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Composite Materials
Products in Composite Materials: Out of Autoclave Prepreg
87 Products found in Composite Materials
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Prepregs & Molding Compounds
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Prepregs & Molding Compounds
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Evonik
ROHACELL® A
Core Type:
Polymethacrylimide (PMI) Foam
Functions:
Core Material
ROHACELL® A is a closed-cell rigid foam crafted from polymethacrylimide (PMI) chemistry. Notably, it is entirely devoid of CFCs, aligning with environmental considerations. Engineered with precision, ROHACELL® A foam is tailored to meet the rigorous standards of the aerospace industry. It offers versatility in aerospace applications, supporting both prepreg processing and vacuum infusion across various pressure and temperature ranges.
Evonik
ROHACELL® WF
Core Type:
Polymethacrylimide (PMI) Foam
Functions:
Core Material
ROHACELL® WF is a core material with a coarse cell size that offers exceptional heat resistance and creep compression strength. It is characterized by its high temperature and compressive resistance, making it suitable for various applications, including aircraft, space, automotive, industrial, and radomes.
Evonik
ROHACELL® XT
Core Type:
Polymethacrylimide (PMI) Foam
Functions:
Core Material
ROHACELL® XT is a closed-cell rigid foam based on polymethacrylimide (PMI) chemistry that are free of CFCs and designed to meet the most extreme and demanding processing requirements. ROHACELL® XT foam is compatible with autoclave technologies, vacuum infusion, RTM, and VARTM processes.
Evonik
ROHACELL® S
Core Type:
Polymethacrylimide (PMI) Foam
Functions:
Core Material
ROHACELL® S is a closed-cell rigid foam created using polymethacrylimide (PMI) chemistry, and it is entirely free of CFCs. This foam is self-extinguishing, meaning it has fire-resistant properties. It is well-suited for various applications, including use in rail vehicles, watercraft, and the aerospace industry, where fire safety is a critical consideration.
Evonik
ROHACELL® SL
Core Type:
Polymethacrylimide (PMI) Foam
Functions:
Core Material
ROHACELL® SL foam cores exhibit exceptional mechanical strength, particularly under tensile loads, and high tenacity. These characteristics make it an excellent choice for applications subjected to significant dynamic mechanical loads. A ROHACELL® sandwich can provide the solution for achieving goals like excellent bending stiffness and strength, stabilizing thin FRP sheets against external forces, or creating complex 3-D geometries with minimal effort.
Evonik
ROHACELL® HERO
Core Type:
Polymethacrylimide (PMI) Foam
Functions:
Core Material
ROHACELL® HERO represents cutting-edge material technology, revolutionizing the production of lightweight and durable composite aircraft structures. These advanced sandwich cores, made from ROHACELL® HERO, offer unmatched weight-saving potential among all structural foams. They not only reduce the weight of aircraft but also enhance their durability over their operational lifespan. Additionally, they contribute to cost savings in the manufacturing process, making them a superior choice for modern aircraft construction.
Toray
Toray RS-17B
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Processing Methods:
Prepreg Processing, Vacuum Bagging, Out of Autoclave Prepreg
Toray RS-17B is a modified epoxy resin that delivers extremely low moisture absorption while providing excellent mechanical properties, toughness, and modulus. RS-17B is a flexible cure system that may be cured from 135°C to 177°C (275°F to 350°F). RS-17B has a long spaceflight heritage. 135°C–177°C (275°F–350°F) Cure Epoxy.
Park Aerospace
Park Aerospace E-765 T700 Uni Tape
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Reinforcement Material:
Glass Fibers, Carbon Fibers
Processing Methods:
Vacuum Bagging, Out of Autoclave Prepreg, Prepreg Processing, Compression Molding
End Uses:
Wing Skins, Doors, Wing Ribs, Wing Box, Bulkheads, Fuselage, Fairings, Radomes
Park’s E-765 is a toughened 270°F cure epoxy prepreg system designed to replace 350°F cure systems in many aircraft structural applications. Park’s E-765-3K-PW, -6K-5HS and 7781 materials are AGATE approved. FAA-approved, B-Basis design allowable databases for AGATE materials are available upon request. Park has also developed AGATE approved material and process specifications which are also available upon request.
