Available in strip and wire
Nickel alloys are renowned for their exceptional strength, heat resistance, and corrosion resistance, making them indispensable in high-performance industries such as aerospace, defence, medical, electronics, automotive, oil & gas, and power generation. Whether you require materials capable of withstanding extreme temperatures, resisting aggressive chemical environments, or delivering precise electrical performance, our range of nickel alloys provides proven solutions.
From four dedicated stock and service centres, the Knight Group offers one of Europe’s most extensive ranges of precision nickel alloys, including Inconel®, Incoloy®, Hastelloy®, Haynes®, Monel®, Nimonic®, Waspaloy®, Rene®, Nilo®, Ni-Span® , available in strip and wire form.
INCONEL® 600 / Nickel Alloy 600 / 2.4816 / N06600
INCONEL® 601 / Nickel Alloy 601 / 2.4851 / N06601
INCONEL® 625 / Nickel Alloy 625 / 2.4856 / N06625
INCONEL® 718 / Nickel Alloy 718 / 2.4668 / N07718
INCONEL® X-750 / Nickel Alloy X750 / N07750
INCOLOY® 25-6MO / 1.4529 / N08926
INCOLOY® A-286 / 1.4980 / S66286
INCOLOY® 800 / Nickel Alloy 800
INCOLOY® 825 / Nickel Alloy 825 / N08825
INCOLOY® 925 / N09925
HASTELLOY® B-3 / N10675
HASTELLOY® C-4 / N06455
HASTELLOY® X / Nickel Alloy X / 2.4665 / N06002
HASTELLOY® C-22 / Nickel Alloy C22 / 2.4602 / N06022
HASTELLOY® C-2000 / Nickel Alloy C2000 / 2.4675 / N06200
HASTELLOY® C-276 / Nickel Alloy C 276 / 2.4819 / N10276
HAYNES® 242 / N10242
HAYNES® 282 / N07208
HAYNES® 230 / N06230
HAYNES® 263 / N07263
HAYNES® 214 / Nickel Alloy 214 / 2.4646 / N07214
HAYNES® HR-120® Alloy / 2.4854 / N08120
HAYNES® 25 / L605 / 2.4964 / 2.4967 / R30605
HAYNES® 188 / 2.4683 / R30188
HAYNES® 233 / Nickel Alloy 233
HAYNES® 224 / Nickel Alloy 224
MONEL® K500 / Nickel Alloy K-500 / N05500
MONEL® 400 / Nickel Alloy 400 / 2.4360 / 2.4361 / N04400
RENE 41 / 2.4973/ N07041
WASPALOY® / 2.4654 / N07001
NIMONIC® 75 / Nickel Alloy 75 / 2.4951 / N06075
NIMONIC® 90 / Nickel Alloy 90 / 2.4632 / 2.4969 / N07090
Nickel Alloy 201 / N02201
Nickel Alloy 200 / N02200
Nickel 212
Ni Cr 37/18 / Ni Cr 3718
Ni Cr 60/16 / NO 6004 / 2.4867 / Ni Cr 6015
Ni Cr 80/20 / NO6003 / 2.4869 / Ni Cr 8020
NI-SPAN-C® ALLOY 902 / N09902
CuNi6 / IMPHY® CuNi6 / 2.0807
CuNi2 / IMPHY® CuNi2 / 2.0802
CuNi44 / Hecnum / IMPHY® CuNi44 / 2.0842
CuNi30/ CuNi30Mn / IMPHY® CuNi30/ 2.0838 / 2.0890
CuNi10 / IMPHY® CuNi10 / 2.0811
CuNi23 / IMPHY® CuNi23 / 2.0881
Nilo® 42 / K94100 / K94101 / NiFe42
Nilo® K / K94610 / 29/18 / NiFeK
Nilo® 48 / K94800 / NiFe48
Nilo® 36 / K93603 / NiFe36
Nilo®52 / N14052 / NiFe52
Nickel alloys deliver a unique combination of high-temperature strength, oxidation/corrosion resistance, weldability, and formability, making them essential for applications in aerospace, defence, chemical processing, oil and gas, power generation, precision engineering and battery technologies. As temperatures climb or environmental chemistries get harsher, stainless steels can reach their limits; nickel alloys keep working, extending the operating window—from cryogenic service up to ~1000 °C+ (1832°F)
Nickel is a transition metal found in the Earth’s core as a nickel-iron alloy, and in the crust, where it is mainly in laterite ores (such as nickeliferous limonite and garnierite) and magmatic sulphide deposits (notably pentlandite). Identified in 1751 by Axel Fredrik Cronstedt, nickel has since become essential in alloy development, particularly in many stainless steels—stabilising austenite and improving corrosion resistance; while in duplex grades it helps phase balance alongside nitrogen and molybdenum.
