Advanced composite solutions for aerospace (passenger plane seating)
SHD SECTOR EXPERTISE

Aerospace

Advanced composites specified across major commercial aircraft today.

MARKET EXPERTISE

Advanced composite solutions for the Aerospace market

SHD’s advanced composites are specified across major commercial aircraft today.

We are an advanced material partner to the world’s leading aerospace OEMs, delivering premium advanced composite prepreg solutions for a full range of manufacturing processes and design needs, all engineered to AS9100/EN9100 aerospace quality.

SHD offers what legacy suppliers cannot:

  • Short 2-week lead times and low MOQs

  • Continuous innovation pushing material performance further

  • Alternative processing with out of autoclave or rapid cure systems

  • Extensive technical data

  • Wide range of reinforcement types for optimal lightweighting and performance

SHD’s advanced materials support civil aviation, commercial aviation, defense, helicopters, drones, UAVs and AAVs. Applications include fuselage, structures, blades, engine components, communication systems, land gears, empennage, wings, nacelles, pylons, and interiors.

We have state-of-the-art production facilities in the UK, USA and Europe, offering continuous innovation and local service backed by 2-week lead times, low MOQs, and AS9100/EN9100 quality.

Interiors

SHD’s advanced materials are used throughout a wide range of aerospace interior components flying today. Applications include ducting, ceiling panels, overhead bins, sidewall panels, trolleys, seat structures, floor panels and underfloor cable ducts.

Below is a quick guide to product selection in typical application area.

SHD Prepreg composite material

FIND A PREPREG PRODUCT

We offer a wide range of tooling and component prepregs suitable for autoclave, press and oven curing. Using our product selector guide you can browse our products by process, type, resin system and market to find the right product for your needs.

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Application Areas

01

Interiors

FRVC411

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A versatile fire retardant epoxy component system with a low minimum temperature cure and increased toughness. UL94 V0 certifications on carbon and glass reinforcements.

FR308

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Sustainable solution, FR308 is highly flame retardant with exceptional Flame, Smoke and Toxicity (FST) and heat release rate (HRR) performance and has been designed and optimised for use in the rail, aerospace, and construction sectors. The PFA system is compliant with CS 25.853 and EN45545-1 to HL3. Depending on application, FR308 offers a cost effective, more environmentally friendly alternative to phenolic and FR epoxy systems.

MTC521FR

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A clear, flame retardant epoxy prepreg delivering premium visual carbon fibre finishes with certified fire performance. UL94 V1 and CS/FAR 25.853 compliant, it offers reliable processing and consistent clarity for cosmetic and safety critical components.
Advanced composite solutions for aerospace (passenger plane seating)
02

Battery box and fire containment

FRVC411

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A versatile fire retardant epoxy component system with a low minimum temperature cure and increased toughness. UL94 V0 certifications on carbon and glass reinforcements.

MTC510FRB

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General purpose flame retardant system

PS200

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Outstanding thermal and fire protection with non-structural service possible 150-250°C (dry). Ability to cope with rapid but limited time excursions >500°C. Meets ISO 2685 and AC 20-135.
03

Structures

MTC400

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Curing 135°C to 200°C, a toughened epoxy system with max dry Tg of 225°C and wet Tg > 160°C. Excellent property retention temperature up to 180°C, with good chemical resistance and typically used for components around the engine and pressure pipes.

MTC400-1

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Toughened epoxy system curing 135°C-180°C and providing dry Tgs of 145°C and 205°C respectively. Typically used on monocoque and elevated temperature structures has excellent retention of properties up to 150°C. Supported by extensive database.

MTC412

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Toughened system with max dry Tg of 170°C. Wet Tg of > 105°C. Developed for out of autoclave processing.

MTB350

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A 30% bio-derived epoxy component system with an exceptional outlife at 20°C of 6 months. Excellent all-round properties and particularly suitable for use with natural fibres and recycled fibre mats. Service up to 140-150°C possible.

HTC400

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Toughened epoxy system with an exceptionally high max dry Tg of 263°C and dry service at ~ 200°C.

VTC401

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Toughened epoxy system with versatile curing (65°C-120°C) and max Tg dry of 143°C. Excellent for prototyping and series production, with good OOA processing capability.

VTC410

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Toughened versatile cure (65-180°C) with max (dry) Tg of 190°C. Excellent for prototyping and limited series product, with good OOA processing.

MTC700

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Highly performance toughened epoxy prepreg system with dual cure at 135°C-180°C producing dry Tgs of 165°C and 203°C respectively. Designed for critical structures within the motorsport, high-performance automotive and aerospace markets. Performs excellently with a range of premium fibres and is supported by an extensive database.
Plane wing structure
04

Systems

MTC510

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General purpose epoxy system with a max dry Tg of 130°C. High quality, stable product widely used and proven for communications and antenna applications.

VTC401

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Toughened epoxy system with versatile curing (65°C-120°C) and max Tg dry of 143°C. Excellent for prototyping and series production, with good OOA processing capability.

VTC410

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Toughened versatile cure (65-180°C) with max (dry) Tg of 190°C. Excellent for prototyping and limited series product, with good OOA processing.
Boeing 737-800
05

Aerospace Tooling

LTB310-1

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This 30% bio derived tooling system allows for a cure temperature from 45°C to 70°C with a potential maximum service temperature of 200°C. As expected of a tooling system, low CTE and shrinkage values are combined with exceptional handling characteristics entirely in line with fully oil-based systems.

LTC216-3

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Cure range of 45°C - 70°C with maximum onset Tg after post cure of 218°C. 7 days out life at 20°C. Epoxy tooling system with extra room temperature out life for larger tools, warmer ambient temperatures. Excellent handling.

LTC410

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Cure range of 65°C - 80°C with maximum onset Tg after post cure of 192°C. 21 days out life at 20°C. A robust tooling system for general applications, with extra-long out life.

LTC400

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Cure range of 65°C - 80°C with maximum onset Tg after post cure of 207°C. 30 days out life at 20°C. A robust tooling system for aerospace and general applications, with an unmatched extra-long out life.

BMI-1SC

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Cure range of 160°C - 180°C with maximum onset Tg after post cure of 350°C. 30 days out life at 20°C (70°F). A Bismaleimide system with very high service temperatures, providing extended tool life.
Aerospace tooling
06

High Temperature/Space Components

CEM100

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Cyanate ester system with a maximum (limited) service temperature of 350°C from 250°C initial cure. Short exposures to 400°C possible.

CEM160

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120-135°C initial cure, modified, cyanate ester system with a max dry Tg capability of 275°C, after post-cure. Meets low-outgassing requirements.
Plane engine

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