Stress Relieved ASTM B563 vs. Stress Relieved R05400 Tantalum
Both stress relieved ASTM B563 and stress relieved R05400 tantalum are otherwise unclassified metals. Both are furnished in the stress relieved condition. There are 15 material properties with values for both materials. Properties with values for just one material (11, in this case) are not shown.
For each property being compared, the top bar is stress relieved ASTM B563 and the bottom bar is stress relieved R05400 tantalum.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 100 | |
190 |
Elongation at Break, % | 9.1 | |
5.7 |
Poisson's Ratio | 0.37 | |
0.34 |
Shear Modulus, GPa | 37 | |
69 |
Tensile Strength: Ultimate (UTS), MPa | 1050 | |
430 |
Thermal Properties
Latent Heat of Fusion, J/g | 150 | |
140 |
Melting Completion (Liquidus), °C | 1180 | |
3020 |
Specific Heat Capacity, J/kg-K | 260 | |
140 |
Thermal Expansion, µm/m-K | 14 | |
6.5 |
Otherwise Unclassified Properties
Density, g/cm3 | 11 | |
17 |
Common Calculations
Stiffness to Weight: Axial, points | 5.2 | |
6.2 |
Stiffness to Weight: Bending, points | 14 | |
11 |
Strength to Weight: Axial, points | 27 | |
7.2 |
Strength to Weight: Bending, points | 21 | |
7.6 |
Thermal Shock Resistance, points | 54 | |
26 |
Alloy Composition
Carbon (C), % | 0 | |
0 to 0.010 |
Copper (Cu), % | 15.5 to 16.5 | |
0 |
Hydrogen (H), % | 0 | |
0 to 0.0015 |
Iron (Fe), % | 0 | |
0 to 0.010 |
Molybdenum (Mo), % | 0 | |
0 to 0.020 |
Nickel (Ni), % | 0.8 to 1.2 | |
0 to 0.010 |
Niobium (Nb), % | 0 | |
0 to 0.1 |
Nitrogen (N), % | 0 | |
0 to 0.010 |
Oxygen (O), % | 0 | |
0 to 0.030 |
Palladium (Pd), % | 43 to 45 | |
0 |
Platinum (Pt), % | 0.8 to 1.2 | |
0 |
Silicon (Si), % | 0 | |
0 to 0.0050 |
Silver (Ag), % | 37 to 39 | |
0 |
Tantalum (Ta), % | 0 | |
99.7 to 100 |
Titanium (Ti), % | 0 | |
0 to 0.010 |
Tungsten (W), % | 0 | |
0 to 0.050 |
Residuals, % | 0 to 0.4 | |
0 |