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ASTM B817 Type I vs. WE43A Magnesium

ASTM B817 type I belongs to the titanium alloys classification, while WE43A magnesium belongs to the magnesium alloys. There are 29 material properties with values for both materials. Properties with values for just one material (3, 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 WE43A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 100
44
Elongation at Break, % 4.0 to 13
5.2 to 5.4
Fatigue Strength, MPa 360 to 520
85 to 120
Poisson's Ratio 0.32
0.29
Shear Modulus, GPa 40
17
Tensile Strength: Ultimate (UTS), MPa 770 to 960
250 to 270
Tensile Strength: Yield (Proof), MPa 700 to 860
160 to 170

Thermal Properties

Latent Heat of Fusion, J/g 410
330
Maximum Temperature: Mechanical, °C 340
180
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
51
Thermal Expansion, µm/m-K 9.6
27

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.0
12
Electrical Conductivity: Equal Weight (Specific), % IACS 2.0
55

Otherwise Unclassified Properties

Base Metal Price, % relative 36
34
Density, g/cm3 4.4
1.9
Embodied Carbon, kg CO2/kg material 38
28
Embodied Energy, MJ/kg 610
250
Embodied Water, L/kg 200
910

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 30 to 120
12
Resilience: Unit (Modulus of Resilience), kJ/m3 2310 to 3540
280 to 310
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 35
61
Strength to Weight: Axial, points 48 to 60
36 to 39
Strength to Weight: Bending, points 42 to 49
46 to 48
Thermal Diffusivity, mm2/s 2.9
28
Thermal Shock Resistance, points 54 to 68
15 to 16

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
89.5 to 93.5
Manganese (Mn), % 0
0 to 0.15
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
2.4 to 4.4
Vanadium (V), % 3.5 to 4.5
0
Yttrium (Y), % 0
3.7 to 4.3
Zinc (Zn), % 0
0 to 0.2
Zirconium (Zr), % 0
0.4 to 1.0
Residuals, % 0 to 0.4
0 to 0.3