Toray
Toray MicroPly™ EM-3
Functions:
Molding Compound
Chemical Family:
Epoxy & Epoxy Derivatives
Processing Methods:
Vacuum Bagging, Out of Autoclave Prepreg
Toray Toray MicroPly™ EM-3 is a 121°C (250°F) curing expanding epoxy film based on low density syntactic film technology. It is an effective material in generating internal pressure in closed mold Applicationss and honeycomb filling, splicing, and stabilization. Toray MicroPly™ EM-3 is available in film form from 30–91 cm (12–36”) wide with standard thicknesses from 0.0635 cm to 1.27 mm (0.025“ to 0.050”). Other widths and thicknesses may be available upon request. 121°C (250°F) Cure Expanding Syntactic Epoxy Film.
Tubus Bauer GmbH
Tubus Bauer GmbH PEI 4,0-48C
Functions:
Core Material
Core Type:
Thermoplastic Honeycomb
Chemical Family:
Polyimides (PI)
Tubus Bauer GmbH PEI 4,0-48C is a tubus core made with Polyetherimide.
Toray
Toray TC275-1E New
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Processing Methods:
Compression Molding, Prepreg Processing, Vacuum Bagging, Out of Autoclave Prepreg
TC275-1E is an extended out time version of the TC275-1 resin system. TC275-1E is a flexible cure toughened epoxy prepreg designed to enable composite part construction with low pressure or vacuum bag only (VBO) cures. The resin system provides a 28-day total out time to facilitate construction of thick or larger composite structures. TC275-1E may be cured at temperatures from 135°C (275°F) to 177°C (350°F) for higher temperature service. 135–177°C (275–350°F) Cure Toughened Epoxy Resin System
GEN 2 CARBON
G-TEX M 200
Reinforcement Material:
Carbon Fibers
Reinforcement Form:
Mat
Processing Methods:
Compression Molding, Resin Transfer Molding (RTM), Out of Autoclave Prepreg, Spray Lay-up, Vacuum Infusion Processing (VIP)
Features:
High Modulus, Excellent Formability, Good Surface Finish, Autoclaved, Fast Molding Cycle
G-TEX M 200 is Nonwoven fabric made from recycled carbon fiber. 200 denotes the fabric areal weight in gsm.
Toray
Toray BT250E-1
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Processing Methods:
Vacuum Bagging, Out of Autoclave Prepreg
End Uses:
Reflectors, Radomes, Tanks
Toray BT250E-1 resin system is a 121°C (250°F) cure epoxy prepreg system with excellent toughness and strength. It provides an outstanding surface finish under vacuum-bag/oven-cure only. The resin system, which is self-adhesive to honeycomb and foam core, is MIL-R-9300 qualified and makes a great choice for many Applicationss in the low-tomedium-service temperature range.
Toray
Toray CFRT® AG18-2L
Functions:
Laminate
Reinforcement Material:
Glass Fibers
Processing Methods:
Compression Molding, Vacuum Bagging, Out of Autoclave Prepreg
Toray Toray CFRT® AG18-2L is a reinforced thermoplastic composite laminate. It blends the benefits of a thermoplastic polymer matrix with woven glass fibers in a plain weave for enhanced performance. The AG-18 2L style laminate is available in a dual-layer product with glass fibers in both directions (0° & 90°). This construction is ultra-thin, lightweight, and resilient for improved energy return.
Toray
Toray 8020-FR
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Processing Methods:
Out of Autoclave Prepreg, Vacuum Bagging
End Uses:
Tanks, Marine Applications, Medical Devices, Motorsport
Toray 8020-FR is a modified epoxy resin system suitable for curing between 70°C (158°F) and 120°C (248°F). The medium viscosity resin is pre impregnated into high performance fibers such as carbon, glass and aramid. Toray 8020-FR offers excellent structural properties, flame retardance and toughness. Toray 8020-FR is designed for structural Applicationss in the motor racing, general industrial fabrications and marine industries and is suitable for a wide range of engineering Applicationss.
