DIN 1725-1 Grade 3.4365 T5 – High‑Strength 7075 Aluminum Alloy for Aerospace
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.
Additional services: Cuttings, Parts from drawingsSTEEL SCOUT
DISTRIBUTOR
Information and services
Quantity: 1 PCSProperties
General
| Property | Temperature | Value | Condition | Related Standards | Shape |
|---|---|---|---|---|---|
Density | 20.0 °C | 2.8 g/cm³ | T5 | DIN 1725-1, EN 573-3, EN 573-4, WL 3.4364-1 | Forging |
Mechanical
| Property | Temperature | Value | Condition | Related Standards | Shape | Comment |
|---|---|---|---|---|---|---|
Elastic modulus | 20.0 °C | 70.0 - 73.0 GPa | T5 | DIN 1725-1, EN 573-3, EN 573-4, WL 3.4364-1 | Forging | |
Elongation | 20.0 °C | 3.0 % | T5 | DIN 1725-1, EN 573-3, EN 573-4, WL 3.4364-1 | Forging | |
20.0 °C | 4.0 % | T5 | DIN 1725-1, EN 573-3, EN 573-4, WL 3.4364-1 | Forging | ||
20.0 °C | 6.0 % | T5 | DIN 1725-1, EN 573-3, EN 573-4, WL 3.4364-1 | Forging | ||
Hardness, Brinell | 20.0 °C | 115.0 [-] | T5 | DIN 1725-1, EN 573-3, EN 573-4, WL 3.4364-1 | Forging | |
20.0 °C | 120.0 [-] | T5 | DIN 1725-1, EN 573-3, EN 573-4, WL 3.4364-1 | Forging | ||
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 | 20.0 °C | 25.0 - 27.0 GPa | T5 | DIN 1725-1, EN 573-3, EN 573-4, WL 3.4364-1 | Forging | |
Tensile strength | 20.0 °C | 410.0 MPa | T5 | DIN 1725-1, EN 573-3, EN 573-4, WL 3.4364-1 | Forging | |
20.0 °C | 420.0 MPa | T5 | DIN 1725-1, EN 573-3, EN 573-4, WL 3.4364-1 | Forging | ||
20.0 °C | 440.0 MPa | T5 | DIN 1725-1, EN 573-3, EN 573-4, WL 3.4364-1 | Forging | ||
20.0 °C | 450.0 MPa | T5 | DIN 1725-1, EN 573-3, EN 573-4, WL 3.4364-1 | Forging |
Thermal
| Property | Temperature | Value | Condition | Related Standards | Shape | Comment |
|---|---|---|---|---|---|---|
Coefficient of thermal expansion | -50.0 °C | 2.16e-05 1/K | T5 | DIN 1725-1, EN 573-3, EN 573-4, WL 3.4364-1 | Forging | |
100.0 °C | 2.34e-05 1/K | T5 | DIN 1725-1, EN 573-3, EN 573-4, WL 3.4364-1 | Forging | ||
200.0 °C | 2.43e-05 1/K | T5 | DIN 1725-1, EN 573-3, EN 573-4, WL 3.4364-1 | Forging | ||
300.0 °C | 2.52e-05 1/K | T5 | DIN 1725-1, EN 573-3, EN 573-4, WL 3.4364-1 | Forging | ||
Melting point | 465.0 - 655.0 °C | Typical for Wrought 7000 Series Aluminium | ||||
Specific heat capacity | 20.0 °C | 862.0 J/(kg·K) | T5 | DIN 1725-1, EN 573-3, EN 573-4, WL 3.4364-1 | Forging | |
Thermal conductivity | 20.0 °C | 130.0 - 160.0 W/(m·K) | T5 | DIN 1725-1, EN 573-3, EN 573-4, WL 3.4364-1 | Forging |
Electrical
| Property | Temperature | Value | Condition | Related Standards | Shape | Comment |
|---|---|---|---|---|---|---|
Electrical conductivity | 20.0 °C | 19000000.0 - 23000000.0 S/m | T5 | DIN 1725-1, EN 573-3, EN 573-4, WL 3.4364-1 | Forging | |
Electrical resistivity | 2.9e-08 - 5.6e-08 Ω·m | Typical for Wrought 7000 Series Aluminium |
Chemical properties
| Property | Value | Condition | Related Standards | Shape |
|---|---|---|---|---|
Chromium | 0.18 - 0.28 % | T5 | DIN 1725-1, EN 573-3, EN 573-4, WL 3.4364-1 | Forging |
Copper | 1.2 - 2.0 % | T5 | DIN 1725-1, EN 573-3, EN 573-4, WL 3.4364-1 | Forging |
Iron | 0.5 | T5 | DIN 1725-1, EN 573-3, EN 573-4, WL 3.4364-1 | Forging |
Magnesium | 2.1 - 2.9 % | T5 | DIN 1725-1, EN 573-3, EN 573-4, WL 3.4364-1 | Forging |
Manganese | 0.3 | T5 | DIN 1725-1, EN 573-3, EN 573-4, WL 3.4364-1 | Forging |
Silicon | 0.4 | T5 | DIN 1725-1, EN 573-3, EN 573-4, WL 3.4364-1 | Forging |
Titanium | 0.2 | T5 | DIN 1725-1, EN 573-3, EN 573-4, WL 3.4364-1 | Forging |
Zinc | 5.1 - 6.1 % | T5 | DIN 1725-1, EN 573-3, EN 573-4, WL 3.4364-1 | Forging |
Technological properties
| Property | ||
|---|---|---|
| Brazing | Excellent | |
Metal
- DIN 1725-1 Grade 3.4365 F53 – High-Strength 7075 Aluminum for Aerospace
- DIN 1725‑1 Grade 3.4365 O – Premium High‑Strength Aluminum Alloy for Aerospace
- DIN 1725-1 Grade 3.4365 T792 – High-Strength 7075 Aluminum for Aerospace Applications
- DIN 1725-1 Grade 3.4365 T79511 – High-Strength 7075 Aluminum Alloy
- DIN 1725-1 Grade 3.4365 H14 – High‑Strength 7075 Aluminum Alloy for Aerospace
- DIN 1725-1 Grade 3.4365 T8 – High‑Strength 7075 Aluminum Alloy
- DIN 1725-1 Grade 3.4365 T73 – High‑Strength 7075 Aluminum Alloy
- DIN 1725-1 Grade 3.4365 T7351: High-Strength, Corrosion-Resistant Aluminum 7075 for Aerospace
- DIN 1725-1 Grade 3.4365 T73510 – Premium High‑Strength Aluminum 7075 Alloy
- DIN 1725-1 Grade 3.4365 T73511: Premium High-Strength Alloy for Aerospace Applications