ARALDITE® LY 5052 / ARADUR® 5052

ARALDITE® LY 5052 / ARADUR® 5052 is a cold-curing epoxy system used in aerospace and industrial composites, tooling, and aircraft repair. ARALDITE® LY 5052 is a low-viscosity epoxy resin, and Aradur® 5052 is a mixture of polyamines.

RTU Product Type: Laminating Resin System

Product End Uses: Aerospace Materials, Aircraft, Marine Applications

Chemical Family: Epoxy & Epoxy Derivatives

Composites Processing Methods: Filament Winding, Infusion, Pressure Molding, Resin Transfer Molding (RTM), Wet Lay-Up

Features: Cold Curing, Fast Setting, Good Dynamic Properties, Good Impregnation Capability, Good Mechanical Properties, High Temperature Resistance, Long Potlife, Low Viscosity

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Identification & Functionality

Features & Benefits

Ready-to-Use Product Features
Key Properties
  • Low viscosity, easy impregnation of reinforcement materials.
  • Long pot life (2 hours for 100 ml at ambient), ample processing time allows production of big objects.
  • High temperature resistance (glass transition temperature) after ambient cure: 60 °C, after post-cure at 100:120 °C.
  • Excellent mechanical and dynamic properties after ambient cure with potential for even higher properties after post-cure at elevated temperatures.
  • Also laminates show outstanding mechanical and dynamic properties. This system is qualified by the Luftfahrtbundesamt (German Aircraft Authority) for the production of gliders.

Adequate skin protection is indispensable.

Features and Benefits
  • Low viscosity, easy impregnation of reinforcement materials.
  • Long pot life (2 hours for 100 ml at ambient), ample processing time allows production of big objects.
  • High temperature resistance (glass transition temperature) after ambient cure: 60 °C, after post-cure at 100:120 °C.
  • Excellent mechanical and dynamic properties after ambient cure with potential for even higher properties after post-cure at elevated temperatures.
  • Also laminates show outstanding mechanical and dynamic properties. This system is qualified by the Luftfahrtbundesamt (German Aircraft Authority) for the production of gliders.
  • Adequate skin protection is indispensable.

Applications & Uses

Application Area
Composites Processing Methods
Product End Uses
Markets
Applications
Applications

Aerospace and industrial composites, tooling, aircraft repair

Application Details

Aerospace and industrial composites, tooling, aircraft repair

Properties

Physical Form

Regulatory & Compliance

Technical Details & Test Data

Processing Data
  • Wet lay-up
  • Resin Transfer Moulding (RTM)
  • Pressure Moulding
  • Filament Winding
Typical Cured Properties

Property

Value

Unit

Test Method

Condition

Initial Mix Viscosity at 64 °F

1150 - 1350

[cps]

ISO 12058-1

64 °F

Initial Mix Viscosity at 77 °F

500 - 700

[cps]

ISO 12058-1

77 °F

Initial Mix Viscosity at 104 °F

200 - 250

[cps]

ISO 12058-1

104 °F

Viscosity Buildup at 77 °F

to 1500

[cps]

ISO 12058-1

77 °F

Viscosity Buildup at 77 °F

to 3000

[cps]

ISO 12058-1

77 °F

Viscosity Buildup at 104 °F

to 1500

[cps]

ISO 12058-1

104 °F

Viscosity Buildup at 104 °F

to 3000

[cps]

ISO 12058-1

104 °F

Viscosity Buildup at 140 °F

to 1500

[cps]

ISO 12058-1

140 °F

Viscosity Buildup at 140 °F

to 3000

[cps]

ISO 12058-1

140 °F

Viscosity Buildup Time at 77 °F

50 - 60

[min]

ISO 12058-1

77 °F

Viscosity Buildup Time at 77 °F

90 - 110

[min]

ISO 12058-1

77 °F

Viscosity Buildup Time at 104 °F

40 - 45

[min]

ISO 12058-1

104 °F

Viscosity Buildup Time at 104 °F

50 - 60

[min]

ISO 12058-1

104 °F

Viscosity Buildup Time at 140 °F

15 - 18

[min]

ISO 12058-1

140 °F

Viscosity Buildup Time at 140 °F

18 - 22

[min]

ISO 12058-1

140 °F

Pot Life at 64 °F

280 - 320

[min]

TECAM, 100 mL, 65 % RH

64 °F

Pot Life at 77 °F

110 - 160

[min]

TECAM, 100 mL, 65 % RH

77 °F

Pot Life at 104 °F

45 - 55

[min]

TECAM, 100 mL, 65 % RH

104 °F

Gel Time at 77 °F

420 - 500

[min]

Hot Plate

77 °F

Gel Time at 104 °F

150 - 170

[min]

Hot Plate

104 °F

Gel Time at 104 °F

40 - 55

[min]

Hot Plate

104 °F

Gel Time at 176 °F

14 - 17

[min]

Hot Plate

176 °F

Gel Time at 212 °F

4 - 6

[min]

