Stress Relieved ASTM B563 vs. Stress Relieved 363 Molybdenum
Both stress relieved ASTM B563 and stress relieved 363 molybdenum 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 363 molybdenum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 100 | |
| 310 |
| Elongation at Break, % | 9.1 | |
| 6.2 |
| Poisson's Ratio | 0.37 | |
| 0.31 |
| Shear Modulus, GPa | 37 | |
| 120 |
| Tensile Strength: Ultimate (UTS), MPa | 1050 | |
| 720 |
Thermal Properties
| Latent Heat of Fusion, J/g | 150 | |
| 370 |
| Melting Completion (Liquidus), °C | 1180 | |
| 2280 |
| Specific Heat Capacity, J/kg-K | 260 | |
| 250 |
| Thermal Expansion, µm/m-K | 14 | |
| 7.0 |
Otherwise Unclassified Properties
| Density, g/cm3 | 11 | |
| 10 |
Common Calculations
| Stiffness to Weight: Axial, points | 5.2 | |
| 17 |
| Stiffness to Weight: Bending, points | 14 | |
| 22 |
| Strength to Weight: Axial, points | 27 | |
| 20 |
| Strength to Weight: Bending, points | 21 | |
| 17 |
| Thermal Shock Resistance, points | 54 | |
| 24 |
Alloy Composition
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| Carbon (C), % | 0 | |
| 0.010 to 0.030 |
| Copper (Cu), % | 15.5 to 16.5 | |
| 0 |
| Iron (Fe), % | 0 | |
| 0 to 0.010 |
| Molybdenum (Mo), % | 0 | |
| 99.3 to 99.5 |
| Nickel (Ni), % | 0.8 to 1.2 | |
| 0 to 0.0020 |
| Nitrogen (N), % | 0 | |
| 0 to 0.0020 |
| Oxygen (O), % | 0 | |
| 0 to 0.0030 |
| Palladium (Pd), % | 43 to 45 | |
| 0 |
| Platinum (Pt), % | 0.8 to 1.2 | |
| 0 |
| Silicon (Si), % | 0 | |
| 0 to 0.010 |
| Silver (Ag), % | 37 to 39 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 0.4 to 0.55 |
| Zirconium (Zr), % | 0 | |
| 0.060 to 0.12 |
| Residuals, % | 0 to 0.4 | |
| 0 |