Nickel’s unique atomic structure and properties make it an ideal foundation for alloy development. Nickel provides strength, ductility, and corrosion/oxidation resistance and readily forms solid solutions with many elements, enabling alloys tailored for extreme heat and aggressive chemistries. Depending on grade and design, service spans cryogenic to ~1000 °C+ (1832°F), with some grades exceeding 1,000 °C (1,832 °F). In practice, nickel-based alloys are commonly specified from ~870 °C (1,598 °F). Today, with their wide range of commercial applications, nickel alloys represent one of the most versatile and technologically advanced groups of engineering materials used in modern manufacturing.
The development of nickel alloys represents sophisticated metallurgical engineering, with each alloying element serving specific purposes.
Chromium additions promote a stable chromium-oxide/passive film, improving oxidation and general corrosion resistance; specific contents vary by grade. In many Ni-Cr and Ni-Cr-Fe alloys, this is typically between 14–25%; however, actual ranges are alloy-specific and can fall outside of this range.
Molybdenum and tungsten provide solid-solution strengthening and markedly improve resistance to pitting and crevice corrosion, especially in chloride-bearing media.
Iron is tuned to purpose: high-Ni, low-Fe alloys maximise corrosion resistance, while Fe-Ni compositions (e.g.NILO® 36) deliver controlled thermal expansion or soft-magnetic behaviour for precision uses.
Copper additions enhance performance in reducing acids (notably sulphuric); examples include INCOLOY® 825 and HASTELLOY® C-2000, where Cu improves resistance to reducing environments while Cr supports oxidising resistance.
Titanium and aluminium enable precipitation hardening via γ′ (Ni₃(Al,Ti)), delivering exceptionally high-temperature strength retention in many nickel-base superalloys.
Renowned for their exceptional performance characteristics, nickel alloys perform where conventional materials fall short. No matter how demanding the requirements, nickel alloys can provide a uniquely tailored combination of properties to exceed performance expectations.
Outstanding corrosion resistance is a key attribute of nickel alloys, significantly enhancing their durability in harsh environments, making them a popular choice for a broad range of applications. Their exceptional corrosion resistance stems from the formation of a stable oxide on their surface. This layer acts like a protective barrier against harsh chemical agents, including acidic solutions, seawater, and high-temperature gases.
Unlike stainless steels, which rely primarily on chromium for corrosion protection, nickel alloys exhibit superior stability and performance across a broader spectrum of conditions. While heat-resistant stainless steels can operate to ~800–950 °C (1472°F-1742°F) in specific roles, nickel alloys extend this range from cryogenic service to ~1000 °C+ (1832°F) and offer better oxidation/creep margins. Furthermore, these impressive alloys effectively maintain their structural integrity not just in oxidising environments, but also in reducing atmospheres that would typically challenge other materials. This dual capability makes nickel alloys particularly valuable in industries where exposure to extreme conditions is common, such as chemical processing, maritime applications, and power generation. Their versatility and reliability ensure that they remain a preferred choice for applications demanding long-lasting resistance to corrosion.
Nickel alloys are characterised by their remarkable thermal stability, setting them apart from other material families. While aluminium alloys experience a rapid loss of strength when exposed to temperatures exceeding 200°C (392°F), and conventional steels become unsuitable for high-temperature applications beyond 600°C (1112°F), nickel alloys are engineered to retain their mechanical properties even at extreme temperatures over 1000°C (1832°F). Exhibiting exceptional thermal stability and outstanding creep resistance, nickel alloys can withstand deformation under prolonged stress and high temperatures.
