ASTM B817 Type I vs. EN 1.4945 Stainless Steel
ASTM B817 type I belongs to the titanium alloys classification, while EN 1.4945 stainless steel belongs to the iron 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 ASTM B817 type I and the bottom bar is EN 1.4945 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 100 | |
200 |
Elongation at Break, % | 4.0 to 13 | |
19 to 34 |
Fatigue Strength, MPa | 360 to 520 | |
230 to 350 |
Poisson's Ratio | 0.32 | |
0.28 |
Shear Modulus, GPa | 40 | |
77 |
Tensile Strength: Ultimate (UTS), MPa | 770 to 960 | |
640 to 740 |
Tensile Strength: Yield (Proof), MPa | 700 to 860 | |
290 to 550 |
Thermal Properties
Latent Heat of Fusion, J/g | 410 | |
290 |
Maximum Temperature: Mechanical, °C | 340 | |
920 |
Melting Completion (Liquidus), °C | 1600 | |
1490 |
Melting Onset (Solidus), °C | 1550 | |
1440 |
Specific Heat Capacity, J/kg-K | 560 | |
470 |
Thermal Conductivity, W/m-K | 7.1 | |
14 |
Thermal Expansion, µm/m-K | 9.6 | |
17 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 1.0 | |
2.9 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 2.0 | |
3.2 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 36 | |
30 |
Density, g/cm3 | 4.4 | |
8.1 |
Embodied Carbon, kg CO2/kg material | 38 | |
5.0 |
Embodied Energy, MJ/kg | 610 | |
73 |
Embodied Water, L/kg | 200 | |
150 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 30 to 120 | |
130 to 180 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 2310 to 3540 | |
210 to 760 |
Stiffness to Weight: Axial, points | 13 | |
14 |
Stiffness to Weight: Bending, points | 35 | |
24 |
Strength to Weight: Axial, points | 48 to 60 | |
22 to 25 |
Strength to Weight: Bending, points | 42 to 49 | |
20 to 22 |
Thermal Diffusivity, mm2/s | 2.9 | |
3.7 |
Thermal Shock Resistance, points | 54 to 68 | |
14 to 16 |
Alloy Composition
Aluminum (Al), % | 5.5 to 6.8 | |
0 |
Carbon (C), % | 0 to 0.1 | |
0.040 to 0.1 |
Chlorine (Cl), % | 0 to 0.2 | |
0 |
Chromium (Cr), % | 0 | |
15.5 to 17.5 |
Hydrogen (H), % | 0 to 0.015 | |
0 |
Iron (Fe), % | 0 to 0.4 | |
57.9 to 65.7 |
Manganese (Mn), % | 0 | |
0 to 1.5 |
Nickel (Ni), % | 0 | |
15.5 to 17.5 |
Niobium (Nb), % | 0 | |
0.4 to 1.2 |
Nitrogen (N), % | 0 to 0.040 | |
0.060 to 0.14 |
Oxygen (O), % | 0 to 0.3 | |
0 |
Phosphorus (P), % | 0 | |
0 to 0.035 |
Silicon (Si), % | 0 to 0.1 | |
0.3 to 0.6 |
Sodium (Na), % | 0 to 0.2 | |
0 |
Sulfur (S), % | 0 | |
0 to 0.015 |
Titanium (Ti), % | 87 to 91 | |
0 |
Tungsten (W), % | 0 | |
2.5 to 3.5 |
Vanadium (V), % | 3.5 to 4.5 | |
0 |
Residuals, % | 0 to 0.4 | |
0 |