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PRF Composite Materials RP542-4

PRF Composite Materials RP542-4 is a controlled flow, toughened epoxy prepreg system formulated for the manufacture of high performance structural composite parts requiring very good impact strength properties. The system has been formulated for a medium temperature cure of 80 - 120°C under vacuum or autoclave pressure and is also suitable for press molding. Fully cured, this system has a dry service temperature capability up to 120°C. The component surface finish with this system is excellent. The tack level of this system has been optimized to meet the constructor’s requirements and will be retained for up to 60 days at 20°C making this system suitable for the manufacture of large composite components. RP-542-4 can be supplied on most of the vast range of PRF reinforcement materials in widths up to 1350 mm wide.

Polymer Name: Epoxy Resins & Compounds

Functions: Prepreg

Reinforcement Material: Carbon Fibers

Processing Methods: Compression Molding, Prepreg Processing, Rolling, Vacuum Bagging

Technical Data Sheet
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Knowde Enhanced TDS

Identification & Functionality

Reinforcement Material
Composite Materials Functions

Features & Benefits

Main Features

• Excellent surface finish
• Core bondable
• Standard Cure 80°C - 120°C
• Service Temperature up to 120°C
• Peak Tg 138°C : 1 hour 120°C : DMA
• Controlled flow system
• Out life 60 days at 20°C
• Available on most of PRF’s reinforcement fabrics

Applications & Uses

Applications

• Aerospace
• Automotive
• Motorsport Components
• Marine
• Defense

Processing Methods

• Vacuum bag
• Autoclave
• Press molding
• Tube rolling
• Pressure bag

Processing

RP542-4 prepreg resin system may be processed at room temperature using established prepreg molding techniques on properly prepared molds. The cure cycle depends on the construction of the component and processing method. If honeycomb core is used in the part, the temperature ramp should be increased at a slower rate to enable a controlled flow of the resin to form a filet between the core and skin. Recommended cure cycle is to ramp from ambient to 120°C at 1-2°C/minute and then dwell for 1 hour. Part should then be allowed to cool naturally before demoulding. Alternative cure temperatures are in testing.

Properties

Physical Form
Mechanical Properties
ValueUnitsTest Method / Conditions
Tensile Strength (Unidirectional Epoxy Prepreg 300g/m2 34-700 12K)1961MPaISO 527-4
Tensile Modulus (Unidirectional Epoxy Prepreg 300g/m2 34-700 12K)125GPaISO 527-4
Strain At Failure (Unidirectional Epoxy Prepreg 300g/m2 34-700 12K)1.55%ISO 527-4
Compressive Strength (Unidirectional Epoxy Prepreg 300g/m2 34-700 12K)1204MPaISO 14126
Compressive Modulus (Unidirectional Epoxy Prepreg 300g/m2 34-700 12K)109GPaISO 14126
Flexural Strength (Unidirectional Epoxy Prepreg 300g/m2 34-700 12K)1.3GPaISO 14125
Flexural Modulus (Unidirectional Epoxy Prepreg 300g/m2 34-700 12K)97GPaISO 14125
ILSS (Unidirectional Epoxy Prepreg 300g/m2 34-700 12K)82MPaISO 14130
Interlaminar Shear Strength (Epoxy Prepreg 200gsm 2x2 Carbon Twill TR30S 12K)61.6MPaISO 14130 (1997)
Flexural Strength (Epoxy Prepreg 200gsm 2x2 Carbon Twill TR30S 12K)890MPaASTM D790-02
Flexural Modulus (Epoxy Prepreg 200gsm 2x2 Carbon Twill TR30S 12K)55.5GPaASTM D790-02
Compressive Strength (Epoxy Prepreg 200gsm 2x2 Carbon Twill TR30S 12K)538MPaISO 14126
Compressive Modulus (Epoxy Prepreg 200gsm 2x2 Carbon Twill TR30S 12K)55.6GPaISO 14126
Tensile Strength (Epoxy Prepreg 200gsm 2x2 Carbon Twill TR30S 12K)770MPaISO 527-4/3/2
Tensile Modulus (Epoxy Prepreg 200gsm 2x2 Carbon Twill TR30S 12K)56.1GPaISO 527-4/3/2

Technical Details & Test Data

Cure Cyle

Laminates with honeycomb core
Elevate temperatures at 2 - 5°C per minute up to 120°C. Hold the final temperature for 1 hour then allow the component to cool naturally inside the oven/autoclave before demoulding.
Vacuum bagged monolythic laminates
Elevate temperature at 3 - 5°C per minute up to 120°C, hold for 1 hour then allow the component to cool naturally inside the oven/autoclave before demoulding.
Press molded monolythic laminates
RP-542-4 system may be applied directly to hot press molds at temperatures up to 130°C. The cure time at the highest temperature will be approximately 45 minutes. The mold and component temperatures should be cooled to below 80°C before demouding. It is important, when manufacturing honeycomb sandwich panels without the use of adhesive films, to increase the resin content on the fabric plies being used as the first layers against the honeycomb. This ensures enough resin is available for the formation of the resin filet between the honeycomb and the skins.
 

Post cure cycle
A post cure can be carried out if the maximum Tg is required. The recommended post cure cycle is to ramp the temperature to 120°C at 1-2°C/minute and hold for 1 hour. Tg after this time will be 120-125°C (measured by DSC).

Storage & Handling

Storage

This product should be stored in refrigerated conditions.
Shelf life is 6 months at below -5°C or 12 months at below -18°C.