This combination of thermal stability and resistance to creep makes these alloys vital in critical applications such as aerospace engines, where they endure intense heat and pressure, as well as in power generation turbines that operate at elevated temperatures for sustained periods.
High-strength characteristics enable nickel alloys to deliver exceptional mechanical performance through two key mechanisms: precipitation hardening and solid solution strengthening. Precipitation hardening involves the formation of fine particles within the alloy, which impede the movement of dislocations and thereby increase the material’s strength. Solid solution strengthening, on the other hand, occurs when the atoms of the alloying element are dissolved in the nickel matrix, effectively increasing the strength of the material. This engineering process enables superalloys like INCONEL 718 to retain high strength up to ~700 °C (1292°F), with a typical tensile strength of 1100 MPa (160 ksi) at 650 °C (1202°F). This provides the strength-to-weight ratios essential for rotating aerospace components and high-stress structural applications.
The magnetic properties of nickel alloys offer distinct advantages in electronics and precision instrumentation. Some alloys demonstrate controlled expansion characteristics that are essential for hermetic sealing applications, while others possess soft magnetic properties that are crucial for electromagnetic devices. Low expansion alloys, such as NILO® 36, exhibit ultra-low expansion, with thermal expansion coefficients as low as 1.56 × 10⁻⁶/°C over 20–300°C (68-572°F), achieving dimensional stability that is not attainable with other conventional materials.
Electrical resistance properties of specialised nickel-chromium alloys make them essential for heating elements and resistive applications. These alloys maintain a stable electrical resistivity, ensuring consistent performance even under extreme conditions. Notably, they exhibit excellent resistance to oxidation at elevated temperatures, capable of withstanding environments typically up to ~1100–1200°C (2012-2192°F) depending on the grade.
This remarkable durability enables precise thermal control in a variety of industrial processes, including high-temperature furnaces, laboratory applications, and specialised heating systems. Operating reliably at such high temperatures without significant degradation makes nickel-chromium alloys a reliable choice for manufacturers looking to enhance efficiency and safety in thermal management solutions.
Glass sealing capabilities of controlled expansion alloys enable hermetic packaging for electronics and instrumentation. The precise matching of thermal expansion coefficients between metal and glass components ensures reliable seals that maintain integrity across temperature cycling. Reliability is crucial for critical applications, in sectors like aerospace and defence electronics, where electronic components often encounter extreme operating conditions. These sectors operate under rigorous standards, where requiring robust environmental sealing is paramount, as even minor failures can lead to catastrophic results.
| Property | Nickel Alloy Advantage |
|---|---|
| Corrosion Resistance | Effective in oxidising & reducing conditions, incl. acids & seawater |
| High‑Temperature Strength | Retains useful strength to high temperatures (grade-dependent; commonly ~700–1000 °C / 1292-1832°F °F); resists creep. |
| Mechanical Strength | Tensile strength to 1200+ MPa (~174 ksi); precipitation/solution hardened |
| Magnetic & Expansion | Low expansion alloys for glass-sealing & precision systems |
| Electrical Resistance | Stable resistivity up to 1150 °C (2102°F); long life in thermal cycling |
| Glass Sealing | Controlled expansion for hermetic, fail-safe performance |
Nickel alloys are typically grouped by chemistry, but can also be categorised by performance, trademarked family, strengthening mechanism, or application class. These categories are not mutually exclusive, and boundaries within categories often overlap, so many alloys fall into multiple classification groups.
Nickel alloys are commonly organised by their chemical composition and manufacturing heritage, with each family offering distinct performance characteristics.
Solid Solution Strengthened Alloys
These alloys derive their strength from the atomic distortion created by alloying elements in solid solution. Solid Solution Strengthened Nickel Alloys include INCONEL® 625 and HASTELLOY® C-276, which offer exceptional corrosion resistance without requiring heat treatment. Their excellent formability in precision strip and wire forms makes them ideal for complex aerospace components and chemical processing equipment.
