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Norplex-Micarta
Norplex-Micarta NP512
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Reinforcement Material:
Glass Fibers
End Uses:
Structural Parts
High flexural, impact and tensile strengths, and very high flexural modulus. It is constructed of glass fabric impregnated with an epoxy resin system. NP512 is engineered to provide better physical properties than NEMA FR-4, and be more dimensionally stable than standard NP510A. Applications for this material are where enhanced flexural modulus and physical strength are desired.
Norplex-Micarta
Norplex-Micarta NP193PM
Polymer Name:
Phenolic Compound
Functions:
Prepreg
Reinforcement Material:
Aramid (Kevlar), Glass Fibers
End Uses:
Pump Parts, Conveyor Parts, Belts/Belt Parts
NP193PM is composed of a 17 oz. aramid and "soft glass" fibers are combined to make a fabric that is stronger than pure aramid and less abrasive than glass fabrics. This material is impregnated with a high temperature phenolic resin matrix which includes a non-conducting solid lubricant. This composite has excellent mechanical strength at elevated temperatures and adverse environments. Applications include wear plates for conveyor systems, valve plates, and compressor and pump vanes.
Norplex-Micarta
Norplex-Micarta NP193P
Polymer Name:
Aramid (Kevlar), Phenolic Compound
Functions:
Prepreg
Reinforcement Material:
Aramid (Kevlar), Glass Fibers
End Uses:
Pump Parts, Conveyor Parts, Aerospace Applications, Brake Pads
17 oz. aramid and "soft glass" fibers are combined to make a fabric that is stronger than pure aramid and less abrasive than glass fabrics. This material is impregnated with a high temperature phenolic resin matrix, which produces a composite with excellent mechanical strength at elevated temperatures and adverse environments. Applications include wear plates for conveyor systems, valve plates, and compressor and pump vanes. Variations of this material may be developed for specific applications.
Norplex-Micarta
Norplex-Micarta NP193E
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Reinforcement Material:
Aramid (Kevlar), Glass Fibers
17 oz. aramid and "soft glass" fibers are combined to make a fabric that is stronger than pure aramid and less abrasive than glass fabrics. This material is impregnated with a high temperature epoxy resin matrix, which produces a composite with excellent mechanical strength at elevated temperatures and adverse environments.
Hexcel
HexPly® 954-6
Polymer Name:
Cyanate Ester Resin
Functions:
Prepreg
Processing Methods:
Prepreg Processing
HexPly® 954-6 is a 250ºF (121ºC) curing toughened cyanate resin with 300ºF (149ºC) Tg. HexPly® 954-6 is formulated for autoclave curing. Recommended cure is three hours at 250 F (121ºC). Service temperatures are maximized by a post cure of 350ºF - 450ºF (177ºC - 205ºC). The recommended lay-up procedure is HSP-L3. The recommended cure procedure is HSP-C4. Typical applications for HexPly® 954-6 include space structures, such as solar arrays, antennae and support structures, or any application where impact resistance, light weight, excellent dielectric and low outgassing properties are required. HexPly® 954-6 can be impregnated on all available fibers and fabrics.
KREMPEL GmbH
PREPREG system HH (polyimide resin)
Polymer Name:
Thermoset Polyimide (PI), Polyimide (PI)
Functions:
Prepreg
Processing Methods:
Compression Molding
End Uses:
Structural Components
PREPREG system HH (polyimide resin) are based on a high temperature resistant polyimide resin . Its processing is hot pressing or PREPREG winding.
Toray
Toray 8020 Rapi-Ply
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Processing Methods:
Vacuum Bagging, Out of Autoclave Prepreg
End Uses:
Medical Devices, Tanks
8020 Rapi-Ply is a Outstanding vacuum-bag-only (out-of-autoclave) processing capability. No debulking required off Bi-layer form facilitates fast lay-up
Renegade Materials Corporation
Renegade Materials Corporation RM-3002-CF
Polymer Name:
Thermoset Polyimide (PI)
Reinforcement Material:
Glass Fibers, Carbon Fibers
Functions:
Prepreg
Processing Methods:
Compression Molding
Renegade Materials Corporation RM-3002-CF Bismaleimide (BMI) prepreg product line includes Autoclave, Press and Out-of-Autoclave (vacuum bag only) processable BMI’s. Renegade Materials offers compatible BMI Film and Paste Adhesives, as well as BMI Infusion Resins for RTM/VaRTM processing. All of these products are formulated using next generation formulating technologies and a global supply chain. Renegade Materials' BMI's outperform the competition and exceed industry standards for quality, availability and price. It is a BMI Press Cure Prepreg.
