S21904 Stainless Steel vs. ASTM B817 Type I
S21904 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 S21904 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, % | 17 to 51 | |
4.0 to 13 |
Fatigue Strength, MPa | 380 to 550 | |
360 to 520 |
Poisson's Ratio | 0.28 | |
0.32 |
Shear Modulus, GPa | 78 | |
40 |
Tensile Strength: Ultimate (UTS), MPa | 700 to 1000 | |
770 to 960 |
Tensile Strength: Yield (Proof), MPa | 390 to 910 | |
700 to 860 |
Thermal Properties
Latent Heat of Fusion, J/g | 290 | |
410 |
Maximum Temperature: Mechanical, °C | 980 | |
340 |
Melting Completion (Liquidus), °C | 1400 | |
1600 |
Melting Onset (Solidus), °C | 1350 | |
1550 |
Specific Heat Capacity, J/kg-K | 480 | |
560 |
Thermal Conductivity, W/m-K | 14 | |
7.1 |
Thermal Expansion, µm/m-K | 17 | |
9.6 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 2.5 | |
1.0 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 2.9 | |
2.0 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 15 | |
36 |
Density, g/cm3 | 7.7 | |
4.4 |
Embodied Carbon, kg CO2/kg material | 3.0 | |
38 |
Embodied Energy, MJ/kg | 43 | |
610 |
Embodied Water, L/kg | 160 | |
200 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 160 to 310 | |
30 to 120 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 380 to 2070 | |
2310 to 3540 |
Stiffness to Weight: Axial, points | 14 | |
13 |
Stiffness to Weight: Bending, points | 25 | |
35 |
Strength to Weight: Axial, points | 25 to 36 | |
48 to 60 |
Strength to Weight: Bending, points | 23 to 29 | |
42 to 49 |
Thermal Diffusivity, mm2/s | 3.8 | |
2.9 |
Thermal Shock Resistance, points | 15 to 21 | |
54 to 68 |
Alloy Composition
Aluminum (Al), % | 0 | |
5.5 to 6.8 |
Carbon (C), % | 0 to 0.040 | |
0 to 0.1 |
Chlorine (Cl), % | 0 | |
0 to 0.2 |
Chromium (Cr), % | 19 to 21.5 | |
0 |
Hydrogen (H), % | 0 | |
0 to 0.015 |
Iron (Fe), % | 59.5 to 67.4 | |
0 to 0.4 |
Manganese (Mn), % | 8.0 to 10 | |
0 |
Nickel (Ni), % | 5.5 to 7.5 | |
0 |
Nitrogen (N), % | 0.15 to 0.4 | |
0 to 0.040 |
Oxygen (O), % | 0 | |
0 to 0.3 |
Phosphorus (P), % | 0 to 0.045 | |
0 |
Silicon (Si), % | 0 to 1.0 | |
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 |