Precipitation Hardened Nickel Alloys
Alloys such as INCONEL® 718 and X-750 utilise controlled precipitation of intermetallic phases to achieve remarkable strength at elevated temperatures. These alloys are essential for rotating aerospace components where strength-to-weight ratios are critical. The ability to age-harden after forming enables complex geometries whilst maintaining dimensional precision.
Superalloys
High-performance nickel-based alloys are engineered for extreme temperature and stress conditions, typically above 540°C (1004°F). These include INCONEL® 718, Waspaloy®, and RENÉ® 41, which maintain exceptional strength and creep resistance in gas turbine engines and aerospace applications.
Heat Resistant / High Temperature Alloys
Alloys optimised for oxidation resistance and structural stability at elevated temperatures, such as HAYNES® 230, HAYNES® 214, and INCONEL® 601. These materials resist scaling and maintain integrity in furnace environments and high-temperature processing equipment.
Corrosion-Resistant Alloys
Materials engineered primarily for chemical resistance across diverse environments, including HASTELLOY® C-276, HASTELLOY® C-22, and INCONEL® 625. These alloys excel in chemical processing, marine environments, and aggressive industrial conditions.
High Strength Alloys
Alloys developed for mechanical performance requirements, including precipitation-hardened grades like INCONEL® 718, A-286, and age-hardenable variants that provide superior strength-to-weight ratios for structural applications.
Electrical Resistance Alloys (Wire Grades)
Specialised nickel-chromium alloys designed for heating elements and electrical resistance applications. These include Ni Cr 80/20, Ni Cr 60/16, and Ni Cr 37/18, which provide controlled electrical resistivity and oxidation resistance for heating wire applications up to ~1100–1200 °C (2012-2192°F ) depending on the grade..
Controlled Expansion Alloys
Specialised alloys like NILO® 36 and NILO® 42 provide minimal thermal expansion for precision instrumentation and glass-sealing applications. These materials are irreplaceable in electronics where dimensional stability across temperature ranges is paramount.
There is no definitive number of nickel alloys, as slight variations in chemical composition can lead to distinct performance traits. The continuous demand for improved performance, safety, and efficiency in industries such as aerospace and defence, chemical processing, energy, and electronics drives the ongoing metallurgy development.
Vertically integrated producers, such as Special Metals and Haynes International, offer services that span R&D and melting through to rolling, drawing, and testing. This enables producers to meet the needs of niche applications, continuously expand the range of high-performance alloys, while keeping pace with present manufacturing challenges and those on the horizon. Behind each innovation lies an extensive and costly development process, involving carefully engineered proprietary compositions and processing techniques, resulting in a concentration of patented nickel alloys. Many of the most recognisable nickel alloys were developed as part of larger patented families, such as Inconel®, Incoloy®, Hastelloy®, Haynes®, Monel®, Nimonic®, Waspaloy®, Rene®, and Nilo®.
INCONEL®, INCOLOY®, NILO®, and NI-SPAN® are trademarks of Special Metals Corporation. HASTELLOY® and HAYNES® are trademarks of Haynes International. MONEL® and NIMONIC® are trademarks of their respective owners.
Nickel alloys in precision strip and wire require exceptional dimensional control, surface quality, and mechanical consistency to meet the demanding requirements of applications found in high-reliability sectors, such as aerospace and defence, energy, electronics, and battery systems. Strip products typically range from ~0.05mm to 3.0mm (0.00197” – 0.1181″) thickness with widths up to ~600mm (23.62”), and Wire is produced from ~0.025 mm (0.0098″) diameter upwards for ultra-fine applications.
Strip manufacturing combines multi-stage cold rolling, annealing, and precision finishing to maintain tight thickness and flatness targets. Thickness tolerances as tight as ±0.01 mm are achievable on thin strip in suitable tempers and widths. Edge quality and surface finish are controlled for the end-use.
