A medium strength aerospace aluminium alloy with, depending upon temper, Yield Strength of up to 35 ksi (240 MPa) and Tensile Strength of 42 ksi (290 MPa)
SAE AMS QQ-A-250/11 Alloy QQ A 250/11 |
|
---|---|
Chemical Element | % Present |
Aluminium (Al) | balance |
Other (Each) | 0.05 max |
Manganese (Mn) | 0.15 max |
Titanium (Ti) | 0.15 max |
Others (Total) | 0.15 max |
Zinc (Zn) | 0.25 max |
Chromium (Cr) | 0.04 - 0.35 |
Copper (Cu) | 0.15 - 0.4 |
Iron (Fe) | 0.7 max |
Silicon (Si) | 0.4 - 0.8 |
Magnesium (Mg) | 0.8 - 1.2 |
Aluminium alloy QQ-A-250/11 has similarities to the following standard designations and specifications but may not be a direct equivalent:
Alloy 6061, UNS A96061, ASTM B209, AMS 4026, AMS 4027
Alloy QQ-A-250/11 is supplied in a wide range of tempers:
Alloy QQ-A-250/11 is supplied in plate and sheet
Physical Property | Value |
---|---|
Density | 2.63 g/cm³ |
Melting Point | 650 °C |
Thermal Expansion | 23.3 x10^-6 /K |
Modulus of Elasticity | 70 GPa |
Thermal Conductivity | 180 W/m.K |
Electrical Resistivity | 46.5 % IACS |
Mechanical Properties shown are for '0' temper
Thickness (mm) | Proof Strength (Min) | Tensile Strength (Min) | Elongation % (Min) |
Over 0.2 up to & incl. 0.5 | 83 | 152 | 14 |
Over 0.5 up to & incl. 3.2 | 83 | 152 | 16 |
Over 3.2 up to & incl. 12.8 | 83 | 152 | 18 |