AISI 305 Stainless Steel vs. Grade 9 Titanium
AISI 305 stainless steel belongs to the iron alloys classification, while grade 9 titanium belongs to the titanium alloys. There are 30 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 AISI 305 stainless steel and the bottom bar is grade 9 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 200 | |
110 |
Elongation at Break, % | 34 to 45 | |
11 to 17 |
Fatigue Strength, MPa | 210 to 280 | |
330 to 480 |
Poisson's Ratio | 0.28 | |
0.32 |
Shear Modulus, GPa | 77 | |
40 |
Shear Strength, MPa | 400 to 470 | |
430 to 580 |
Tensile Strength: Ultimate (UTS), MPa | 580 to 710 | |
700 to 960 |
Tensile Strength: Yield (Proof), MPa | 230 to 350 | |
540 to 830 |
Thermal Properties
Latent Heat of Fusion, J/g | 290 | |
410 |
Maximum Temperature: Mechanical, °C | 540 | |
330 |
Melting Completion (Liquidus), °C | 1450 | |
1640 |
Melting Onset (Solidus), °C | 1400 | |
1590 |
Specific Heat Capacity, J/kg-K | 480 | |
550 |
Thermal Conductivity, W/m-K | 16 | |
8.1 |
Thermal Expansion, µm/m-K | 17 | |
9.1 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 2.4 | |
1.4 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 2.7 | |
2.7 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 16 | |
37 |
Density, g/cm3 | 7.8 | |
4.5 |
Embodied Carbon, kg CO2/kg material | 3.2 | |
36 |
Embodied Energy, MJ/kg | 45 | |
580 |
Embodied Water, L/kg | 150 | |
150 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 200 to 210 | |
89 to 110 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 130 to 320 | |
1380 to 3220 |
Stiffness to Weight: Axial, points | 14 | |
13 |
Stiffness to Weight: Bending, points | 25 | |
35 |
Strength to Weight: Axial, points | 20 to 25 | |
43 to 60 |
Strength to Weight: Bending, points | 20 to 23 | |
39 to 48 |
Thermal Diffusivity, mm2/s | 4.2 | |
3.3 |
Thermal Shock Resistance, points | 13 to 15 | |
52 to 71 |
Alloy Composition
Aluminum (Al), % | 0 | |
2.5 to 3.5 |
Carbon (C), % | 0 to 0.12 | |
0 to 0.080 |
Chromium (Cr), % | 17 to 19 | |
0 |
Hydrogen (H), % | 0 | |
0 to 0.015 |
Iron (Fe), % | 65.1 to 72.5 | |
0 to 0.25 |
Manganese (Mn), % | 0 to 2.0 | |
0 |
Nickel (Ni), % | 10.5 to 13 | |
0 |
Nitrogen (N), % | 0 | |
0 to 0.030 |
Oxygen (O), % | 0 | |
0 to 0.15 |
Phosphorus (P), % | 0 to 0.045 | |
0 |
Silicon (Si), % | 0 to 0.75 | |
0 |
Sulfur (S), % | 0 to 0.030 | |
0 |
Titanium (Ti), % | 0 | |
92.6 to 95.5 |
Vanadium (V), % | 0 | |
2.0 to 3.0 |
Residuals, % | 0 | |
0 to 0.4 |