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Permabond Engineering Adhesives LtdEpoxy Adhesives (1-K & 2-K)

PERMABOND ET515

Aerospace-Star — Permabond-recommended epoxy for aircraft seat trays, highly flexible with 100–150 N/25 mm peel resistance.

Chemical Group (A)
Epoxy resin
Color (A)
Colorless
Specific gravity (A)
1.1
Chemical Group (B)
Amine hardener

CHF 0.00 / ml
  • Manufacturer
  • Brand
  • Container
  • Chemical Group (A)
  • Color (A)
  • Viscosity 20rpm (A)
  • Specific gravity (A)
  • Chemical Group (B)
  • Color (B)
  • Viscosity 20rpm (B)
  • Specific Gravity (B)
  • Country of origin
  • Operating temperature (°C)
  • Mixing Ratio
  • Color
  • Viscosity (adhesives)
  • Hardness (Shore D)
  • Storage Temperature (°C)
  • Maximum gap fill (mm)
  • Pot Life at 23°C
  • Functional Strength
  • UFI Part A
  • UFI Part B
  • TG Value
  • Dielectric strength
  • Steel
  • Glass/ Polyester
  • Glass/ Epoxy
  • Carbon fiber
  • Peel resistance (aluminum) (ISO 4578)
  • Elongation at break (elasticity) (ISO37)
  • TG Value
  • Dielectric strength
  • Thermal conductivity
Your selection PERMABOND ET515 49-515.KT.ML050
General terms and conditions of business

Internal reference: 49-515.KT.ML050
HS code: 3506.9190000

PERMABOND ET515 Sample Offer

Technical Data

Typical values, not a specification. The technical data sheet (TDS) is binding.

Product Information

Manufacturer
Permabond Engineering Adhesives Ltd
Brand
Permabond
Container
50 ml
Country of origin
Italy
Mixing Ratio
1:1

Physical Properties A

Chemical Group (A)
Epoxy resin
Color (A)
Colorless
Viscosity 20rpm (A)
10000-20000
Specific gravity (A)
1.1
UFI Part A
0830-50Q0-D006-TXAD

Physical Properties B

Chemical Group (B)
Amine hardener
Color (B)
Colorless
Viscosity 20rpm (B)
14000-24000
Specific Gravity (B)
1.1
UFI Part B
XC30-P0DD-P00Q-F8WF

Performance at Full Cure

Dielectric strength
15-25 kV/mm
Peel resistance (aluminum) (ISO 4578)
70-90 N/25mm
Elongation at break (elasticity) (ISO37)
20-40%
Dielectric strength
15-25 kV/mm
Thermal conductivity
0.3 W/(mK)

Bonding Properties

Functional Strength
24 hours

Physical Properties

Color
colorless
Viscosity (adhesives)
12000-22000

Curing values

Maximum gap fill (mm)
2
Pot Life at 23°C
10-20 minutes

Mechanical properties

Hardness (Shore D)
30-50

Shear strength ISO 4587 in N/mm²

Steel
8 - 12 N/mm²
Glass/ Polyester
3-5 N/mm²
Glass/ Epoxy
4-6 N/mm²
Carbon fiber
4-6 N/mm²

Thermal Properties

Operating temperature (°C)
-55 to +100
Storage Temperature (°C)
5-25

Features

TG Value
+50-60°C
TG Value
20-40%
Keywords
  • Metal
  • Wood
  • Composite Materials
  • Pictogram

Product Description

Permabond ET515 is a highly flexible 2K epoxy specifically for bonding different materials (composite, metal, plastic) — with exceptional flexibility, high peel resistance and aerospace suitability for aircraft seat trays.

With an elongation at break of 20–40% and a temperature difference (Tg) of +20 °C, ET515 is significantly more flexible than standard epoxies—this flexibility buffers thermal expansion and contraction between dissimilar materials (such as carbon fiber to aluminum). Its peel strength of 100–150 N/25 mm is a top value for industrial structures.

The official Permabond recommendation for bonding aircraft seat trays underscores its suitability for aerospace applications. ET515 bonds steel (8–12 N/mm²), aluminum (9–12 N/mm²), carbon fiber (8–12 N/mm²), polyester GRP, epoxy FRP, and polycarbonate (substrate failure). The 2 mm gap filling accommodates large tolerances.

AEROSPACE STAR

Aerospace epoxy for aircraft seat trays — Permabond ET515 is officially recommended by Permabond for bonding aircraft seat tray structures. Its combination of high flexibility (20–40% elongation at break) and peel strength (100–150 N/25 mm) makes it the premium choice for composite structural bonding with differing coefficients of thermal expansion.

Permabond ET515 in figures
100–150
N/25 mm peel resistance
20–40 %
Elongation at break
Aerospace
Aircraft seats
1:1
Mixture 2 mm Gap

What distinguishes Permabond ET515

Aerospace suitability
Aircraft Seat Trays — Permabond-recommended for aircraft interiors.
Highly flexible
20–40% elongation at break — buffers thermal stresses between dissimilar materials.
Highest peel resistance
100–150 N/25 mm — peak value for 2K epoxies.
Multi-Substrate
Steel, aluminum, CFRP, GFRP, polycarbonate — all in one application.
2 mm gap filling
Even large tolerances can be covered.
Full cure at room temperature
No heat step — suitable for temperature-sensitive composites.

