Annealed SAE-AISI H25 vs. Annealed Nickel 201
Annealed SAE-AISI H25 belongs to the iron alloys classification, while annealed nickel 201 belongs to the nickel alloys. There are 22 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 annealed SAE-AISI H25 and the bottom bar is annealed nickel 201.
Metric UnitsUS Customary Units
Mechanical Properties
Brinell Hardness | 210 | |
110 |
Elastic (Young's, Tensile) Modulus, GPa | 200 | |
180 |
Poisson's Ratio | 0.29 | |
0.31 |
Shear Modulus, GPa | 79 | |
70 |
Tensile Strength: Ultimate (UTS), MPa | 710 | |
400 |
Thermal Properties
Latent Heat of Fusion, J/g | 250 | |
290 |
Melting Completion (Liquidus), °C | 1750 | |
1450 |
Melting Onset (Solidus), °C | 1700 | |
1440 |
Specific Heat Capacity, J/kg-K | 420 | |
440 |
Thermal Conductivity, W/m-K | 26 | |
78 |
Thermal Expansion, µm/m-K | 12 | |
13 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 38 | |
65 |
Density, g/cm3 | 9.1 | |
8.9 |
Embodied Carbon, kg CO2/kg material | 6.2 | |
11 |
Embodied Energy, MJ/kg | 93 | |
150 |
Embodied Water, L/kg | 83 | |
230 |
Common Calculations
Stiffness to Weight: Axial, points | 12 | |
11 |
Stiffness to Weight: Bending, points | 22 | |
21 |
Strength to Weight: Axial, points | 22 | |
12 |
Strength to Weight: Bending, points | 20 | |
13 |
Thermal Diffusivity, mm2/s | 6.7 | |
20 |
Thermal Shock Resistance, points | 22 | |
12 |
Alloy Composition
Carbon (C), % | 0.22 to 0.32 | |
0 to 0.020 |
Chromium (Cr), % | 3.8 to 4.5 | |
0 |
Copper (Cu), % | 0 to 0.25 | |
0 to 0.25 |
Iron (Fe), % | 77.2 to 81.3 | |
0 to 0.4 |
Manganese (Mn), % | 0.15 to 0.4 | |
0 to 0.35 |
Nickel (Ni), % | 0 to 0.3 | |
99 to 100 |
Phosphorus (P), % | 0 to 0.030 | |
0 |
Silicon (Si), % | 0.15 to 0.4 | |
0 to 0.35 |
Sulfur (S), % | 0 to 0.030 | |
0 to 0.010 |
Tungsten (W), % | 14 to 16 | |
0 |
Vanadium (V), % | 0.4 to 0.6 | |
0 |