SAE-AISI H25 Steel vs. C99400 Brass
SAE-AISI H25 steel belongs to the iron alloys classification, while C99400 brass belongs to the copper alloys. There are 19 material properties with values for both materials. Properties with values for just one material (8, in this case) are not shown.
For each property being compared, the top bar is SAE-AISI H25 steel and the bottom bar is C99400 brass.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 200 | |
120 |
Poisson's Ratio | 0.29 | |
0.34 |
Shear Modulus, GPa | 79 | |
44 |
Tensile Strength: Ultimate (UTS), MPa | 710 to 1620 | |
460 to 550 |
Thermal Properties
Latent Heat of Fusion, J/g | 250 | |
230 |
Melting Completion (Liquidus), °C | 1750 | |
1070 |
Melting Onset (Solidus), °C | 1700 | |
1020 |
Specific Heat Capacity, J/kg-K | 420 | |
400 |
Thermal Expansion, µm/m-K | 12 | |
17 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 38 | |
30 |
Density, g/cm3 | 9.1 | |
8.7 |
Embodied Carbon, kg CO2/kg material | 6.2 | |
2.8 |
Embodied Energy, MJ/kg | 93 | |
45 |
Embodied Water, L/kg | 83 | |
310 |
Common Calculations
Stiffness to Weight: Axial, points | 12 | |
7.5 |
Stiffness to Weight: Bending, points | 22 | |
19 |
Strength to Weight: Axial, points | 22 to 50 | |
15 to 17 |
Strength to Weight: Bending, points | 20 to 34 | |
15 to 17 |
Thermal Shock Resistance, points | 22 to 49 | |
16 to 19 |
Alloy Composition
Aluminum (Al), % | 0 | |
0.5 to 2.0 |
Carbon (C), % | 0.22 to 0.32 | |
0 |
Chromium (Cr), % | 3.8 to 4.5 | |
0 |
Copper (Cu), % | 0 to 0.25 | |
83.5 to 96.5 |
Iron (Fe), % | 77.2 to 81.3 | |
1.0 to 3.0 |
Lead (Pb), % | 0 | |
0 to 0.25 |
Manganese (Mn), % | 0.15 to 0.4 | |
0 to 0.5 |
Nickel (Ni), % | 0 to 0.3 | |
1.0 to 3.5 |
Phosphorus (P), % | 0 to 0.030 | |
0 |
Silicon (Si), % | 0.15 to 0.4 | |
0.5 to 2.0 |
Sulfur (S), % | 0 to 0.030 | |
0 |
Tungsten (W), % | 14 to 16 | |
0 |
Vanadium (V), % | 0.4 to 0.6 | |
0 |
Zinc (Zn), % | 0 | |
0.5 to 5.0 |
Residuals, % | 0 | |
0 to 0.3 |