R30556 Alloy vs. S82013 Stainless Steel
Both R30556 alloy and S82013 stainless steel are iron alloys. Both are furnished in the annealed condition. They have 53% of their average alloy composition in common. There are 32 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown.
For each property being compared, the top bar is R30556 alloy and the bottom bar is S82013 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 210 | |
200 |
Elongation at Break, % | 45 | |
34 |
Fatigue Strength, MPa | 320 | |
400 |
Poisson's Ratio | 0.28 | |
0.28 |
Shear Modulus, GPa | 81 | |
78 |
Shear Strength, MPa | 550 | |
470 |
Tensile Strength: Ultimate (UTS), MPa | 780 | |
710 |
Tensile Strength: Yield (Proof), MPa | 350 | |
500 |
Thermal Properties
Latent Heat of Fusion, J/g | 300 | |
290 |
Maximum Temperature: Corrosion, °C | 450 | |
430 |
Maximum Temperature: Mechanical, °C | 1100 | |
970 |
Melting Completion (Liquidus), °C | 1420 | |
1420 |
Melting Onset (Solidus), °C | 1330 | |
1380 |
Specific Heat Capacity, J/kg-K | 450 | |
480 |
Thermal Conductivity, W/m-K | 11 | |
15 |
Thermal Expansion, µm/m-K | 15 | |
13 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 1.8 | |
2.2 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 1.9 | |
2.6 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 70 | |
11 |
Density, g/cm3 | 8.4 | |
7.7 |
Embodied Carbon, kg CO2/kg material | 8.7 | |
2.4 |
Embodied Energy, MJ/kg | 130 | |
34 |
Embodied Water, L/kg | 300 | |
140 |
Common Calculations
PREN (Pitting Resistance) | 40 | |
25 |
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 290 | |
220 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 290 | |
640 |
Stiffness to Weight: Axial, points | 14 | |
14 |
Stiffness to Weight: Bending, points | 23 | |
25 |
Strength to Weight: Axial, points | 26 | |
26 |
Strength to Weight: Bending, points | 22 | |
23 |
Thermal Diffusivity, mm2/s | 2.9 | |
4.0 |
Thermal Shock Resistance, points | 18 | |
20 |
Alloy Composition
Aluminum (Al), % | 0.1 to 0.5 | |
0 |
Boron (B), % | 0 to 0.020 | |
0 |
Carbon (C), % | 0.050 to 0.15 | |
0 to 0.060 |
Chromium (Cr), % | 21 to 23 | |
19.5 to 22 |
Cobalt (Co), % | 16 to 21 | |
0 |
Copper (Cu), % | 0 | |
0.2 to 1.2 |
Iron (Fe), % | 20.4 to 38.2 | |
70.5 to 77.1 |
Lanthanum (La), % | 0.0050 to 0.1 | |
0 |
Manganese (Mn), % | 0.5 to 2.0 | |
2.5 to 3.5 |
Molybdenum (Mo), % | 2.5 to 4.0 | |
0 |
Nickel (Ni), % | 19 to 22.5 | |
0.5 to 1.5 |
Niobium (Nb), % | 0 to 0.3 | |
0 |
Nitrogen (N), % | 0.1 to 0.3 | |
0.2 to 0.3 |
Phosphorus (P), % | 0 to 0.040 | |
0 to 0.040 |
Silicon (Si), % | 0.2 to 0.8 | |
0 to 0.9 |
Sulfur (S), % | 0 to 0.015 | |
0 to 0.030 |
Tantalum (Ta), % | 0.3 to 1.3 | |
0 |
Tungsten (W), % | 2.0 to 3.5 | |
0 |
Zinc (Zn), % | 0.0010 to 0.1 | |
0 |