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ASTM B817 Type I vs. WE54A Magnesium

ASTM B817 type I belongs to the titanium alloys classification, while WE54A magnesium belongs to the magnesium alloys. There are 29 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is ASTM B817 type I and the bottom bar is WE54A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 100
44
Elongation at Break, % 4.0 to 13
4.3 to 5.6
Fatigue Strength, MPa 360 to 520
98 to 130
Poisson's Ratio 0.32
0.29
Shear Modulus, GPa 40
17
Tensile Strength: Ultimate (UTS), MPa 770 to 960
270 to 300
Tensile Strength: Yield (Proof), MPa 700 to 860
180

Thermal Properties

Latent Heat of Fusion, J/g 410
330
Maximum Temperature: Mechanical, °C 340
170
Melting Completion (Liquidus), °C 1600
640
Melting Onset (Solidus), °C 1550
570
Specific Heat Capacity, J/kg-K 560
960
Thermal Conductivity, W/m-K 7.1
52
Thermal Expansion, µm/m-K 9.6
25

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.0
10
Electrical Conductivity: Equal Weight (Specific), % IACS 2.0
47

Otherwise Unclassified Properties

Base Metal Price, % relative 36
34
Density, g/cm3 4.4
1.9
Embodied Carbon, kg CO2/kg material 38
29
Embodied Energy, MJ/kg 610
260
Embodied Water, L/kg 200
900

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 30 to 120
10 to 14
Resilience: Unit (Modulus of Resilience), kJ/m3 2310 to 3540
360 to 380
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 35
62
Strength to Weight: Axial, points 48 to 60
39 to 43
Strength to Weight: Bending, points 42 to 49
49 to 51
Thermal Diffusivity, mm2/s 2.9
28
Thermal Shock Resistance, points 54 to 68
18 to 19

Alloy Composition


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Aluminum (Al), % 5.5 to 6.8
0
Carbon (C), % 0 to 0.1
0
Chlorine (Cl), % 0 to 0.2
0
Copper (Cu), % 0
0 to 0.030
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.4
0 to 0.010
Lithium (Li), % 0
0 to 0.2
Magnesium (Mg), % 0
88.7 to 93.4
Manganese (Mn), % 0
0 to 0.030
Nickel (Ni), % 0
0 to 0.0050
Nitrogen (N), % 0 to 0.040
0
Oxygen (O), % 0 to 0.3
0
Silicon (Si), % 0 to 0.1
0 to 0.010
Sodium (Na), % 0 to 0.2
0
Titanium (Ti), % 87 to 91
0
Unspecified Rare Earths, % 0
1.5 to 4.0
Vanadium (V), % 3.5 to 4.5
0
Yttrium (Y), % 0
4.8 to 5.5
Zinc (Zn), % 0
0 to 0.2
Zirconium (Zr), % 0
0.4 to 1.0
Residuals, % 0 to 0.4
0 to 0.3