Park Aerospace
Park Aerospace F-502 3K 8HS PAN
Polymer Name:
Phenolic Compound
Functions:
Prepreg
Reinforcement Material:
Glass Fibers, Carbon Fibers
Processing Methods:
Compression Molding, Prepreg Processing
End Uses:
Ducts
Park’s F-502 is a MIL-R-9299 phenolic resin system suitable for impregnation on any MIL-C-9084 fabric with a compatible finish. F-502 is used in the manufacture of ablative reinforcements in rocket nozzles, as well as ducting and secondary structures.
Renegade Materials Corporation
Renegade Materials Corporation RM-2014-LDk-TK
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Reinforcement Material:
Glass Fibers, Carbon Fibers
Processing Methods:
Vacuum Bagging
End Uses:
Radomes, Microwave Antennas
Renegade Materials Corporation RM-2014-LDK-TK is a 300°F (150°C) cure, modified epoxy prepreg system with very low dielectric and loss properties. RM-2014-LDk-TK provides good tack, drape and handling, and a great balance of mechanical properties.
Axiom Materials
Axiom Materials AX-6201XL
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Reinforcement Material:
Aramid (Kevlar), Glass Fibers, Carbon Fibers
AX-6201XL is a Structural Epoxy Unidirectional Prepreg for Vacuum Bag Only Processing.
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..
Renegade Materials Corporation
Renegade Materials Corporation RM-1066 Polyimide
Polymer Name:
Polyimide (PI)
Functions:
Prepreg
Processing Methods:
Prepreg Processing, Compression Molding
Renegade Materials Corporation RM-1066 Polyimide produces thousands of pounds of polyimide prepregs for flight hardware every month with a perfect quality and delivery record! Renegade Materials' high temperature prepregs and adhesives are powered by next generation polyimide resin technology. As the largest production supplier of polyimide composite materials in the world, we are the industry's most-trusted commercial source for AFR-PE-4 and other aerospace grade polyimide materials. Renegade Materials is the exclusive supplier of prepregs made with proprietary RM-1100 polyimide resin technology offering the highest temperature polymeric solution for commercial and military engine/aircraft applications up to 700°F. Renegade Materials is also the exclusive supplier of prepregs made with patented MVK-14M FreeFormTM, a polyimide prepreg used in global commercial aircraft applications up to 550°F.
Hexcel
HexPly® M27
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
HexPly® M27 is specifically designed for applications with fast curing cycles. It is ideally suited for high volume production techniques—in particular for ski manufacture. HexPly® M27 has been specially developed for UDprepregs with high glass fiber weights, e.g., 1637–6548 lbs/ft2 (500–2000 g/m2).
Hexcel
HexPly® 260
Polymer Name:
Phenolic Compound
Functions:
Prepreg
HexPly 260 is a phenolic resin developed to meet such F.S.T. (Fire, Smoke, Toxicity) regulations and the 1990 O.S.U. index (65/65), for aircraft interior parts as: side wall panels, floor panel, galleys, ceiling panels and lavatories. HexPly 260 prepreg is available in various fabric reinforcements.
Renegade Materials Corporation
Renegade Materials Corporation RM-2005
Polymer Name:
Epoxy Resins & Compounds
Reinforcement Material:
Glass Fibers, Carbon Fibers
Functions:
Prepreg
Processing Methods:
Vacuum Bagging
Renegade Materials Corporation RM-2005 is a 350°F Curing Toughened Epoxy Prepreg system. In response to widespread aerospace market demand for an alternative to industry-standard toughened epoxies, has developed the NEXT generation Toughened Epoxy Prepreg, optimized for both hand-lay-up and automated fiber placement (AFP) processing. RM-2005 is supported by an extensive mechanical property database on both carbon tape and fabric. Excellent mechanical performance and damage tolerance makes RM-2005 a superior choice for military or commercial structural applications. RM-2005 is readily available with no minimum order quantities and the fastest lead times in the industry.
