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Aerospace Spot Weld Shear Strength: magnesium alloy

mag ftu below32 t0032 to mag ftu below32 t0160

Design-allowable shear load per spot (lbs) for resistance spot welds per MIL-HDBK-5J Section 8.2.2.3 and MIL-W-6858. Indexed by material family (aluminum alloy, steel/nickel/cobalt alloy, magnesium alloy, titanium alloy), parent metal Ftu range (ksi), and sheet thickness (in). Tensile allowable is 25% of shear strength. Covers thicknesses 0.020–0.160 in. No filler metal — allowable is empirical load-per-spot based on sheet thickness and parent metal ultimate tensile strength.

Aerospace Engineeringmaterial family: magnesium alloy8 rowsPage 2 of 2
material familyrecord iddesign shear strength lbs (lbf)material ftu range ksisheet thickness in (in)standardtensile allowable lbs (lbf)tensile allowable noteweld spec
magnesium alloymag ftu below32 t003276below 320.032MIL-HDBK-5J Section 8.2.2.31925% of shear strengthMIL-W-6858
magnesium alloymag ftu below32 t0040108below 320.04MIL-HDBK-5J Section 8.2.2.32725% of shear strengthMIL-W-6858
magnesium alloymag ftu below32 t0050148below 320.05MIL-HDBK-5J Section 8.2.2.33725% of shear strengthMIL-W-6858
magnesium alloymag ftu below32 t0063208below 320.063MIL-HDBK-5J Section 8.2.2.35225% of shear strengthMIL-W-6858
magnesium alloymag ftu below32 t0080280below 320.08MIL-HDBK-5J Section 8.2.2.37025% of shear strengthMIL-W-6858
magnesium alloymag ftu below32 t0100376below 320.1MIL-HDBK-5J Section 8.2.2.39425% of shear strengthMIL-W-6858
magnesium alloymag ftu below32 t0125488below 320.125MIL-HDBK-5J Section 8.2.2.312225% of shear strengthMIL-W-6858
magnesium alloymag ftu below32 t0160640below 320.16MIL-HDBK-5J Section 8.2.2.316025% of shear strengthMIL-W-6858

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