Wire production uses controlled multi-pass drawing and intermediate annealing to deliver consistent diameter, mechanical properties and surface condition across long lengths—vital for coilability and downstream forming. Ultra-fine nickel wire, with a diameter of 0.025 mm (0.0098″), is routinely supplied for use in electronics and sensor leads.
As a leading nickel-alloy specialist, the Knight Group supplies 50+ grades of precision strip and wire to suit demanding applications. For compliance-driven programs, products can typically be supplied to European/British/ASTM/AMS specifications or other standards by request.
Choose commercially pure nickel (200/201) for applications requiring maximum conductivity, deep draw/spin forming, caustic environments, or where magnetic properties are beneficial.
Choose Nickel 212 for electrical and electronic applications needing reliability and durability, high strength, good thermal conductivity, and corrosion resistance.
Commercially pure nickel grades are the first choice when you need high electrical and thermal conductivity, excellent workability, and reliable performance in reducing and caustic environments—in precision strip and wire forms.
What it is: Nickel 200 is a general-purpose commercially pure nickel for service up to ~315°C (599°F). It combines high electrical and thermal conductivity with excellent resistance to caustic alkalies and performs well in reducing, non-oxidising media. It is ferromagnetic at room temperature and is readily formed and welded in both strip and wire. Use Nickel 201 above ~315°C (599°F) to avoid graphitisation.
Use it for: Chemical processing hardware, electrical components, caustic handling, and general fabricated strip and wire parts.
What it is: Nickel 201 is the low-carbon version of Nickel 200 (carbon 0.02% max) engineered for elevated-temperature applications. It retains essentially the same aqueous corrosion profile as Nickel 200 but is the preferred grade above ~315°C (599°F). Some producers document successful service in dry chlorine and dry hydrogen chloride to approximately 500–540°C (932-1004°F), and use in laboratory crucibles in oxidising furnace atmospheres to ~1100°C (2012°F), subject to conditions. It also work-hardens more slowly, aiding severe forming.
Use it for: Prolonged high-temperature service
What it is: Nickel–manganese grade designed for higher strength than pure nickel while retaining good conductivity and weldability. Typical uses include electrical lead/lead-in wires, lamp components and electrodes. In practice it is supplied as precision wire; resistivity at 20°C (68°F) is commonly reported around ~10.9 μΩ• cm. (66 ohm circ mil/ft).
Use it for: Lead/lead-in wires, lamp supports, electrodes and related electrical components.
Choose INCONEL® 600/601 for high-temperature oxidation resistance, carburisation resistance, and applications in furnace components and heat treatment equipment. (601 offers best-in-class oxidation/spalling resistance).
Choose INCONEL® 625 for superior corrosion resistance in marine environments, chemical processing, and aerospace applications requiring high strength at elevated temperatures.
Choose INCONEL® 718/X-750 for high-temperature structural applications requiring exceptional strength retention, such as gas turbine components and aerospace fasteners.
.Nickel–chromium alloys are engineered for service where components must retain strength and resist oxidation at elevated temperatures. Chromium promotes a thin, adherent oxide film that protects the metal in hot air and combustion atmospheres, while the nickel matrix provides toughness, corrosion resistance and fabrication ease. This combination gives Ni–Cr alloys an advantage when thermal cycling, carburising or chloride-bearing environments push conventional materials beyond their limits, Typical uses span thermal processing equipment, chemical processing and desalination, power generation and oil & gas, aerospace and defence, and high-performance automotive hot-end components.
Supplied in precision strip and wire, these alloys offer a dependable combination of high-temperature integrity, oxidation/scale resistance and ease of fabrication-friendly, with specific grades chosen to match the balance of corrosion resistance and strength your application requires. INCONEL® alloys are among the most recognised commercial families of nickel-chromium alloys.
INCONEL® alloys are the go-to choice when your application requires exceptional high-temperature strength, outstanding oxidation resistance, and reliable performance in the most demanding corrosive environments—available in precision strip and wire forms. Compared with standard stainless steels, they extend the operating window in hot, aggressive, or chloride-bearing environments.
Within the family, there are two broad types:
INCONEL® is a registered trademark of Special Metals Corporation.
