Haynes Waspaloy™ alloy, sheet

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Haynes Waspaloy™ alloy, sheet
Categories:	Metal; Nonferrous Metal; Nickel Alloy; Superalloy
Material Notes:	Age-hardenable superalloy with very good strength at temperatures up 980°C (1800°F), can be cold-formed in the annealed condition, may also be hot formed at 1040°C (1900°F) and above, good resistance to gas turbine combustion gas environments at temperatures up to 870°C (1600°F). Widely used as a wrought material for forged and fabricated gas turbine and aerospace components. Tensile properties reported after heat treatment per AMS 5544: 1975°F (1080°C)/30 min./WQ + 1825°F (995°C)/2 hr./AC + 1550°F (845°C)/4 hr./AC + 1400°F (760°C)/16hr./AC Data provided by the manufacturer, Haynes International, Inc.
Key Words:	AMS 5544
Vendors:

Available Properties

Density
Tensile Strength, Ultimate
Tensile Strength, Ultimate
Tensile Strength, Ultimate
Tensile Strength, Ultimate
Tensile Strength, Ultimate
Tensile Strength, Ultimate
Tensile Strength, Yield
Tensile Strength, Yield
Tensile Strength, Yield
Tensile Strength, Yield
Tensile Strength, Yield
Tensile Strength, Yield
Elongation at Break, in 51 mm
Elongation at Break, in 51 mm
Elongation at Break, in 51 mm
Elongation at Break, in 51 mm
Elongation at Break, in 51 mm
Elongation at Break, in 51 mm
Modulus of Elasticity
Modulus of Elasticity
Modulus of Elasticity
Modulus of Elasticity
Modulus of Elasticity
Modulus of Elasticity
Modulus of Elasticity
Modulus of Elasticity
CTE, linear
CTE, linear
CTE, linear
CTE, linear
CTE, linear
CTE, linear
Thermal Conductivity
Thermal Conductivity
Thermal Conductivity
Thermal Conductivity
Thermal Conductivity
Thermal Conductivity
Melting Point
Solidus
Liquidus
Maximum Service Temperature, Air, strength retained
Aluminum, Al
Boron, B
Carbon, C
Chromium, Cr
Cobalt, Co
Iron, Fe
Manganese, Mn
Molybdenum, Mo
Nickel, Ni, As Remainder
Silicon, Si
Titanium, Ti
Zirconium, Zr

Property Data

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Manufacturer Notes:
Haynes International, Inc.

Category Notes
none

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