Type 4 Magnetic Alloy vs. AISI 305 Stainless Steel
Type 4 magnetic alloy belongs to the nickel alloys classification, while AISI 305 stainless steel belongs to the iron alloys. They have a modest 26% of their average alloy composition in common, which, by itself, doesn't mean much. There are 28 material properties with values for both materials. Properties with values for just one material (7, in this case) are not shown.
For each property being compared, the top bar is Type 4 magnetic alloy and the bottom bar is AISI 305 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 200 |
| Elongation at Break, % | 2.0 to 40 | |
| 34 to 45 |
| Fatigue Strength, MPa | 220 to 400 | |
| 210 to 280 |
| Poisson's Ratio | 0.31 | |
| 0.28 |
| Shear Modulus, GPa | 73 | |
| 77 |
| Shear Strength, MPa | 420 to 630 | |
| 400 to 470 |
| Tensile Strength: Ultimate (UTS), MPa | 620 to 1100 | |
| 580 to 710 |
| Tensile Strength: Yield (Proof), MPa | 270 to 1040 | |
| 230 to 350 |
Thermal Properties
| Latent Heat of Fusion, J/g | 290 | |
| 290 |
| Maximum Temperature: Mechanical, °C | 900 | |
| 540 |
| Melting Completion (Liquidus), °C | 1420 | |
| 1450 |
| Melting Onset (Solidus), °C | 1370 | |
| 1400 |
| Specific Heat Capacity, J/kg-K | 440 | |
| 480 |
| Thermal Expansion, µm/m-K | 11 | |
| 17 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 2.9 | |
| 2.4 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 3.0 | |
| 2.7 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 60 | |
| 16 |
| Density, g/cm3 | 8.8 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 10 | |
| 3.2 |
| Embodied Energy, MJ/kg | 140 | |
| 45 |
| Embodied Water, L/kg | 210 | |
| 150 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 22 to 200 | |
| 200 to 210 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 190 to 2840 | |
| 130 to 320 |
| Stiffness to Weight: Axial, points | 12 | |
| 14 |
| Stiffness to Weight: Bending, points | 22 | |
| 25 |
| Strength to Weight: Axial, points | 19 to 35 | |
| 20 to 25 |
| Strength to Weight: Bending, points | 18 to 27 | |
| 20 to 23 |
| Thermal Shock Resistance, points | 21 to 37 | |
| 13 to 15 |
Alloy Composition
| Carbon (C), % | 0 to 0.050 | |
| 0 to 0.12 |
| Chromium (Cr), % | 0 to 0.3 | |
| 17 to 19 |
| Cobalt (Co), % | 0 to 0.5 | |
| 0 |
| Copper (Cu), % | 0 to 0.3 | |
| 0 |
| Iron (Fe), % | 9.5 to 17.5 | |
| 65.1 to 72.5 |
| Manganese (Mn), % | 0 to 0.8 | |
| 0 to 2.0 |
| Molybdenum (Mo), % | 3.5 to 6.0 | |
| 0 |
| Nickel (Ni), % | 79 to 82 | |
| 10.5 to 13 |
| Phosphorus (P), % | 0 to 0.010 | |
| 0 to 0.045 |
| Silicon (Si), % | 0 to 0.5 | |
| 0 to 0.75 |
| Sulfur (S), % | 0 to 0.020 | |
| 0 to 0.030 |