A medium strength aerospace aluminium alloy with, depending upon temper, Yield Strength of 12-35 ksi (80 - 240 MPa) and Tensile Strength of 26-38 ksi (180 - 260 MPa).
This alloy is used where good strength combined with workability is required.
SAE AMS QQ-A-200/8 Alloy QQ A 200/8 |
|
---|---|
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-200/8 has similarities to the following standard designations and specifications but may not be a direct equivalent:
AMS 4150, AMS 4173
Alloy QQ-A-200/8 is supplied in a wide range of tempers:
Alloy QQ-A-200/8 is supplied in sheet, bar, rod, wire, tube and extruded sections:
Physical Property | Value |
---|---|
Density | 2.70 g/cm³ |
Melting Point | 650 °C |
Thermal Expansion | 23.4 x10^-6 /K |
Modulus of Elasticity | 70 GPa |
Thermal Conductivity | 166 W/m.K |
Electrical Resistivity | 0.040 x10^-6 Ω .m |
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 | 241 | 262 | 8 |
Over 6.3 | 241 | 262 | 10 |