Products in Composite Materials: Prepreg

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.

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.

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.

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.

Polyamide 6.6(PA6.6) is a is a industrial,Sports,Leisure and automotive.

Lectromat Glass Cloth and Mats WG-601-7 is applied in coil armor tape.

HexPly® 996 is a 350ºF (177ºC) curing cyanate siloxane resin with a 330ºF (165ºC) glass transition temperature. Standard cure is two hours at 350ºF (177ºC). HexPly® 996 can be autoclave and press cured. HexPly® 996 can be impregnated on all available fibers and fabrics. The recommended lay-up procedure for HexPly® 996 is HSP-L3. The recommended cure procedure is HSP-C1 or HSP-C6. Typical applications for HexPly® 996 are primary and secondary space structures where the optimum dimensional stability and lowest moisture absorption are required.

HexPly® F515 is an advanced, industrial grade, modified epoxy formulation designed for either vacuum bag or autoclave curing to offer very high laminate strengths, coupled with increased fracture toughness. HexPly® F515 has a 250°F (121°C) cure.

HexPly® M9.6H is a hotmelt, thermosetting, low tack epoxy resin matrix, specifically designed for prepreg applications at which short cure cycles of 100°C and above are required. M9.6H can be used for manufacture of large industrial components, suitable for cure of thin and thick sections. M9.6H exhibits a long out-life at ambient conditions.

Toray BTCy-1A is a toughened version of the BTCy-1 cyanate ester prepreg resin system. Its proprietary toughening mechanism and controllable flow make it an ideal product for use not only as a high performance prepreg resin system, but also as an accompanying resin system for film adhesives. BTCy-1A’s straight-up, easy processing at 177°C (350°F) (under low pressures) reduces curing time and production costs, while the system’s negligible volatile emission upon cure allows low void laminates. 177°C (350°F) Cure Toughened Cyanate Ester

HexPly® M91 is a high performance, very tough epoxy matrix for use in aerospace primary structures and engines. HexPly® M91 is a toughened, controlled flow, epoxy resin system supplied with unidirectional fibers.

PREGNIT TP-AC is high gloss, scratch resistant.

LTC400 Prepreg is designed to cure at low to medium temperatures whilst giving the potential for high temperature tooling. It has been formulated to give extended outlife without compromising performance. It can be supplied on a variety of fabrics to meet your cost and manufacturing requirements.

AX-4500 is a Toughened Phenolic Aramid Prepreg, Self-Adhesive.

HS Carbon Fiber UD300H60 is a E3 Matrix System with a precursor as PAN.

HexPly® M14 is a modified epoxy resin which provides good adhesion to honeycomb and foam cores. Its selfextinguishing characteristics meet the fire, smoke, and toxicity requirements of aerospace and railway specifications. HexPly® M14 can be used for very large industrial components subjected to severe environmental conditions.

Toray TC410 is Toray’s newest high performance cyanate ester resin system designed specifically for the latest generation of radomes and satellite structures. TC410 is unique in that it allows for low stress cures at 121°C (250°F) while achieving extremely low moisture absorption and high conversion levels. The lower cure temperature allows for lower stress in part fabrication. TC410 possesses all the key attributes for satellite use with good resistance to atomic radiation, low microcracking, and excellent resistance to process moisture. TC410 possesses low dielectric and loss tangents for radome usage. 121°C (250°F) Cure Toughened Cyanate Ester Resin System

TU300 is a polyetherketoneketone (PEKK) fiber-reinforced uni-directional tape that processes in the 675-725oF (360-385oC) temperature range. The prepreg is used in a variety of high performance, structural composite applications. PEKK is a high temperature semi-crystalline polymer with a good combination of toughness, chemical and solvent resistance, low moisture absorption and superior FST properties.

HexPly® 1454 is a self-extinguishing epoxy resin system with very high self adhesion properties. It has good handling and is tolerant of a wide range of processing conditions. HexPly® 1454 is ideal for the fabrication of honeycomb sandwich structures when high peel strength and good impact properties are required. HexPly® 1454 prepregs are only available with fabric reinforcements.

Resinoid 1365 is a glass reinforced, two-step phenolic molding compound offering excellent mechanical strength as well as good electrical and thermal characteristics. This material is offered as a moderate size pellet suitable for compression and transfer molding. It can be used in injection molding systems with deep flight screws.

HexPly® M21 is a high performance, very tough epoxy matrix for use in primary aerospace structures. It exhibits excellent damage tolerance, especially at high energy impacts. HexPly® M21 is a toughened epoxy resin system supplied with unidirectional or woven carbon or glass fibers. HexPly® M21 was developed as a controlled flow system to operate in environments up at 121°C (250°F).

THINPREG™ TP 135 is a breakthrough product combining high strength and high toughness in a thin ply format. The PES-toughened epoxy system shows compression after impact properties typical of 3rd generation aerospace matrices. Thin ply materials achieve higher usable properties from the fiber through spreading load more consistently though the laminate and delaying first ply failure. Negligible ply drop-off effects and greater degrees of freedom in design are now combined with a PES-toughened system for high resolution, highly optimized, super-strong composite structures.

Toray Toray AmberTool® HX56 is a low temperature curing epoxy composite tooling prepreg. After a suitable post cure, an end use temperature of 180°C (356°F) is achieved. Toray AmberTool® HX56 achieves an excellent surface finish for small to medium sized autoclave tooling.

GMS Composites EP-282 is a formulated epoxy resin matrix prepreg with long shelf life. 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-282 is a resin film available on a lightweight scrim or without a scrim. The EP-282 resin is compatible with GMS Composites pre-pregs. The resin film has good flow and the tack of EP-282 can be varied.

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

AX-3100 is a toughened low dielectric epoxy fiberglass prepreg.

PREPREG system HH (polyimide resin) are based on a high temperature resistant polyimide resin . Its processing is hot pressing or PREPREG winding.

Deltapreg DT197 is a Automotive with heat managment Application.

HS Carbon Fiber UD150H60 is a E3 Matrix System with a precursor as PAN.

HS Carbon Fiber UD100H60 is a E3 Matrix System with a precursor as PAN.

Park’s F-552 is a high purity silica filled phenolic resin coated on high strength grade silica fabric. F-552 is used in the manufacture of intermediate temperature ablative rocket nozzles, heat shields, and combustion chambers in highly oxidative environments.

AX-3270 is a Structural Epoxy Fiberglass Prepreg.

Taconic 7208 PTFE-Glass Fabric is a Standard Grade PTFE-Glass Fabric is used in the widest range of applications due to its combination of high performance and moderate price. Applications include release sheets on heat-sealing machines and laminate presses, release surface for paints, adhesives and food products, gaskets, seals and bearings for chemicals, oils, and gasses, thermal insulation for high-temperature and chemical-resistant applications and covers on hot platens, chutes, hoppers and troughs.

HexPly® EH25 is a high performance, tough 180°C curing matrix for use in Aerospace primary structures. HexPly® EH25 is a self-extinguishing epoxy resin with controlled flow. HexPly® EH25 prepregs are available with fabric and UD tape.

Renegade Materials Corporation RM-2002 provides high-performance materials for aircraft applications, both primary and secondary structure and toughened prepregs available.

CM 15 is a Visual composites, Semi Structural and Fast Isothermally Press Curable, Class A Surface quality for painting, Hot Demoldable, Improved UV and environmental resistance, Improved fiber imprinting resistance