A very high strength aerospace aluminium alloy with, depending upon temper, Yield Strength of 24-68 ksi (165 - 465 MPa) and Tensile Strength of 40-78 ksi (275 - 540 MPa).
This alloy is used where high strength is required and where good resistance to general corrosion is NOT important.
SAE AMS QQ-A-200/11 Alloy QQ A 200/11 |
|
---|---|
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-200/11 has similarities to the following standard designations and specifications but may not be a direct equivalent:
AMS 4166, AMS 4168, AMS 4169
Alloy QQ-A-200/11 is supplied in a wide range of tempers:
Alloy QQ-A-200/11 T6511 is supplied in extruded bar
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 |
These Mechanical Properties are for Bar in the T6511 temper
Diameter (mm) | Proof Strength (Min) | Tensile Strength (Min) | Elongation % (Min) |
Up to & incl. 6.3 | 482 | 538 | 7 |
Over 6.3 up to & incl. 12.7 | 503 | 558 | 7 |
Over 12.7 up to & incl. 76.2 | 496 | 558 | 7 |
Over 76.2 up to & incl. 114 | 489 | 558 | 7 |
Over 114 up to & incl. 127 | 469 | 538 | 6 |