D2344, Short Beam Warp (0°), IM7-6K-5HS
Maximum Service Temperature, Air, Continuous; depends on cure cycle
Maximum Service Temperature, Air, short term; depends on cure cycle
Minimum Service Temperature, Air
Glass Transition Temp, Tg, QC-PT-22, Wet
Glass Transition Temp, Tg, Post Cure: 177°C for 6 hrs
Glass Transition Temp, Tg, Post Cure: 190°C for 6 hrs
Glass Transition Temp, Tg, Post Cure: 210°C for 6 hrs
Glass Transition Temp, Tg, Post Cure: 227°C for 6 hrs
Glass Transition Temp, Tg, QC-PT-22, Dry
Glass Transition Temp, Tg, Post Cure: 243°C for 6 hrs
Processing Temperature, Cure Temperature - Autoclave
Gel Time, QC-TP-87, in nitrogen atmosphere
Shelf Life
Shelf Life
Shelf Life

Property Data

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Manufacturer Notes:
Solvay, former Rhodia Engineering Plastics

Category Notes
Plastic

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