A high strength aerospace aluminium alloy with, depending upon temper, Yield Strength of up to 54ksi (370 MPa) and Tensile Strength of up to 67 ksi (460 MPa)
Chemical Element | % Present |
---|---|
Aluminium (Al) | balance |
Other (Each) | 0.05 max |
Others (Total) | 0.15 max |
Titanium (Ti) | 0.2 max |
Chromium (Cr) | 0.18 - 0.28 |
Manganese (Mn) | 0.3 max |
Silicon (Si) | 0.4 max |
Iron (Fe) | 0.5 max |
Copper (Cu) | 1.2 - 2 |
Magnesium (Mg) | 2.1 - 2.9 |
Zinc (Zn) | 5.1 - 6.1 |
Aluminium alloy QQ-A-250/12 has similarities to the following standard designations and specifications:
AMS 4044, Alloy 7075, UNS A97075
Alloy QQ-A-250/12 is supplied in a wide range of tempers:
Alloy QQ-A-250/12 T7351 is supplied in sheet and plate
Physical Property | Value |
---|---|
Density | 2.81 g/cm³ |
Melting Point | 635 °C |
Thermal Expansion | 23.5 x10^-6 /K |
Modulus of Elasticity | 72 GPa |
Thermal Conductivity | 134-160 W/m.K |
Electrical Resistivity | 40 % IACS |
The Mechanical Properties given are for Plate in the T7351 temper
Thickness (mm) | Proof Strength (Min) | Tensile Strength (Min) | Elongation % (Min) |
Over 6.3 up to & incl. 25.4 | 393 | 476 | 7 |
Over 25.4 up to & incl. 50.8 | 393 | 476 | 6 |
Over 50.8 up to & incl. 63.5 | 359 | 455 | 6 |
Over 63.5 up to & incl. 76.2 | 338 | 441 | 6 |
Over 76.2 up to & incl. 88.9 | 338 | 434 | 6 |
Over 88.9 up to & incl. 101.6 | 331 | 421 | 6 |