Toray
Toray TC275-1
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Processing Methods:
Compression Molding, Prepreg Processing, Vacuum Bagging, Out of Autoclave Prepreg
Toray TC275-1 is a dual-cure toughened epoxy prepreg designed to facilitate composite part construction with low pressure or vacuum pressure cures. The resin system features a 14-day tack life and 14-day total out time to allow the construction of thick or larger composite structure. TC275-1 may be cured at a lower temperature of 135°C (275°F) or can be cured at 177°C (350°F) for higher temperature service. 135–177°C (275–350°F) Cure Toughened Epoxy Resin System
Toray
Toray CFRT® BW-1000
Functions:
Laminate
Reinforcement Material:
Glass Fibers
Processing Methods:
Compression Molding, Vacuum Bagging, Out of Autoclave Prepreg
Toray Toray CFRT® BW-1000 is a reinforced thermoplastic composite laminate. It blends the benefits of a thermoplastic polymer matrix with woven carbon and glass fibers in a basket weave for enhanced performance. The BW-1000 style laminate is available in a single-layer product; carbon in one direction and glass fibers at a 90° orientation to the carbon that is ultra-thin, lightweight, and resilient for improved energy return.
Park Aerospace
Park Aerospace E-752 3K PW G30-500
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Reinforcement Material:
Glass Fibers, Carbon Fibers
Processing Methods:
Out of Autoclave Prepreg, Prepreg Processing
End Uses:
Radomes, Fairings, Nacelles, Ducts
Park’s E-752 is a toughened, 365°F cure epoxy system designed for demanding structural applications up to 265°F/wet. E-752 offers a good balance of toughness, high service temperature and good moisture resistance, as well as excellent tack and drape. Formulated for both oven and autoclave cure, E-752 provides for easy processing with oven cure, without sacrificing mechanical properties.
Toray
Toray TC250
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Processing Methods:
Prepreg Processing, Vacuum Bagging, Compression Molding, Out of Autoclave Prepreg
End Uses:
Reflectors, Radomes, Satellites, Tanks, Microwave Antennas
Toray’s TC250 offers an excellent balance of toughness, mechanical properties, and hot/wet performance. It is easily processed via vacuum bag/oven, autoclave, or press curing operations. Although TC250 is a 130°C (265°F) cure system, it can be post cured for a higher dry and wet Tg, which enhance the product’s elevated temperature performance. TC250 can also be cured or freestanding post cured to 177°C (350°F) to increase its high temperature performance. TC250 is available with virtually all fiber reinforcements in uni-directional tape, slit unidirectional tape, woven, and non-woven prepreg forms. 130°C (265°F) Cure, Toughened Epoxy Resin System
Park Aerospace
Park Aerospace E-766B 7781 E-Glass
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Reinforcement Material:
Glass Fibers
Processing Methods:
Out of Autoclave Prepreg, Compression Molding, Prepreg Processing
Park’s E-766B is a low tack, self adhesive epoxy resin system designed for honeycomb applications. E-766B displays excellent peel properties.
Tubus Bauer GmbH
Tubus Bauer GmbH PEI 4,0-64C
Functions:
Core Material
Core Type:
Thermoplastic Honeycomb
Chemical Family:
Polyimides (PI)
Tubus Bauer GmbH PEI 4,0-64C is a tubus core made with Polyetherimide.
Kordsa
Kordsa OM 12
Polymer Name:
Epoxy Resins & Compounds
Reinforcement Material:
Aramid (Kevlar), Glass Fibers, Carbon Fibers
Functions:
Prepreg
Processing Methods:
Out of Autoclave Prepreg
End Uses:
Structural Components, Structural Parts
OM 12 is a glass fiber or carbon fiber reinforced composites offer advantages of high corrosion resistance and high strength-to-weight ratio than traditional wood or steel materials. Kordsa may provide different reinforcement materials including glass or carbon UD, 2D and multiaxial impregnated with epoxy. For the huge size part production, generally vacuum bag only prepregs (OM12) are recommended
Toray
Toray E650
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Processing Methods:
Vacuum Bagging, Out of Autoclave Prepreg
End Uses:
Motorsport, Medical Devices, Tanks
Toray E650 is a low temperature curing toughened resin system pre-impregnated into high performance fibers such as carbon, glass and aramid. It is designed for the production of composite structures in the leisure and sporting industries and also for a range of engineering Applicationss. Toray E650 is compatible for co-cure with Toray’s low temperature cure resin film, Toray EF44, and Toray’s low temperature cure syntactic core, Toray MicroPly™ LT64.
