S35500 Stainless Steel vs. ASTM B817 Type I
S35500 stainless steel belongs to the iron alloys classification, while ASTM B817 type I belongs to the titanium alloys. There are 29 material properties with values for both materials. Properties with values for just one material (5, in this case) are not shown.
For each property being compared, the top bar is S35500 stainless steel and the bottom bar is ASTM B817 type I.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 200 | |
100 |
Elongation at Break, % | 14 | |
4.0 to 13 |
Fatigue Strength, MPa | 690 to 730 | |
360 to 520 |
Poisson's Ratio | 0.28 | |
0.32 |
Shear Modulus, GPa | 78 | |
40 |
Tensile Strength: Ultimate (UTS), MPa | 1330 to 1490 | |
770 to 960 |
Tensile Strength: Yield (Proof), MPa | 1200 to 1280 | |
700 to 860 |
Thermal Properties
Latent Heat of Fusion, J/g | 280 | |
410 |
Maximum Temperature: Mechanical, °C | 870 | |
340 |
Melting Completion (Liquidus), °C | 1460 | |
1600 |
Melting Onset (Solidus), °C | 1420 | |
1550 |
Specific Heat Capacity, J/kg-K | 470 | |
560 |
Thermal Conductivity, W/m-K | 16 | |
7.1 |
Thermal Expansion, µm/m-K | 11 | |
9.6 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 2.2 | |
1.0 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 2.5 | |
2.0 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 16 | |
36 |
Density, g/cm3 | 7.8 | |
4.4 |
Embodied Carbon, kg CO2/kg material | 3.5 | |
38 |
Embodied Energy, MJ/kg | 47 | |
610 |
Embodied Water, L/kg | 130 | |
200 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 180 to 190 | |
30 to 120 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 3610 to 4100 | |
2310 to 3540 |
Stiffness to Weight: Axial, points | 14 | |
13 |
Stiffness to Weight: Bending, points | 25 | |
35 |
Strength to Weight: Axial, points | 47 to 53 | |
48 to 60 |
Strength to Weight: Bending, points | 34 to 37 | |
42 to 49 |
Thermal Diffusivity, mm2/s | 4.4 | |
2.9 |
Thermal Shock Resistance, points | 44 to 49 | |
54 to 68 |
Alloy Composition
Aluminum (Al), % | 0 | |
5.5 to 6.8 |
Carbon (C), % | 0.1 to 0.15 | |
0 to 0.1 |
Chlorine (Cl), % | 0 | |
0 to 0.2 |
Chromium (Cr), % | 15 to 16 | |
0 |
Hydrogen (H), % | 0 | |
0 to 0.015 |
Iron (Fe), % | 73.2 to 77.7 | |
0 to 0.4 |
Manganese (Mn), % | 0.5 to 1.3 | |
0 |
Molybdenum (Mo), % | 2.5 to 3.2 | |
0 |
Nickel (Ni), % | 4.0 to 5.0 | |
0 |
Niobium (Nb), % | 0.1 to 0.5 | |
0 |
Nitrogen (N), % | 0.070 to 0.13 | |
0 to 0.040 |
Oxygen (O), % | 0 | |
0 to 0.3 |
Phosphorus (P), % | 0 to 0.040 | |
0 |
Silicon (Si), % | 0 to 0.5 | |
0 to 0.1 |
Sodium (Na), % | 0 | |
0 to 0.2 |
Sulfur (S), % | 0 to 0.030 | |
0 |
Titanium (Ti), % | 0 | |
87 to 91 |
Vanadium (V), % | 0 | |
3.5 to 4.5 |
Residuals, % | 0 | |
0 to 0.4 |