Choose INCOLOY® 800 for general high-temperature service with oxidation and carburisation resistance; suitable for load-bearing service up to about 815 °C (1500 °F). For applications where creep-rupture governs (especially above ~600–650 °C), specify 800H/800HT instead of 800.
Choose INCOLOY® 825 for superior aqueous-corrosion resistance in mixed reducing/oxidising media (sulfuric, phosphoric, seawater, chlorides). It is generally selected for corrosion service rather than high-temperature creep duties; avoid prolonged exposure above about 540 °C (1000 °F) because microstructural changes reduce ductility/impact strength.
Choose INCOLOY® A-286 for high-strength aerospace and gas-turbine components; age-hardenable with excellent mechanical properties for high-strength service to about 700 °C (1300 °F).
Choose INCOLOY® 925 (age-hardenable) for demanding oil-and-gas downhole/surface components requiring high strength and resistance to H₂S/CO₂ sour environments.
Nickel-iron-chromium alloys balance nickel’s toughness and chloride stress-corrosion cracking with chromium’s oxidation protection at high temperatures and the cost-effectiveness of iron. The result is a group of alloys that bridge the gap between austenitic stainless steels and higher nickel content superalloys, offering enhanced high-temperature and oxidation/carburisation resistance and lower thermal expansion than the popular 300-series stainless steels (e.g., α≈14.1–14.4 µm/m·°C at 100 °C (572°F) for 825/800 vs ~17 µm/m·°C typical for 304).
Supplied as precision strip and wire, nickel-iron-chromium grades are widely used in thermal processing, petrochemical, power generation and chemical processing—e.g., furnace fixtures, heaters/heat-treat equipment, heat-exchanger tubing, and electrical-heater sheathing.
800 Series Nickel Alloys
Designed to withstand the harsh conditions of the petrochemical industry, 800-series nickel alloys are optimised for high-temperature service in furnaces and petrochemical heaters. 800H and 800HT feature controlled carbon (and for 800HT, controlled Al+Ti) to optimise creep-rupture strength at elevated temperatures.
INCOLOY® alloys are the preferred choice when your application demands reliable high-temperature performance, excellent oxidation resistance, and enhanced resistance to carburisation and reducing environments—available in precision strip and wire forms. They offer superior performance compared to conventional austenitic stainless steels in high-temperature service whilst providing economic advantages over high-nickel alloys where appropriate.
Both are families of nickel-based alloys from Special Metals. INCONEL® grades typically have a higher nickel content and target extreme high-temperature strength/oxidation resistance. INCOLOY® grades are nickel-iron-chromium alloys that balance high-temperature corrosion resistance with cost and thermal-expansion considerations.
The iron content in INCOLOY® alloys is strategically optimised to provide thermal expansion characteristics that closely match those of carbon and low-alloy steels, making them ideal for applications involving dissimilar metal joining. In comparison, INCONEL® alloys have a much higher nickel content, resulting in superior performance at higher temperatures. However, when it comes to material selection, INCOLOY® alloys offer a more economical solution for high-temperature/ corrosive applications that do not need the extended service range of INCONEL® alloys.
Choose INCONEL® alloys for applications requiring excellent strength and corrosion resistance in extreme environments,
Choose INCOLOY® alloys for applications requiring a balance of high-temperature strength, oxidation and carburisation resistance properties at a lower cost.
INCONEL® and INCOLOY® are registered trademarks of Special Metals Corporation.
Choose HAYNES® 25 for excellent high-temperature strength combined with good resistance to oxidising environments up to 980°C (1800°F); the strongest of the fabricable cobalt-base alloys with outstanding resistance to metal galling and cavitation. However, it exhibits thermal instability at intermediate temperatures and has largely been superseded by newer alloys for aerospace applications.
Choose HAYNES® 188 for superior high-temperature strength with excellent oxidation resistance up to 1095°C (2000°F); ideal for combustor liners and gas turbine components that require outstanding fabricability, weldability, and better thermal stability compared to HAYNES® 25. Excellent for prolonged high-temperature service.
