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Name:Hastelloy X (UNS N06002)
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Brief introduction: Hastelloy X (UNS N06002)
HASTELLOY X (HX) (UNS N06002)
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   Hastelloy® X is a high temperature and corrosion resistant nickel-based solid solution strengthened alloy. This alloy has outstanding resistance to oxidation and possesses exceptional strength at elevated temperatures. Molybdenum enables this alloy to be hard, strong, and suitable for welding applications. Alloy X exhibits good formability and machinability.

Alloy X is non-magnetic. It has high strength up to 1500ºF (816ºC) and good oxidation resistance up to 2200ºF (1204ºC). This alloy is especially resistant to carburization and nitriding, conditions which cause failure in some high temperature alloys. It is used extensively in high temperature jet engine and chemical processing applications and is highly resistant to stress corrosion cracking in petrochemical applications.  Industrial furnace applications incorporate Alloy X for its resistance to oxidizing and its ability to maintain good ductility after prolonged exposure to extremely high temperatures.

Chemistry

Chemical Requirements


Ni

Cr

Mo

Mn

C

Si

Fe

Max

Bal

23.0

10.0

1.00

0.15

1.00

20.0

Min


20.5

8.00


0.05


17.0


Tensile Data

Mechanical Property Requirements


Ultimate Tensile

Yield Strength (0.2% OS)

Elong.

R/A

Hardness

Min

95 KSi

35 KSi

35



Max






Min

655 MPa

240 MPa




Max







Specifications

Form

Standard

Metal Type

UNS N06002

Bar

ASTM B572 AMS 5754

Wire

AMS 5798W AMS 5798C

Sheet

ASTM B435 AMS 5536

Plate

ASTM B435 AMS 5536

Tube

AMS 5587 AMS 5588 ASTM B619 ASTM B622

Pipe

AMS 5587 AMS 5588 ASTM B619 ASTM B622

Fitting

ASTM B366

Forging

AMS 5754 GE B50TF31

Weld Wire

A5.14 ERNiCrMo-2

Weld Electrode

A5.11 ENiCrMo-2

Din

2.4665


Heat-Treatment Wrought forms of HASTELLOY® X alloy are furnished in the solution heat-treated condition unless otherwise specified. X alloy is typically solution heat-treated at 2150°F (1177°C) and rapid cooled. Bright annealed products are cooled in hydrogen. Annealing at temperatures lower than the solution heat- treating may cause precipitation of secondary phases, which may affect the alloy’s strength and ductility. Useful for Aircraft, Furnace and Chemical Process Components X alloy has wide use in gas turbine engines for combustion zone components such as transition ducts, combustor cans, spray bars and flame holders as well as in afterburners, tailpipes and cabin heaters. It is recommended for use in industrial furnace applications because it has unusual resistant to oxidizing, reducing and neutral atmospheres. Furnace rolls of this alloy were still in good condition after operating for 8,700 hours at 2150°F (1177°C). 

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