MASTIKPLEXX 1100

MASTIKPLEXX 1100 is a two-component structural methacrylate adhesive, designed for the bonding of very high resistance of metals and composite materials.

  • Used for structural bonding of metal fasteners for composite molded parts.
  • Excellent adhesion on different substrates, with no surface treatments necessity of specific (primers or sanding)
  • Suitable for bonding aluminum and stainless steel letters, advertising sector.
  • Used in the automotive market for carbon fiber and thermoplastic panels bonding
  • Suitable for Fasteners & Fiberglass bonding in the Marine.
  • Suitable for bonding dissimilar metals in the Truck & Bus construction.
  • Cracks repairs.
  • Excellent resistance to acids and bases and hydrocarbon solvents.

Attachment

MASTIKPLEXX_1100_ENG

Description

PROPERTIES PART A PART B
CHEMICAL NATURE Methyl Methacrylate Activator
COLOUR Off white / Black Off white
DENSITY @ 25 °C 0,97 ± 0,02 g/ml 0,97 ± 0,02 g/ml
VISCOSITY @ 25 °C 30.000 – 70.000 mPa.s 30.000 – 50.000 mPa.s
MIX RATIO BY VOLUME 1 1
TYPICAL CHARACTERISTICS OF THE MIXED PRODUCT
OPEN TIME @ 24°C 10 – 20 mins
FIXTURE TIME @ 24°C 30 – 40 mins
FULL CURE TIME @ 24°C 24 hours
EXOTHERMIC PEAK OF THE REACTION ≈ 100 °C
DENSITY 0,97 ± 0,02 g/ml
HARDNESS 60 – 65 Shore D
MINIMUM GAP FILL 0,50 mm
MAXIMUM FUNCTIONAL GAP FILL 4 mm
TENSILE STRENGHT (ASTM D1002) Aluminium: 18 N/mm2

Mild steel: 25 N/mm2

Stainless steel: 28 N/mm2

Glass fiber: Substrate failure

ABS/Acrylate: Substrate failure

TENSILE ELONGATION 35 %
TENSILE MODULUS 1200 – 1700 MPa
OPERATING TEMPERATURE – 50 / + 120 °C

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 ÷ 30 MINUTES

Adhesive Fixture Time

30 ÷ 90 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

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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