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High Temperature Resistant Alloys

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Hastelloy® Alloy X (HX)

 (26)
Hastelloy® Alloy X (HX) (UNS N06002) Ni 47.5, Cr 21.8, Fe 18.5, Mo 9.
Excellent high temperature strength and oxidation resistance to 2200 °F. Excellent forming and welding characteristics. Resistance to oxidizing, reducing, and neutral atmospheres. Resistant to SCC in petrochemical applications. Good ductility after prolonged service temperatures of 1200, through 1600 °F for 16,000 hours.
Gas turbine combustion cans and ducting, heat-treating equipment, spray bars, flame holders, furnace rolls, furnace baffles, and flash drier components.

A wrought nickel base alloy with excellent high temperature strength and oxidation resistance. All of the product forms are excellent in terms of forming and welding. Although ...


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Inconel® Alloy 625

 (33)
Inconel® Alloy 625 (UNS N06625) Ni 61.0, Cr 21.5 Mo 9.0, Nb+Ta 3.6
High strength and toughness from cryogenic temperatures to 1800 °F (980 °C), good oxidation resistance, exceptional fatigue strength, and good corrosion resistance. Chemical and pollution control equipment, ash pit seals, nuclear reactors, marine equipment, ducting, thrust reverser assemblies, fuel nozzles, afterburners, spray bars.

A material with excellent resistance to pitting, crevice and corrosion cracking. Highly resistant in a wide range of organic and mineral acids. Good high temperature strength.


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Inconel® Alloy 718

 (22)
Inconel® Alloy 718 (UNS N07718) Ni 52.5, Cr 19.0 Fe 18.5 Mo 3.0 Nb+Ta 3.6
Excellent strength from -423 °F to 1300 °F (-253 °C to 705 °C). Age hardenable and may be welded in fully aged condition, excellent oxidation resistance up to 1800 °F (980 °C).
Jet engines, pump bodies and parts, rocket motors and thrust reversers, nuclear fuel element spacers, hot extrusion tooling.

Gamma Prime strengthened alloy with excellent mechanical properties at elevated temperatures, as well as cryogenic temperatures. Suitable for temperatures up to around 1300 °F. Can be readily worked and age hardened.

Excellent strength from -423 °F to 1300 °F (-253 °C to 705 °C). Age hardenable and ...


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Inconel® alloy 600

 (24)
Inconel® alloy 600 (UNS N06600) Ni 76.0, Cr 15.5, Fe 8.0 INCONEL® alloy 600 (UNS N06600) Ni 76.0, Cr 15.5, Fe 8.0

A nickel-chromium alloy with good oxidation resistance at higher temperatures. With good resistance in carburizing and chloride containing environments.

Alloy 600 is a nickel-chromium alloy designed for use from cryogenic to elevated temperatures in the range of 2000 deg F(1093 °C). The high nickel content of the alloy enables it to retain considerable resistance under reducing conditions and makes it resistant to corrosion by a number of organic and inorganic compounds. The nickel content gives it excellent resistance to chloride-ion stress-corrosion cracking and also provides excellent resistance to ...


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Inconel® Alloy 601

 (20)
Inconel® Alloy 601 (UNS N06601) Ni 61, Fe Bal, Cr 22, Al 1.4
Nickel, higher chromium content for better resistance to oxidizing and reducing environments; for severely corrosive environments at elevated temperatures. Good oxidation resistance to 2200 °F. Good formability.
Instrument probes, furnace muffles, electronic components, chemical and food process equipment, heat treating equipment, nuclear steam generator tubing.

Inconel nickel-chromium-iron alloy 601 is a general-purpose engineering material for applications that require resistance to heat and corrosion. The outstanding characteristic of Inconel alloy 601 is its resistance to high-temperature oxidation. The alloy also has good resistance to aqueous ...


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Incoloy® Alloy 800H

Incoloy® alloy 800H (UNS N08811) Fe base, Ni 32, Cr 21, Mn 1.5

UNS N08810 / UNS N08811
Exhibits excellent resistance to carburization, oxidation and nitriding atmospheres. The alloy is dual certified and combines the properties of both forms.

800HT is an iron-nickel-chromium alloy having the same basic composition as Alloy 800, with significantly higher creep rupture strength. The higher strength results from close control of carbon, aluminum and titanium contents in conjunction with a high temp anneal. The 800H modification was to control carbon (0.05 to 0.10%) and grain size to (>ASTM 5) to optimize stress rupture properties. 800HT has further modifications to the combined titanium and aluminum levels (0.85 to ...


Haynes® Alloy 25 (L605)

 (15)
Haynes® Alloy 25 (L605) (UNS R30605) Co 50.0, Cr 20.0, W 15.0, Ni 10.0, Fe 3.0 Mn 1.5
Excellent strength for continues service to 1800 °F. Oxidation and carburization resistance to 1900 °F. Galling resistant, with resistance to marine environments, acids and body fluids. Non-magnetic, even when severely cold reduced, can reach Rc 50 when cold reduced and aged. Resistant to hydrochloric and nitric acid at certain concentrations and temperatures, and wet chlorine environments at room temperature.
Gas turbine engine components: combustion chambers, and afterburners. Other uses also include: high temperature ball bearing service, springs, and heart valves.

Alloy L-605 is the strongest of the formable cobalt alloys, ...


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Nitronic® 60 (Alloy 218)

 (78)
Nitronic® 60 (Alloy 218) (UNS S21800) Fe 63, Cr 17, Mn 8, Ni 8.5, Si 4, N 0.13
High strength fully Austenitic alloy that resists galling and wear. Significantly lower cost to extend part life and lower maintenance. The yield strength is twice that of 304 and 316 stainless steels, in the annealed condition. Tensile strengths can be produced in excess of 200 ksi. Chloride pitting is superior to that of type 316, and the oxidation resistance is similar to type 321 at elevated temperatures, and excellent cryogenic impact strength. Valves stems, seats, and trim; fastening systems, screening, pins, bushings, roller bearings, pump shafts and rings. Food handling, medical, automotive, aerospace and nuclear.

Austenitic ...


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