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Aerospace Spot Weld Shear Strength: steel nickel cobalt

steel ftu above185 t0040 to steel ftu above220 t0040

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: steel nickel cobalt10 rowsPage 3 of 5
material familyrecord iddesign shear strength lbs (lbf)material ftu range ksisheet thickness in (in)standardtensile allowable lbs (lbf)tensile allowable noteweld spec
steel nickel cobaltsteel ftu above185 t0040600above 1850.04MIL-HDBK-5J Section 8.2.2.315025% of shear strengthMIL-W-6858
steel nickel cobaltsteel ftu above185 t0050800above 1850.05MIL-HDBK-5J Section 8.2.2.320025% of shear strengthMIL-W-6858
steel nickel cobaltsteel ftu above185 t00631,040above 1850.063MIL-HDBK-5J Section 8.2.2.326025% of shear strengthMIL-W-6858
steel nickel cobaltsteel ftu above185 t00801,360above 1850.08MIL-HDBK-5J Section 8.2.2.334025% of shear strengthMIL-W-6858
steel nickel cobaltsteel ftu above185 t01001,760above 1850.1MIL-HDBK-5J Section 8.2.2.344025% of shear strengthMIL-W-6858
steel nickel cobaltsteel ftu above185 t01252,280above 1850.125MIL-HDBK-5J Section 8.2.2.357025% of shear strengthMIL-W-6858
steel nickel cobaltsteel ftu above185 t01602,960above 1850.16MIL-HDBK-5J Section 8.2.2.374025% of shear strengthMIL-W-6858
steel nickel cobaltsteel ftu above220 t0025380above 2200.025MIL-HDBK-5J Section 8.2.2.39525% of shear strengthMIL-W-6858
steel nickel cobaltsteel ftu above220 t0032520above 2200.032MIL-HDBK-5J Section 8.2.2.313025% of shear strengthMIL-W-6858
steel nickel cobaltsteel ftu above220 t0040680above 2200.04MIL-HDBK-5J Section 8.2.2.317025% of shear strengthMIL-W-6858

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