Hot Plate

212 °F

Gel Time at 248 °F

2 - 3

[min]

Hot Plate

248 °F

Gelation Start at 23 °C

5 - 6.5

[h]

-

Thin layers (0.4 - 0.7 mm)

Gelation End at 23 °C

7 - 8

[h]

-

Thin layers (0.4 - 0.7 mm)

Typical Cure Cycle 1

-

-

-

1 day 23 °C + 15 h 50 °C

Typical Cure Cycle 2

-

-

-

1 day 23 °C + 4 h 100 °C

The values shown are for small amounts of pure resin/hardener mix. In practice, fiber content and laminate thickness may modify the gel time to a very significant extent. In composite structures the gel time can differ significantly from the given values depending on the fiber content and the laminate thickness.

Cured Reinforced Formulation Properties

FLEXURAL TEST

(ISO 178)
Samples: 16 layers (4 mm)
E-glass fabric 1:1, 280-300 g/m2
Fiber volume content: 45 - 46 %
Cure: 10 h 176°F

Property Value Unit Test Method Condition
Flexural Strength (Unconditioned) 63.8 - 71.1 [Ksi] ISO 178 Unconditioned
Elongation at Flexural Strength (Unconditioned) 2.7 - 3.0 [%] ISO 178 Unconditioned
Ultimate Strength (Unconditioned) 60.9 - 66.7 [Ksi] ISO 178 Unconditioned
Ultimate Elongation (Unconditioned) 2.9 - 3.2 [%] ISO 178 Unconditioned
Flexural Modulus (Unconditioned) 2900 - 3190 [Ksi] ISO 178 Unconditioned
Flexural Strength (After 30 days in H2O 73°F) 55.1 - 58.0 [Ksi] ISO 178

After 30 days in H2O 73°F

Elongation at Flexural Strength (After 30 days in H2O 73°F) 2.7 - 3.0 [%] ISO 178

After 30 days in H2O 73°F

Ultimate Strength (After 30 days in H2O 73°F) 49.3 - 53.7 [Ksi] ISO 178

After 30 days in H2O 73°F

Ultimate Elongation (After 30 days in H2O 73°F) 1.9 - 3.4 [%] ISO 178

After 30 days in H2O 73°F

Flexural Modulus (After 30 days in H2O 73°F) 2755 - 3045 [Ksi] ISO 178

After 30 days in H2O 73°F

TENSILE TEST

(ISO 527)
Samples: 16 layers (4 mm)
E-glass fabric 1:1, 280-300 g/m2
Fiber volume content : 45 - 46 %
Cure: 10 h 176°F

Property

Value

Unit

Test Method

Condition

Tensile Strength

52.2 - 56.6

[Ksi]

ISO 527

10 h 176°F

Ultimate Elongation

1.6 - 1.9

[%]

ISO 527

10 h 176°F

Tensile Modulus

4800 - 5670

[Ksi]

ISO 527

10 h 176°F

INTERLAMINAR SHEAR STRENGTH

(ASTM D 2344)
Short beam: E-glass unidirectional specimen, thickness t = 3.2 mm
Fiber volume content: 60 %

Property

Value

Unit

Test Method

Condition

Interlaminar Shear Strength (Unconditioned)

8265 - 8845

[psi]

ASTM D 2344

7 days RT

Interlaminar Shear Strength (After 1 hour in H2O 100 °C)

7975 - 8700

[psi]

ASTM D 2344

After 1 h in H2O 100 °C

Interlaminar Shear Strength (After 8 hours in H2O 80 °C)

8700 - 9425

[psi]

ASTM D 2344

After 8 h in H2O 80 °C

Interlaminar Shear Strength (After 8 hours in H2O 80 °C)

8410 - 8990

[psi]

ASTM D 2344

After 8 h in H2O 80 °C

Packaging & Availability

Packaging Type

Storage & Handling

Storage Conditions

Araldite® LY 5052 should be stored in a dry place, in the sealed original container, away from heat and humidity, at temperatures between +2°C and +40°C (+35.6°F and +104°F). Under these storage conditions, the shelf life is 3 years. The product should not be exposed to direct sunlight.

Aradur® 5052 should be stored in a dry place, in the sealed original container, away from heat and humidity, at temperatures between +2°C and +40°C (+35.6°F and +104°F). Under these storage conditions, the shelf life is 3 years. The product should not be exposed to direct sunlight.

Storage Information
  • ARALDITE® LY 5052 should be stored in a dry place, in the sealed original container, away from heat and humidity, at temperatures between +2°C and +40°C (+35.6°F and +104°F). Under these storage conditions, the shelf life is 3 years. The product should not be exposed to direct sunlight.
  • ARADUR® 5052 should be stored in a dry place, in the sealed original container, away from heat and humidity, at temperatures between +2°C and +40°C (+35.6°F and +104°F). Under these storage conditions, the shelf life is 3 years. The product should not be exposed to direct sunlight.