BS HR 206:1973 Specification for nickel-cobalt-chromium-molybdenum-titanium-aluminium heat-resisting alloy plate, sheet and strip (nickel base, Co 20, Cr 20, Mo 5.9, Ti 2.1, Al 0.5)
British Standard : Aerospace Series Specification for
Nickel-cobalt-chromium-molybdenum-titanium-
aluminium heat-resisting alloy plate,
sheet and strip
(Nickel base, Co 20, Cr 20, Mo 5.9, Ti 2.7, Al 0.5)
1. Inspection and testing procedure
2. Manufacture
3. Chemical composition
4. Condition
5. Heat treatment
6. Selection and preparation of mechanical test samples
7. Mechanical properties
BS HR 206:1973 history
2009BS 2HR 206:2009 Specification for nickel-cobalt-chromium-molybdenum-titanium-aluminium heat-resisting alloy plate, sheet and strip (nickel base, Co 20, Cr 20, Mo 5.9, Ti 2.1, Al 0.5)
1973BS HR 206:1973 Specification for nickel-cobalt-chromium-molybdenum-titanium-aluminium heat-resisting alloy plate, sheet and strip (nickel base, Co 20, Cr 20, Mo 5.9, Ti 2.1, Al 0.5)