Epoxy prepreg

MTC700

Med Temp Cure, High Temp Structural

Key Features & Benefits

Key Feature Highly toughened, high strain performance system with outstanding mechanical properties

Application Highly toughened with outstanding mechanical properties across reinforcement types for Motorsport, Automotive and Aerospace

Initial Cure Temp 275°F

Initial Cure Time 3 Hours- 6 Hours

Post Cure Option yes

Outlife 30 days at 70°F

TG Onset* 397°F -DMA

TG Peak* 414°F -DMA

Toughened Yes

Cure Autoclave

Availability All sites

MTC700 is an outstanding high strain, highly toughened epoxy prepreg system with dual cure and high Tg capabilities. Designed for high load bearing structures within the motorsport, high-performance automotive and aerospace markets.

MTC700 performs excellently with a range of fibres, offering high energy absorbing, G1c crack propagation
and interlaminar properties, combined with high strain-to-failure characteristics. The maximum Tg Onset of MTC700 is circa 200°C after a post-cure and 160°C after initial cure only.

It is supported by an extensive mechanical database and is available in both woven fabric and unidirectional formats on typically short lead-times.

Why choose this material

MTC700 is an elite performance system engineered for motorsport structures. It is a highly toughened, high strain matrix material designed to work with performance reinforcements across the motorsport market.

Supplied with SHD's renowned service, including:

Short two-week lead times and low MOQs
Exceptional product quality
First class technical support
Excellent customer service
The same manufacturing equipment and processes across all sites

Advanced composite solution for Motorsport

Advanced composite solutions for aerospace (passenger plane seating)

Motorsport Automotive Aerospace

Motorsport

SHD Composites is the advanced prepreg partner behind winning race teams

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Automotive

World-class performance with unmatched premium aesthetics for prestigious supercar and hypercar brands

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Aerospace

Advanced composites specified across major commercial aircraft today

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Technical Guidance Information

This material should be kept frozen at -18°C (0°F). It must be kept sealed in a polythene bag which must not be opened until fully thawed to room temperature. If the material is not fully used, then the material must be resealed in the polythene bag to prevent moisture absorption.

This material contains epoxy resin which can cause allergic reactions with skin contact and must avoid repeated and prolonged skin contact.

Please refer to the product Safety Data Sheet before using this material. The following precautions must be taken when using epoxy resin prepregs:

Overalls must be worn
Impervious gloves must be worn
Curing schedule is meant to be as a guide only and is subject to local conditions
To avoid exotherm, particular care must be taken with thick laminates
Ramp rates must not exceed 3.0°C (5.4°F)/min during initial cure and 0.3°C (0.5°F)/min during post cure