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SUPERALLOY

Waspaloy

UNS N07001, AMS 5706, AMS 5707
SuperalloyVery High Cost
DENSITY
8 kg/m³
MELTING POINT
1,330°C
TENSILE STRENGTH
1,275 MPa
MAX SERVICE TEMP
870°C

Waspaloy is a superalloy used in aerospace applications. Melting point: 1,330 °C. Tensile strength: 1,275 MPa.

ABOUT WASPALOY

Waspaloy is a nickel-based superalloy with excellent high-temperature strength and corrosion resistance, developed originally for jet engine applications. It maintains good mechanical properties up to 870°C and has outstanding creep-rupture strength. It is widely used in turbine discs and rocket engine components.

CHEMICAL COMPOSITION

Ni 58%, Cr 19%, Co 13.5%, Mo 4.3%, Ti 3%, Al 1.4%

ROCKET & SPACECRAFT APPLICATIONS
Turbine discs
Compressor discs
Rocket turbopump housings
Fasteners for hot sections
Shaft and ring components
MANUFACTURING PROPERTIES
CORROSION RESISTANCE
Excellent
WELDABILITY
Fair
MACHINABILITY
Poor
COST RATING
Very High
MECHANICAL PROPERTIES
DENSITY8 kg/m³
TENSILE STRENGTH1,275 MPa
YIELD STRENGTH795 MPa
STRENGTH-TO-WEIGHT155677.7 kN·m/kg
THERMAL PROPERTIES
MELTING POINT1,330 °C
MAX SERVICE TEMPERATURE870 °C
THERMAL CONDUCTIVITY11.7 W/m·K
THERMAL EXPANSION12.4 µm/m·K
COMPLETE SPECIFICATIONS
CATEGORYSuperalloy
DESIGNATIONSUNS N07001, AMS 5706, AMS 5707
MANUFACTURERAllegheny Technologies (ATI)
DENSITY8 kg/m³
TENSILE STRENGTH1,275 MPa
YIELD STRENGTH795 MPa
MELTING POINT1,330 °C
MAX SERVICE TEMP870 °C
THERMAL CONDUCTIVITY11.7 W/m·K
THERMAL EXPANSION12.4 µm/m·K
CORROSION RESISTANCEExcellent
WELDABILITYFair
MACHINABILITYPoor
COST RATINGVery High

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