EN 573-3 Grade 3.4365 H13 Aluminum Alloy – High Strength & Corrosion Resistance
DIN 3.4365 is a high-strength alloy that offers good stress-corrosion cracking resistance. Known as a mainstay in the aerospace industry since it was introduced, Aluminum 7075 brings moderate toughness as well as an excellent strength-to-weight ratio. It is also important to note that at sub-zero temperatures Aluminum 7075 increases in strength.
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Quantity: 1 PCSProperties
General
| Property | Value | Condition | Related Standards |
|---|---|---|---|
Density | 2.8 g/cm³ | H13 | EN 573-3, EN 1301 |
Mechanical
| Property | Value | Condition | Related Standards | Comment |
|---|---|---|---|---|
Elastic modulus | 72.0 GPa | H13 | EN 573-3, EN 1301 | |
Elongation | 2.5 % | H13 | EN 573-3, EN 1301 | |
Plane-Strain Fracture Toughnes | 22.0 - 35.0 MPa·√m | Typical for Wrought 7000 Series Aluminium | ||
Poisson's ratio | 0.33 [-] | Typical for Wrought 7000 Series Aluminium | ||
Shear modulus | 27.1 GPa | H13 | EN 573-3, EN 1301 | |
Tensile strength | 230.0 - 310.0 MPa | H13 | EN 573-3, EN 1301 |
Thermal
| Property | Temperature | Value | Condition | Related Standards |
|---|---|---|---|---|
Coefficient of thermal expansion | -50 °C | 2.16e-05 1/K | H13 | EN 573-3, EN 1301 |
20 °C | 2.16e-05 1/K | H13 | EN 573-3, EN 1301 | |
20 °C | 2.3399999999999996e-05 1/K | H13 | EN 573-3, EN 1301 | |
20 °C | 2.43e-05 1/K | H13 | EN 573-3, EN 1301 | |
20 °C | 2.52e-05 1/K | H13 | EN 573-3, EN 1301 | |
100 °C | 2.3399999999999996e-05 1/K | H13 | EN 573-3, EN 1301 | |
200 °C | 2.43e-05 1/K | H13 | EN 573-3, EN 1301 | |
300 °C | 2.52e-05 1/K | H13 | EN 573-3, EN 1301 | |
Melting point | 480.0 - 640.0 °C | H13 | EN 573-3, EN 1301 | |
Specific heat capacity | 862.0 J/(kg·K) | H13 | EN 573-3, EN 1301 | |
Thermal conductivity | 130.0 - 160.0 W/(m·K) | H13 | EN 573-3, EN 1301 |
Electrical
| Property | Value | Condition | Related Standards |
|---|---|---|---|
Electrical conductivity | 19000000.0 - 23000000.0 S/m | H13 | EN 573-3, EN 1301 |
Electrical resistivity | 4.35e-08 - 5.26e-08 Ω·m | H13 | EN 573-3, EN 1301 |
Chemical properties
| Property | Value | Condition | Related Standards |
|---|---|---|---|
Chromium | 0.18 - 0.28 % | H13 | EN 573-3, EN 1301 |
Copper | 1.2 - 2.0 % | H13 | EN 573-3, EN 1301 |
Iron | 0.50 % | H13 | EN 573-3, EN 1301 |
Magnesium | 2.1 - 2.9 % | H13 | EN 573-3, EN 1301 |
Manganese | 0.3 % | H13 | EN 573-3, EN 1301 |
Silicon | 0.4 % | H13 | EN 573-3, EN 1301 |
Titanium | 0.2 % | H13 | EN 573-3, EN 1301 |
Zinc | 5.1 - 6.1 % | H13 | EN 573-3, EN 1301 |
Technological properties
| Property | ||
|---|---|---|
| Anodizing | decorative: not suitable, Protective: acceptable | |
| Brazing | hard brazing (with flux/ without flux): not suitable / not suitable, friction soldering: not suitable, soft brazing with flux: not suitable | |
| Corrosion properties | Seawater: sufficient to poor, weathering: sufficient to poor | |
| Workability | Bending / Spinning (cold): sufficient (O) / not suitable, Impact extrusion (cold): not suitable, Deep drawing / upsetting (Condition) not suitable / not suitable | |
Metal
- EN 573-3 Grade 3.4365 O3 Aluminum 7075 – High-Strength Aerospace Alloy
- High-Strength AA 7075 H13 Aluminum Alloy – Aerospace Grade
- EN 573-3 Grade AW-3003 H13: Premium Aluminum Alloy with Superior Corrosion Resistance
- EN 573-3 Grade 3.4365 H18 – High‑Strength 7075 Aluminum Alloy
- High-Strength DIN 3.4365 (Al 7075) – Aerospace-Grade T652 Alloy
- EN 573-3 Grade 3.4365 T732 – High-Strength Aluminum 7075 Alloy for Aerospace
- EN 573-3 Grade 3.4365 T81 – High-Strength Aluminum Alloy for Aerospace
- EN 573-3 Grade 3.4365 T7352: High-Strength Aluminum Alloy for Aerospace Applications
- EN 573-3 Grade 3.4365 T76 Aluminum 7075 – High Strength, Corrosion‑Resistant Alloy
- EN 573-3 Grade 3.4365 T7651 – High-Strength Aluminum 7075 Alloy for Aerospace Applications