UNS R58153: Metastable‑Beta Alloy for Aerospace Sheet Metal, Foils, and Castings
UNS R58153 is a metastable-Beta Alloy is used primarily in sheet metal form. It is age-hardenable and highly cold-formable. It can be produced as foil and is an excellent alloy for castings. For aerospace applications, this grade is often specified as AMS 4914.
Properties
General
| Property | Value | Shape |
|---|---|---|
Density | 4.76 g/cm³ | Sheet, Plate |
Dimension
| Property | Value | Shape |
|---|---|---|
Length | 1500 mm | Sheet, Plate |
5000 mm | Sheet | |
6500 mm | Plate | |
Width | 400 mm | Sheet |
600 mm | Plate | |
1524 mm | Sheet | |
1600 mm | Plate |
valueMetaData
| Property | Value |
|---|
Mechanical
| Property | Value | Shape |
|---|---|---|
Elastic modulus | 82.0 GPa | Sheet, Plate |
Elongation | 22.0 % | Sheet, Plate |
Hardness, Rockwell B | 95.0 | Sheet, Plate |
Poisson's ratio | 0.33 [-] | Sheet, Plate |
Shear modulus | 30.8 GPa | Sheet, Plate |
Tensile strength | 790.0 MPa | Sheet, Plate |
Yield strength | 770.0 MPa | Sheet, Plate |
Thermal
| Property | Value | Shape | Comment |
|---|---|---|---|
Coefficient of thermal expansion | 7.099999999999997e-06 - 9.699999999999999e-06 1/K | Typical for Titanium Beta Alloy | |
Melting point | 1550.0 - 1815.0 °C | Typical for Titanium Beta Alloy | |
Specific heat capacity | 490.0 - 580.0 J/(kg·K) | Typical for Titanium Beta Alloy | |
Thermal conductivity | 8.08 W/(m·K) | Sheet, Plate |
Chemical properties
| Property | Value | Shape |
|---|---|---|
Aluminium | 3.0 | Sheet, Plate |
Hydrogen | 3.0 % | Sheet, Plate |
Tin | 3.0 | Sheet, Plate |
Vanadium | 15.0 | Sheet, Plate |
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