SHD Composites
SHD Composites MTC811
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Processing Methods:
Prepreg Processing
MTC811 is a toughened, honeycomb bondable epoxy resin system designed to produce a durable cost effective component with an excellent surface finish. It can be supplied on a variety of fabrics and in UD format to meet your cost and manufacturing requirements.
Hexcel
HexPly® M95
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
HexPly® M95 is an epoxy resin which meets flammability, smoke, toxicity and heat release requirements for aircraft interiors. It is an alternative to raditional phenolic resins with the advantages of being REACH compliant, providing better mechanical properties and improving the surface aspect. HexPly® M95 epoxy resin is a high Tg epoxy system allowing hot in/hot out extremely fast cure cycles in press. It is an excellent mechanical performance epoxy resin system, suitable for structural and semi-structural parts in the cabin interior with high production rates.
Simex Technologies
SIMPREX® M745
Polymer Name:
Vinyl Ester Resin
Functions:
Prepreg
Processing Methods:
Vacuum Bagging, Compression Molding, Prepreg Processing
End Uses:
Motorsport, FRP Boats
SIMPREX® M745 is an advanced vinyl ester prepreg designed to provide a high performance-to-cost ratio. SIMPREX® M745 has a medium to high tack and provides good adhesion to core materials such as Nomex® honeycomb, balsa and polyurethane foam. It is a great choice for many applications in the range of low to medium service temperature.
Toray
Toray E720
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Processing Methods:
Out of Autoclave Prepreg, Vacuum Bagging
End Uses:
Tanks, Marine Applications, Medical Devices, Motorsport
Toray E720 is a 120°C (248°F) cure toughened epoxy prepreg. E720 offers excellent adhesive properties, allowing direct lamination to honeycomb without the use of a film adhesive. E720 is designed for structural Applicationss in motorsport and marine industries. E720 would also suit general aircraft fittings, sporting equipment, and a wide range of engineering Applicationss. Toray E720 is compatible for co-cure with Toray’s 120°C (248°F) cure resin film MicroPly™ EF72 and syntactic core Toray MicroPly™ SC72A. If fire retardant properties are required, refer to Toray E721-FR. 120°C (248°F) Cure Toughened Epoxy Resin System
ACP Composites
ACP Composites 5.9 oz. Carbon Fiber 2x2 Twill Weave RTS Prepreg
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Reinforcement Material:
Carbon Fibers
ACP Composites 5.9 oz. Carbon Fiber 2x2 Twill Weave RTS Prepreg is a twill weave fabric woven from 3K carbon fibers and impregnated with a thermosetting epoxy resin system. It is storable at room temperatures and does not require freezer storage. With the long out life of the resin matrix, the carbon fiber prepreg can be shipped and handled at room temperatures. It is ideal for use when a long shelf life is desired, high-temperature capabilities are not required and controlled resin content is wanted.
GMS Composites
GMS Composites EP – 270
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Reinforcement Material:
Aramid (Kevlar), Glass Fibers, Carbon Fibers
Processing Methods:
Prepreg Processing
End Uses:
Tanks
GMS Composites EP – 270 is a formulated epoxy resin matrix prepreg with long out life. The product has a versatile curing cycle from as low as 70°C or as high as 130°C, thus enabling the product to be used to produce a wide range of composite items, from large structures to numerous small components. EP-270 is available in a range of substrates such as carbon, glass or aramid. EP-270 allows faster cycle times at elevated temperatures. The product also has good dynamic strength properties. The prepreg has good flow and the tack of EP-270 can be varied.
SHD Composites
SHD Composites MTC475
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Processing Methods:
Prepreg Processing
MTC475 is an epoxy resin system designed to combine excellent clarity and elevated service temperature. It cures from 80°C to 120°C, allowing flexibility in component manufacture. It can be supplied on a variety of fabrics to meet your cost and manufacturing requirements.
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
PRF Composite Materials
PRF Composite Materials RP522
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Reinforcement Material:
Carbon Fibers
Processing Methods:
Vacuum Bagging, Compression Molding, Prepreg Processing, Rolling
PRF Composite Materials RP522 is made up of Woven fabrics which is used for General and Industrial Purpose.