Tubus Bauer GmbH
Tubus Bauer GmbH PEI 4,0-75C
Functions:
Core Material
Core Type:
Thermoplastic Honeycomb
Chemical Family:
Polyimides (PI)
Tubus Bauer GmbH PEI 4,0-75C is a tubus core made with Polyetherimide.
GEN 2 CARBON
G-TEX M 1200
Reinforcement Material:
Carbon Fibers
Reinforcement Form:
Mat
Processing Methods:
Compression Molding, Resin Transfer Molding (RTM), Out of Autoclave Prepreg, Spray Lay-up, Vacuum Infusion Processing (VIP)
Features:
High Modulus, Excellent Formability, Good Surface Finish, Autoclaved, Fast Molding Cycle
G-TEX M 1200 is Nonwoven fabric made from recycled carbon fiber. 1200 denotes the fabric width in mm.
Toray
Toray CFRT® TW-2000
Functions:
Laminate
Reinforcement Material:
Carbon Fibers
Processing Methods:
Compression Molding, Vacuum Bagging, Out of Autoclave Prepreg
Toray Toray CFRT® TW-2000 is a reinforced thermoplastic composite laminate. It blends the benefits of a thermoplastic polymer matrix with woven carbon fibers in a twill weave for enhanced performance. The TW-2000 1L & 2L style laminate is available in a single or multilayer product; carbon fiber reinforcement at 0° and 90° orientations that is ultra-thin, lightweight, and resilient for improved energy return.
Toray
Toray CFRT® XTS 3L and 4L
Functions:
Laminate
Reinforcement Material:
Glass Fibers
Processing Methods:
Compression Molding, Vacuum Bagging, Out of Autoclave Prepreg
Toray Toray CFRT® XTS 3L and 4L are reinforced thermoplastic composite laminates. They blend the benefits of a thermoplastic polymer matrix with uni-directional glass fibers for enhanced performance. The XTS style laminate is offered in 3-layer (0°/90°/0°Fiber orientations) and 4-layer (0°/90°/90°/0°Fiber orientations) construction that is ultrathin, lightweight, and resilient for improved energy return.
Toray
Toray MicroPly™ ES72A-2
Functions:
Core Material
Core Type:
Thermoset Foam
Chemical Family:
Epoxy & Epoxy Derivatives
Toray Toray MicroPly™ ES72A-2 is a 125°C (257°F) curing low-density, expanding, unsupported, epoxy syntactic core. ES72A-2 offers reduced processing, a one-shot cure, the ability to anchor inserts or fastenings, and increases the opportunity to consider lightweight, thin-walled composite sandwich structures. ES72A-2 can be easily contoured and shaped. Toray MicroPly™ ES72A-2 expands using a closed cell process ensuring complete homogeneous cell structure, the density/strength may be altered simply by changing cure pressure or limiting the volume available for expansion, the material is capable of expanding up to 650%. Toray MicroPly™ ES72A-2, formerly Amspand, is available in a variety of thicknesses down to 1 mm, and is supplied in sheets (625 mm x 400 mm).
NMG Composites
NMG Composites FENIX60
Functions:
Core Material
Core Type:
Thermoplastic Foam
FENIX60 is is a new type of environmentally friendly flame retardant sandwich material with excellent environmental protection, flame retardancy, low smoke density and low smoke toxicity. It is suitable for trains, subways and other transportation manufacturing industries, aerospace, ships, and flame retardant performance requirements Higher field.
