Chemical Compositions Of Hastelloy X Nickel Alloy Composition Ni Cr Fe Mo W Co C Mn Si S Cu Al Ti Content (%) Min. Bal. 20.5 17.0 8.0 0.2 0.5 0.05 Max. 23.0 20.0 10.0 1.0 2.5 0.15 1.0 1.0 0.015 0.5 0.15 0.5

Mechanical Properties (Minimum Value At 20℃) Tensile Strength (σb/MPa) Yield Strength (σp0.2/MPa) Elongation (σ5/%) 690 275 30

Chemical Compositions Of Hastelloy X Nickel Alloy Composition Ni Cr Fe Mo W Co C Mn Si S Cu Al Ti Content (%) Min. Bal. 20.5 17.0 8.0 0.2 0.5 0.05 Max. 23.0 20.0 10.0 1.0 2.5 0.15 1.0 1.0 0.015 0.5 0.15 0.5

Mechanical Properties (Minimum Value At 20℃) Tensile Strength (σb/MPa) Yield Strength (σp0.2/MPa) Elongation (σ5/%) 690 275 30

Alloy X/ UNS N06002

Grade: Hastelloy X/ UNS N06002/Alloy X

Sheet/Plate: 0.3mm-150mm

Strip/Foil: 0.02mm-16mm

Pipe: 6mm*0.5mm-1200mm*100mm

Bar: Ф6mm – Ф600mm

Wire: Ф0.01mm – Ф6mm

Others: Forged Rings, Flanges, Elbows, Tees, Reducers etc.

Standard: ASTM/ASME/AMS

The Hastelloy X nickel alloy, with higher iron content, has favorable resistance to oxidation and corrosion combined with excellent creep and rupture strength at temperatures under 900℃. In addition to this, Hastelloy alloy X has great fabricability by cold and hot working and good weldability.

1. High degree of oxidation resistance up to 2200° F

2. Outstanding high-temperature strength

3. Easily fabricated including forming and welding

4. Good ductility after prolonged exposure at high-temperatures

5. Good resistance to chloride stress-corrosion cracking

6. Resistant to carburization and nitriding

7. Develops a protective oxide film that does not spall off

Chemical Compositions Of Hastelloy X Nickel Alloy

Composition		Ni	Cr	Fe	Mo	W	Co	C	Mn	Si	S	Cu	Al	Ti
Content (%)	Min.	Bal.	20.5	17.0	8.0	0.2	0.5	0.05
	Max.		23.0	20.0	10.0	1.0	2.5	0.15	1.0	1.0	0.015	0.5	0.15	0.5

Mechanical Properties (Minimum Value At 20℃)

Tensile Strength (σb/MPa)	Yield Strength (σp0.2/MPa)	Elongation (σ5/%)
690	275	30

Applications

This oxidation resistant alloy can be used for combustor components and other high temperature parts of aircraft engines, for long term use at temperature under 900℃ and short time use up to 1080℃.
1.Gas turbine engines
2.Transition ducts
3.Combustor cans
4.Spray bars and flame holders
5.Afterburners, tailpipes, and cabin heaters
6.Chemical processing retorts, muffles, and tubing