Specification for nickel-cobalt-chromium-molybdenum-aluminium-titanium heat-resisting alloy billets, bars, forgings and parts (nickel base, Co 20, Cr 14.8, Mo 5, Al 4.8, Ti 1.2)|Air transport engineering, Aluminium-containing alloys, Chemical composition, Mechanical properties of materials, Cobalt-containing alloys, Heat-resistant materials, Billets, Forgings, Chromium-containing alloys, Metal sections, Titanium-containing alloys, Molybdenum-containing alloys, Bars (materials), Semi-finished products, Nickel alloys, Heat treatment