GMS Composites
GMS Composites EP – 284
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Reinforcement Material:
Aramid (Kevlar), Glass Fibers, Carbon Fibers
Processing Methods:
Prepreg Processing
End Uses:
Tanks
GMS Composites EP – 284 is a formulated epoxy resin matrix prepreg with long shelf life and improved handling. The product has a versatile curing cycle from as low as 80°C or as high as 150°C, thus enabling the product to be used to produce a wide range of composite items, from large structures to numerous small components. EP-284 is available in a range of substrates such as carbon, glass or aramid. The product also has good dynamic strength properties as well as outstanding hot-wet resistance. The improved handling allows for easier molding of complex parts. The prepreg has good flow and the tack of EP-284 can be varied.
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.
SHD Composites
SHD Composites MTC400
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Processing Methods:
Prepreg Processing
MTC400 is an epoxy resin system designed to cure between 85°C and 135°C allowing flexibility in component manufacture. It is a toughened epoxy resin system designed for component manufacturing that can be supplied on a variety of fabrics and in UD format to meet your cost and manufacturing requirements.
SHD Composites
SHD Composites VTC401
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Processing Methods:
Prepreg Processing
VTC401 is an epoxy resin system designed to give an initial cure at low temperatures or snap cure at high temperatures with enhanced toughness, honeycomb bondability and higher service temperature, giving greater flexibility in component manufacture. It can be supplied on a variety of fabrics in UD format to meet your cost and manufacturing requirements.
PRF Composite Materials
PRF Composite Materials RP570
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Reinforcement Material:
Carbon Fibers
Processing Methods:
Compression Molding
PRF Composite Materials RP570 is a high performance formulated epoxy resin system with rapid Tg development enabling extremely short process times and excellent esthetic finish. A press tool held at constant temperature of 140°C can produce a part every 4 minutes ready for painting. RP-570 can be supplied on a variety of woven fabrics.
Kordsa
Kordsa AV10AF
Polymer Name:
Epoxy Resins & Compounds
Functions:
Adhesion Promoter, Prepreg, Surface Finish
Reinforcement Material:
Aramid (Kevlar), Glass Fibers, Carbon Fibers
End Uses:
Structural Reinforcement
AV10AF is a adhesive film prepreg and Adhesive film prepreg for metal-metal, metal-thermoset, thermoset-thermoset, thermoset-honeycomb bonding applications.
Kordsa
Kordsa EF 12
Polymer Name:
Epoxy Resins & Compounds
Reinforcement Material:
Aramid (Kevlar), Glass Fibers, Carbon Fibers
Functions:
Prepreg
Processing Methods:
Compression Molding, Prepreg Processing
End Uses:
Structural Components, Structural Parts
EF 12 is above 240 °C. High Tg EF12 resin system is used to produce structural prepregs. Optimized cure methods for these resin systems are Press and Autoclave molding.
APCM
APCM SG 4528-016AL-104V
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Processing Methods:
Prepreg Processing
APCM SG 4528-016AL-104V is a lightweight, conductive, surfacing film composed of a non-woven metallic aluminum mesh impregnated with a toughened epoxy resin plus an ultra light weight veil for outstanding surfacing capability. It is designed for lightning and shielding protection of aircraft, equipotential ground planes and as a counterpoise for antenna installations.
Axiom Materials
Axiom Materials AX-5202HT
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Reinforcement Material:
Carbon Fibers
AX-5202HT is a High Temp Cosmetic Epoxy Carbon Prepreg.
Toray
Toray E732 New
Polymer Name:
Epoxy Resins & Compounds
Functions:
Prepreg
Processing Methods:
Vacuum Bagging, Out of Autoclave Prepreg
End Uses:
Tanks
Toray E732 is a snap cure toughened epoxy resin matrix optimized for press curing (compression molding) prepreg Applicationss. With a cure time of 4 minutes at 160°C (320°F), an onset Tg of 170°C (338°F) is achieved. At this higher temperature, medium-to-high production rates can be accomplished, with customers able to produce beyond 50,000 parts per year. Toray E732 is a versatile matrix with a range of processing options allowing a variety of automotive and industrial Applicationss to be realized.
Arlon Electronic Materials
Arlon® 84N
Polymer Name:
Polyimide (PI)
Functions:
Prepreg
84N is a high performance ceramic-filled polyimide prepreg based on Arlon’s 85N pure polyimide system, designed for use in filling etched areas in polyimide multilayers that contain thick copper layers and for filling clearance holes in metal cores. The ceramic filler in the resin serves to reduce shrinkage and inhibit crack formulation during through-hole drilling in filled clearance areas.
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