Toray
Toray RS-3
Polymer Name:
Cyanate Ester Resin
Functions:
Prepreg
Processing Methods:
Prepreg Processing, Vacuum Bagging, Out of Autoclave Prepreg
Toray RS-3 is a modified cyanate ester prepreg resin developed to provide a good balance between toughness and high temperature/wet performance. RS-3 has been evaluated and qualified in the areas of satellite, airframe/missile, and dielectric structures. RS-3 is also available in several modified formulations including: RS-3C, a controlled-flow vacuum-bag/oven-cure version; and RS-3M, an extremely low-flow autoclave version. 177°C (350°F) Service Toughened Cyanate Ester Resin
Composites Evolution Ltd
Evopreg® EPC200
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Reinforcement Material:
Carbon Fibers, Aramid (Kevlar), Flax Fibers, Glass Fibers
Processing Methods:
Prepreg Processing, Vacuum Bagging, Out of Autoclave Prepreg
End Uses:
Motorsport, Snowboards, Yacht, Surfboards
Evopreg® EPC200 component prepregs are primarily designed for low-temperature, out-of- autoclave processing. Their flexible cure profile also makes them ideally suited to rapid processing at higher temperatures. Based on a toughened epoxy resin system, Evopreg® EPC200 is formulated specifically for high performance, ease of lay-up and excellent surface finish. The prepregs can be supplied with a range of reinforcement fibers and fabric constructions. They can be consolidated by vacuum bag/oven, autoclave or press molding and are designed for a range of applications including automotive, motorsport, sporting goods and general industrial..
Toray
Toray BTCy-2
Polymer Name:
Cyanate Ester Resin
Functions:
Prepreg
Processing Methods:
Out of Autoclave Prepreg
Toray BTCy-2 is our lowest dielectric cyanate ester prepreg resin system. This resin system is valued in high-energy microwave Applicationss due to the low loss tangent. 177°C (350°F) Cure Cyanate Ester
Toray
Toray CFRT® SL2000 / SuperLam
Functions:
Laminate
Reinforcement Material:
Glass Fibers, Carbon Fibers
Processing Methods:
Compression Molding, Vacuum Bagging, Out of Autoclave Prepreg
Toray Toray CFRT® SL2000 / SuperLam, is a reinforced thermoplastic composite laminate. It blends the benefits of a thermoplastic polymer matrix with woven carbon fibers in a twill or plain weave for enhanced performance. The SL-2000/SuperLam style laminate is available in a single-layer product that is ultra-thin, lightweight, and resilient for improved energy return.
Park Aerospace
Park Aerospace E-752-MTS HTS45 UDT
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Processing Methods:
Out of Autoclave Prepreg, Prepreg Processing, Compression Molding
End Uses:
Wing Skins, Fairings, Nacelles, Ducts, Wing Ribs, Wing Box
Park’s E-752-MTS is a toughened; 350°F cure epoxy system designed with improved mechanical properties and damage tolerance that is suitable for primary aircraft structures. Consistent with the E-752 family of epoxies, the E-752-MTS allows flexible and robust processing in Autoclave, Out of Autoclave and Press cures. It exhibits improved toughness and impact strength while maintaining good tack and drapeability for ease of layup.
Toray
Toray TC890
Polymer Name:
Thermoset Polyimide (PI)
Functions:
Prepreg
Processing Methods:
Out of Autoclave Prepreg
Toray TC890 high temperature polyimide prepreg system utilizes PROOF Research Advanced Composites Division 900HT resin system. TC890 is a high temperature, polyimide-based thermoset prepreg with outstanding dry property retention at 343°C (650°F), wet service property retention at 288°C (550°F), and short-term and intermittent service temperature capability to 427°C (800°F). TC890 has been successfully demonstrated in short term, transient heating Applicationss to temperatures as high as 1300°F. TC890 is an excellent non-MDA replacement for high temperature PMR-15 Applicationss. TC890 prepreg system is easily processable and thermally stable, exhibiting the highest glass transition temperature of commercially available structural matrices. This system displays exceptional toughness, excellent dielectric properties, and low toxicity. High Temperature Polyimide
Toray
Toray RS-36
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Processing Methods:
Vacuum Bagging, Out of Autoclave Prepreg
Toray RS-36 is an advanced modified epoxy system for structural composite Applicationss. RS-36 offers an excellent balance of mechanical properties, low moisture absorption, high glass transition temperatures, and a range of processing options. A higher Tg version, RS-36-1, with similar mechanical properties, is available. 177°C (350°F) Cure Epoxy Resin System
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