SAE AS7468 Bolts, Cobalt-Chromium-Nickel Alloy, UNS R30035, Tensile Strength 260 ksi, Procurement Specification
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Product Code:SAE AS7468
Title:Bolts, Cobalt-Chromium-Nickel Alloy, UNS R30035, Tensile Strength 260 ksi, Procurement Specification
Issuing Committee:E-25 General Standards For Aerospace And Propulsion Systems
Scope: This procurement specification covers aircraft bolts made from a corrosion resistant, work-strengthened, cobalt-chromium-nickel alloy of the type identified under the Unified Numbering System as UNS R30035. The following specification designations and their properties are covered: AS7468, 260 ksi minimum ultimate tensile strength at room temperature, 135 ksi tension to 13.5 ksi tension fatigue at room temperature; AS7468-1, 260 ksi minimum ultimate tensile strength at room temperature, 145 ksi minimum ultimate shear strength at room temperature. Primarily for aerospace propulsion system applications where an excellent combination of strength, fatigue, and corrosion resistance is required at temperatures upto 700掳F.
Title:Bolts, Cobalt-Chromium-Nickel Alloy, UNS R30035, Tensile Strength 260 ksi, Procurement Specification
Issuing Committee:E-25 General Standards For Aerospace And Propulsion Systems
Scope: This procurement specification covers aircraft bolts made from a corrosion resistant, work-strengthened, cobalt-chromium-nickel alloy of the type identified under the Unified Numbering System as UNS R30035. The following specification designations and their properties are covered: AS7468, 260 ksi minimum ultimate tensile strength at room temperature, 135 ksi tension to 13.5 ksi tension fatigue at room temperature; AS7468-1, 260 ksi minimum ultimate tensile strength at room temperature, 145 ksi minimum ultimate shear strength at room temperature. Primarily for aerospace propulsion system applications where an excellent combination of strength, fatigue, and corrosion resistance is required at temperatures upto 700掳F.
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