What is Permabond ET515 used for?

Aircraft Seat Trays
Permabond is recommended for use as an airplane seat cushion.
Composite structural bonding
CFRP and GFRP components in aerospace, sporting goods, and mechanical engineering.
Multi-material bonding
Components with different thermal expansion rates.
Structures subjected to shock and vibration
High peel resistance for dynamic loads.
Model making and prototyping
Composite constructions with weight requirements.

Processing

1
Clean surfaces
Bonding surfaces must be clean, dry, and free of grease. Degrease with Permabond Cleaner A or a solvent (acetone, isopropanol). Lightly sand aluminum and copper to remove oxide layers.
2
Mix components A + B
For twin cartridges: attach mixing nozzle, press evenly (1:1 by volume mixing ratio). For larger containers: weigh resin and hardener in the correct ratio and mix thoroughly until no streaks are visible. Avoid air entrapment.
3
Apply adhesive + join components
Apply the mixed adhesive to a bonding surface within the pot life (10–20 minutes @ 23 °C). Join components with sufficient pressure to ensure the adhesive spreads over the entire bonding surface.
4
Fix components during curing
Use a clamping device or clamp to ensure the components do not move during curing. Wait for handling strength and functional strength according to the TDS.
5
Full cure at room temperature
Final strength is typically reached after 72 hours at 23 °C. Increasing the temperature by 8 °C halves the curing time; lower temperatures slow down the process. If required, optional post-curing at 60–80 °C for maximum strength.
Data Sheets & Safety Data Sheet
Complete TDS and SDS in DE, EN, FR — view or download directly.
To the documents →

Recommended accessories


Important Notes

Important Notes
Before bonding, degrease surfaces with Permabond Cleaner A. Lightly sand aluminum for maximum adhesion. Test compatibility with thermoplastic substrates. Full curing takes 72 hours at 23 °C — higher temperatures accelerate curing.
Storage
Store at 5 to 25 °C. Keep 2K epoxy components in closed packaging — especially protect the hardener from moisture.

Which Permabond 2K epoxy for which application?

Permabond ET515 in direct comparison with related products of the ET series.

Permabond ET515
Current Product
Permabond ET514 →Permabond ET5422 →Permabond ET5441 →
Application / PropertyHighly flexible 2K epoxy 1:1 — Aerospace, Composite, Multi-MaHigher strength, less flexibleHighest strengthUL94, thermally conductive
Mixing ratio1:1 by volume1:1100:442:1
Pot life10–20 minutes @ 23 °C30–50 min——
Steel shear strength8–12 N/mm²20–30 N/mm²22–26 N/mm²20–25 N/mm²
Carbon fiber8–12 N/mm²—20–30 N/mm² Carbon25–30 N/mm²

Frequently asked questions about Permabond ET515

Practical application and design questions — answered by SILITECH.

Highly flexible aerospace epoxy 1:1 — for aircraft seat trays, composite structural bonding, and maximum peel resistance. This 2-component epoxy is mixed in a 1:1 volume ratio and offers a pot life of 10–20 minutes @ 23 °C.

Mix both components in a 1:1 ratio by volume — use the mixing nozzle for dual cartridges, weigh precisely for larger containers. Apply within the pot life (10–20 minutes @ 23 °C) and join components. Full curing typically occurs after 72 hours at room temperature.

The pot life of Permabond ET515 is typically 10–20 minutes at 23 °C. Higher temperatures shorten, lower temperatures lengthen the pot life. Mixing quantities above approximately 100 g may gel more quickly due to an exothermic reaction.

Permabond ET515 reliably bonds: Steel: 8–12 N/mm²; Aluminum: 9–12 N/mm²; Stainless steel: 6–9 N/mm²; Carbon fiber: 8–12 N/mm²; Polyester-GRP: 3–5 N/mm²; Epoxy-GRP: 4–6 N/mm²; Polycarbonate: >5 N/mm² (substrate failure). For thermoplastic substrates, test compatibility before series production.

Permabond ET515 is approved according to: Aerospace Aircraft Seat Tray Bonding (Permabond-confirmed). Compliance letters and detailed certificates are available from Permabond/SILITECH.

Permabond ET515 is a highly flexible 2-component epoxy 1:1 — for aerospace, composite, and multi-material applications (1:1 volume mix, 10–20 minutes pot life @ 23 °C). Permabond ET514 is a high-strength 1:1 epoxy (1:1, 30–50 min pot life) — higher strength, less flexible.

From the Permabond 2K epoxy range, select according to application, mixing ratio, and strength requirements: Permabond ET515 (Highly flexible 2K epoxy 1:1 — Aerospace, Composite, Multi-material); Permabond ET514 (High strength 1:1); Permabond ET5422 (Premium 100:44); Permabond ET5441 (Thermally conductive 2:1). For aerospace applications, see ET515 (Aircraft Seat Trays); for food applications, see ET5162 (EU 10/2011 + FDA); for thermal conductivity/fire protection, see ET5441 (UL94-V0).