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ZK60A Magnesium vs. ASTM B817 Type I

ZK60A magnesium belongs to the magnesium 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 (2, 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 ZK60A magnesium and the bottom bar is ASTM B817 type I.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
100
Elongation at Break, % 4.5 to 9.9
4.0 to 13
Fatigue Strength, MPa 150 to 180
360 to 520
Poisson's Ratio 0.29
0.32
Shear Modulus, GPa 18
40
Tensile Strength: Ultimate (UTS), MPa 320 to 330
770 to 960
Tensile Strength: Yield (Proof), MPa 230 to 250
700 to 860

Thermal Properties

Latent Heat of Fusion, J/g 330
410
Maximum Temperature: Mechanical, °C 120
340
Melting Completion (Liquidus), °C 600
1600
Melting Onset (Solidus), °C 550
1550
Specific Heat Capacity, J/kg-K 960
560
Thermal Conductivity, W/m-K 120
7.1
Thermal Expansion, µm/m-K 26
9.6

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29 to 30
1.0
Electrical Conductivity: Equal Weight (Specific), % IACS 140
2.0

Otherwise Unclassified Properties

Base Metal Price, % relative 13
36
Density, g/cm3 1.9
4.4
Embodied Carbon, kg CO2/kg material 23
38
Embodied Energy, MJ/kg 160
610
Embodied Water, L/kg 940
200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 29
30 to 120
Resilience: Unit (Modulus of Resilience), kJ/m3 570 to 690
2310 to 3540
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 63
35
Strength to Weight: Axial, points 47 to 49
48 to 60
Strength to Weight: Bending, points 55 to 56
42 to 49
Thermal Diffusivity, mm2/s 66
2.9
Thermal Shock Resistance, points 19 to 20
54 to 68

Alloy Composition

Aluminum (Al), % 0
5.5 to 6.8
Carbon (C), % 0
0 to 0.1
Chlorine (Cl), % 0
0 to 0.2
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0
0 to 0.4
Magnesium (Mg), % 92.5 to 94.8
0
Nitrogen (N), % 0
0 to 0.040
Oxygen (O), % 0
0 to 0.3
Silicon (Si), % 0
0 to 0.1
Sodium (Na), % 0
0 to 0.2
Titanium (Ti), % 0
87 to 91
Vanadium (V), % 0
3.5 to 4.5
Zinc (Zn), % 4.8 to 6.2
0
Zirconium (Zr), % 0.45 to 1.0
0
Residuals, % 0
0 to 0.4