MK 50-05

Two-component methacrylate adhesive suitable for bonding fibre-reinforced composites in carbon and metals. Specific product for definitive bonding with no Primer, highly qualified

MK 50-05

  • Structural bonding of metal elements and molded parts in composite material
  • Excellent adhesion on different substrates, primerless, no abrasive surface treatments required
  • Widely used in Automotive for the assembly of external and internal parts in carbon fiber and thermoplastic
  • Suitable for fasteners fixing on fiberglass of the Marine & Military industry
  • It’s also suitable for bonding dissimilar metals in the Truck & Bus production (Tier-One)
  • Suitable for cracks repairs
  • Fast curing-time
  • High temperature resistance, suitable for hot painting cycles
  • Excellent resistance to acids and bases and hydrocarbon solvents

Approvals: FCA – Iveco – Ford – Volkswagen

 


Attachment

TDS MK 50-05
Bi-cartridge usage
Fastener Bonding Procedure ENG

Description

 

TYPICAL ADHESIVE PROPERTIES @ 24°C
Characteristics
Part A
(Adhesive)
Part B
(Activator)
Mix
(Part A + B)
Color Off-white or Black Amber or Black Amber or Black
Mix ratio by volume 1 1
Mix ratio by weight 1 1
Density, g/cc 0,99 1,02 0,98

 

Tensile Strength (MPa) 30 – 35 Lap Shear Strength (MPa) 20 – 27
Maximum Tensile Elongation (%) 2 – 6 Service Temperatures (°C)

-40 / +120

ok cataphoresis

Tensile Modulus (MPa) (1.200 – 1.700)

 

Cartridges

System

Drum System

Adhesive | Activator

Working Time

(minutes)

Fixture Time

(minutes)

MK 50-05 MK 50-05 A | MK 50-05 B 4 – 7 12 – 15

 

Additional information

Specific work-setting (component)

Operating Temperature > 90 ° C, Operating Temperature <0 ° C, STATIC bonding-line <100 cm (LIGHT HANDLING)

Type of joint (application mode)

BEAD – OVERLAP, SMALL POINT – DROP

Adhesive Working Time

< 10 MINUTES

Adhesive Fixture Time

10 ÷ 30 MINUTES

Substrates (suitable adherings match))

CARBON FIBER-REINFORCED COMPOSITES # CARBON FIBER-REINFORCED COMPOSITES, CARBON FIBER-REINFORCED COMPOSITES # GLASS REINFORCED FIBER COMPOSITES, GLASS REINFORCED FIBER COMPOSITES # GLASS REINFORCED FIBER COMPOSITES, HIGH ENERGY SURFACE THERMO-PLASTIC POLYMERS # CARBON FIBER-REINFORCED COMPOSITES, HIGH ENERGY SURFACE THERMO-PLASTIC POLYMERS # GLASS REINFORCED FIBER COMPOSITES, HIGH ENERGY SURFACE THERMO-PLASTIC POLYMERS # HIGH ENERGY SURFACE THERMO-PLASTIC POLYMERS, HIGH ENERGY SURFACE THERMO-PLASTIC POLYMERS # METALS and / or ALLOYS (Cu / Zn – Fe – Pb), INSERTS – FASTENER # ARAMIDE FIBER-REINFORCED COMPOSITES, INSERTS – FASTENER # CARBON FIBER-REINFORCED COMPOSITES, INSERTS – FASTENER # GLASS REINFORCED FIBER COMPOSITES, INSERTS – FASTENER # HIGH ENERGY SURFACE THERMO-PLASTIC POLYMERS, INSERTS – FASTENER # METALS and / or ALLOYS (Al – Ti – Ni – Cr – Fe), INSERTS – FASTENER # METALS and / or ALLOYS (Cu / Zn – Fe – Pb), METALS and / or ALLOYS (Al – Ti – Ni – Cr – Fe) # HIGH ENERGY SURFACE THERMO-PLASTIC POLYMERS, METALS and / or ALLOYS (Al – Ti – Ni – Cr – Fe) # METALS and / or ALLOYS (Al – Ti – Ni – Cr – Fe), METALS and / or ALLOYS (Cu / Zn – Fe – Pb) # METALS and / or ALLOYS (Al – Ti – Ni – Cr – Fe)

component sector/process

AERONAUTICAL / AEROSPACE, AUTOMOTIVE – TRUCK – BUS – AGRICULTURAL, FORESTRY MACHINES, INDUSTRIAL COMPONENTS, MILITARY DEFENCE, NAUTICAL & NAVAL, SPORT, TRAINS, WIND ENERGY

Type of failure mode (after joint stress)

COHESIVE (bonding failure inside the adhesive: residue presence on substrates), SUBSTRATE ((adhering structure failure: adhesive causes a fracture on substrate)

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