ASTM A369 Grade FP11 vs. 60Cr-40Ni Alloy
ASTM A369 grade FP11 belongs to the iron alloys classification, while 60Cr-40Ni alloy belongs to the otherwise unclassified metals. There are 19 material properties with values for both materials. Properties with values for just one material (13, in this case) are not shown.
For each property being compared, the top bar is ASTM A369 grade FP11 and the bottom bar is 60Cr-40Ni alloy.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 190 | |
220 |
Poisson's Ratio | 0.29 | |
0.25 |
Shear Modulus, GPa | 73 | |
87 |
Tensile Strength: Ultimate (UTS), MPa | 470 | |
870 |
Tensile Strength: Yield (Proof), MPa | 240 | |
660 |
Thermal Properties
Latent Heat of Fusion, J/g | 260 | |
370 |
Specific Heat Capacity, J/kg-K | 470 | |
490 |
Thermal Expansion, µm/m-K | 13 | |
16 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 2.9 | |
49 |
Density, g/cm3 | 7.8 | |
7.8 |
Embodied Carbon, kg CO2/kg material | 1.6 | |
7.4 |
Embodied Energy, MJ/kg | 21 | |
110 |
Embodied Water, L/kg | 52 | |
380 |
Common Calculations
Resilience: Unit (Modulus of Resilience), kJ/m3 | 150 | |
1000 |
Stiffness to Weight: Axial, points | 13 | |
16 |
Stiffness to Weight: Bending, points | 24 | |
26 |
Strength to Weight: Axial, points | 17 | |
31 |
Strength to Weight: Bending, points | 17 | |
26 |
Thermal Shock Resistance, points | 14 | |
18 |
Alloy Composition
Aluminum (Al), % | 0 | |
0 to 0.25 |
Carbon (C), % | 0.050 to 0.15 | |
0 to 0.1 |
Chromium (Cr), % | 1.0 to 1.5 | |
58 to 62 |
Iron (Fe), % | 96.1 to 97.7 | |
0 to 1.0 |
Manganese (Mn), % | 0.3 to 0.6 | |
0 to 0.3 |
Molybdenum (Mo), % | 0.44 to 0.65 | |
0 |
Nickel (Ni), % | 0 | |
34.5 to 42 |
Nitrogen (N), % | 0 | |
0 to 0.3 |
Phosphorus (P), % | 0 to 0.025 | |
0 to 0.020 |
Silicon (Si), % | 0.5 to 1.0 | |
0 to 1.0 |
Sulfur (S), % | 0 to 0.025 | |
0 to 0.020 |
Titanium (Ti), % | 0 | |
0 to 0.5 |