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CE 9000 is a modified epoxy resin system formulated to yield high strength retention under continuous 350°F and high humidity exposure. It is designed for primary and secondary laminate and honeycomb applications.

CE 9000-1 is a modified epoxy which exhibits excellent strength retention at temperatures up to 420°F and maintains high strength retention under high humidity conditions. CE 9000-1 is also a flame retardant system. 

High strength laminates for aircraft, aerospace and missiles applications such as radomes, fairings and other structural parts. CE 9000-1 has excellent compatibility with typical modified epoxy and nitrile phenolic adhesive films. It may be cured under the vacuum bag, autoclave or press conditions. Available in tape or broadgoods. 

 
 

Thermoset composite Type: thermoset composite | Temp: service temp < 320F | Process: autoclave, out of autoclave, press mold | CAI KSI: low | OHC Wet: low | TG Wet: 200 | Proc Temp: 300-330F

CYCOM® 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 flooring Service Temp: 250 F (121 C) | Cure: Autoclave

CYCOM® 1908/T800-12K is a 300⁰F - 350⁰F (149⁰C - 177⁰C) curing epoxy resin with a wet service temperature of 180⁰F - 200⁰F (82⁰C - 93⁰C) and a dry service temperature of 250⁰F - 350⁰F (121⁰C - 177⁰C).
Typical applications for CYCOM® 1908/T800-12K include use in pressure vessels and motor cases.

Features and Benefits

• Capable of oven or autoclave cure 
• High flow resin system which is adjustable through an intermediate hold step
• Resin system allows for good fiber tensile translation 
• Low resin reactivity which manages exothermic reaction and allows this material to be used in manufacturing thick wall composites

Versatile curing, toughened epoxy resin that can be cured from 180°F to 350°F (80°C to 180°C). A one hour cure at 275°F (135°C) gives a Tg of more than 310°F (155°C). Product Form: epoxy | Out Time (days): 60 | Temp: 266 (130) | Cure Flex: 176 - 356 (80 - 180) | Process: autoclave, press | TG: 300 (149) - 399 (204)

CYCOM® 2035 is a variable curing modified epoxy resin developed for high performance applications.
Six sigma principles have been employed to optimize the chemistry of CYCOM® 2035 to give excellent toughness and crash performance with processing ease.
CYCOM® 2035 can be initially autoclave cured between 185°F and 356°F (85°C and 180°C). Free-standing postcures can be applied following lower temperature cures to improve Tg and temperature performance.

Features and Benefits 

• Versatile cure from 185°F to 356°F (85°C to 180°C) 
• Excellent toughness and crash performance 
• Excellent mechanical properties 
• Tg of 347°F (175°C) following post cure 
• Controlled flow 
• Excellent cured surface finish 
• Shop life of 14 days at 75°F (24°C) 
• Available in a wide range of fibers and fabric weaves

Very tough modified epoxy resin system with exceptional high temperature performance. Suitable for highly stressed components exposed to elevated temperature environments (under bonnet/engine bay) including impact/crash structures. A two hour cure at 180°C 356°F) generates a Tg of over 200°C (392°F). Product Form: epoxy | Out Time (days): 21 | Temp: 356 (180) | Cure Flex: 275 - 392 (135 - 200) | Process: autoclave, press | Toughness: High

Extremely tough medium temperature curing modified epoxy resin. To use where impact resistance and lightweight as well as versatile cure conditions are required. 14 days out life at 21°C (70°F). Very high impact resistance. 135°C (275°F) cure temperature. DMA E' onset Tg of 150°C (320°F) following 3 hour at 135°C (275°F) cure. Out Time (days): 14 | Temp: 248 (120) | Cure Flex: 275 - 302 (135 - 150) | Process: autoclave, press

Rubber-modified, self-adhesive phenolic prepreg for interior aircraft applications. Sandwich panel press grade for multiple opening press. Type: Phenolic | Temp: Cure Temperature 260-285 | Process: Press Cure-MOP | OSU Heat Release: Yes | Flamability: Yes | Smoke: Yes | Toxicity: Yes | Reinforcements: Glass, Carbon, Aramid | Core Adhesion Level: High

Rubber modified self-adhesive phenolic prepreg for interior aircraft applications. Specifically designed for matched tool prcesses for fabricating crushed core components. This material has tailor-able tack and is designed for excellent surface quality Type: Phenolic | Temp: Cure temperature 260-285 | Process: Press Cure-MOP | OSU Heat Release: Yes | Flamability: Yes | Smoke: Yes | Toxicity: Yes | Reinforcements: Glass, Carbon, Aramid | Core Adhesion Level: High

Rubber modified self-adhesive phenolic prepreg for interior aircraft applications. Type: Phenolic | Temp: Cure temperature 255-275 | Process: Oven Cure | OSU Heat Release: Yes | Flamability: Yes | Smoke: Yes | Toxicity: Yes | Reinforcements: Glass, Carbon, Aramid | Core Adhesion Level: High

Phenolic system available as a drapeable prepreg for fabrication of complex vacuum bag or autoclave cured parts or as a low tack prepreg for press cured parts. Type: Phenolic | Temp: Cure temperature 200-250 | Process: Press Cure-MOP, Oven Cure, Press Cure-Crushed Core | OSU Heat Release: Yes | Flamability: Yes | Smoke: Yes | Toxicity: Yes | Reinforcements: Glass, Carbon, Aramid | Core Adhesion Level: High

Epoxy resin system Type: thermoset composite | Temp: service temp < 320F | Process: autoclave | CAI KSI: low | OHC Wet: medium | TG Wet: 234 (112) | Proc Temp: 250 (121)

CYCOM®4102 is a polyester structural resin that is a flame-resistant version of CYCOM®4101. CYCOM® 4102 is available on a variety of reinforcing fibers. When combined with fiber glass reinforcements, it is capable of meeting the requirements of Flight Standards Service Regulation No. 453 and MIL-R-7575C Grade B, Class 0. CYCOM®4102 prepregs are used to manufacture heating, defrosting, de-icing, and ventilating ducts, and in general purpose laminated parts. Type: Polyester | Temp: Cure temperature 240-260 | Process: Autoclave, Oven Cure | OSU Heat Release: No | Flamability: Yes | Smoke: No | Toxicity: No | Reinforcements: Glass, Carbon, Aramid | Core Adhesion Level: Medium

CYCOM® 4102A

CYCOM® 4102A is a polyester structural resin that is flame resistant.
CYCOM® 4102A is available on a variety of reinforcing fibers. When combined with fiberglass reinforcements, it is capable of meeting the requirements of FAR 25.853 and MIL-R-7575C Grade A, Class 0 and Class 2.

Typical applications for CYCOM® 4102A prepregs include use in manufacture heating, defrosting, de-icing, ventilating ducts, and general purpose laminated parts.

Features and Benefits 

• Flame resistant polyester resin 
• Meets MIL-R-7575 C requirements when combined with fiberglass

Thermoset composite Type: thermoset composite | Temp: 320F < Service Temp > 500F | Process: out of autoclave | CAI KSI: low | OHC Wet: high | TG Wet: 264 | Proc Temp: 180F

Epoxy resin system Type: thermoset composite | Temp: service temp < 320F | Process: autoclave | CAI KSI: low | OHC Wet: low | TG Wet: 190 (88) | Proc Temp: 250 (121)