Choose HAYNES® 214® for optimum high-temperature oxidation resistance in wrought austenitic materials at temperatures of 955°C (1750°F) and above; forms tightly adherent (Al₂O₃) alumina-type protective oxide scale whilst allowing conventional forming and joining. Susceptible to strain-age cracking at intermediate temperatures.
Choose HAYNES® HR-224® for excellent oxidation resistance with improved fabricability and weldability compared to HAYNES® 214®; it achieves superior oxidation resistance through alumina protective scale formation whilst exhibiting excellent ductility and formability characteristics with enhanced weldability.
Choose HAYNES® 230® for an unparalleled combination of high-temperature strength, outstanding oxidation resistance up to 1149°C (2100°F), and excellent long-term thermal stability; a solid-solution-strengthened alloy with superior resistance to grain coarsening and lower thermal expansion than most high-temperature alloys.
Choose HAYNES® 233® (age-hardenable) for an exceptional combination of excellent oxidation resistance up to 1149°C (2100°F) and superior creep strength; readily fabricable with good hot workability, cold formability, and weldability whilst maintaining excellent high-temperature performance.
Choose HAYNES® 242® (age-hardenable) for applications requiring high strength up to 705°C (1300°F) with exceptionally low thermal expansion characteristics; excellent oxidation resistance up to 815°C (1500°F), outstanding low-cycle fatigue properties, and superior resistance to fluorine-containing environments.
Choose HAYNES® 263 (age-hardenable) for applications up to 900°C (1650°F) requiring good age-hardened strength with excellent fabrication characteristics in the annealed condition; it combines intermediate temperature strength with superior fabricability compared to Waspaloy and R-41 alloys.
Choose HAYNES® 282® (gamma-prime strengthened) for exceptional creep strength in the 649–927°C (1200–1700°F) range with outstanding weldability and fabricability; surpasses Waspaloy and approaches Rene 41 strength while maintaining excellent resistance to strain-age cracking.
Choose HAYNES® HR-120® for excellent strength at elevated temperatures up to 1095°C (2000°F), combined with excellent resistance to carburising and sulphidising environments; significantly higher strength than conventional Fe-Ni-Cr materials whilst maintaining comparable oxidation resistance.
HAYNES® alloys represent the pinnacle of superalloy technology, engineered to withstand the most demanding high-temperature and corrosive environments. These advanced cobalt and nickel-based materials combine exceptional strength, oxidation resistance, and thermal stability, making them suitable for applications where conventional materials fail.
High-Temperature Cobalt-Based Alloys
The cobalt-based HAYNES® alloys (HAYNES® 25, 188) are specifically designed for extreme high-temperature service, where superior strength retention and oxidation resistance at extremely high temperatures are paramount. These solid-solution-strengthened alloys maintain their mechanical properties at temperatures where other materials lose structural integrity, making them indispensable for aerospace and industrial gas turbine applications.
In contrast, the nickel-based grades encompass a comprehensive range from solid-solution-strengthened (230®, HR-120®) to age-hardenable (233®, 242®, 263), gamma-prime strengthened (282®), and advanced alumina-forming alloys (214®, HR-224®).
Advanced Nickel-Based Alloys
HAYNES® nickel-based superalloys incorporate sophisticated metallurgical principles, including solid-solution strengthening (230®, HR-120®), age-hardening mechanisms (233®, 242®, 263), gamma-prime precipitation hardening (282®), and advanced alumina-forming chemistry (214®, HR-224®). These diverse strengthening mechanisms provide tailored performance for specific demanding high-temperature applications whilst maintaining excellent fabricability.
Alumina-forming oxidation alloys: (214®, HR-224®, 233®)
214® and HR-224® (and the newer 233®) rely on aluminium to form a tenacious alumina scale for exceptional oxidation resistance at very high temperature; HR-224® improves fabrication and weldability compared with 214®.
Solid-solution Ni-Cr-W/Mo alloys for oxidation/carburisation (230®, HR-120®)
230® (Ni–Cr–W–Mo) offers a strong combination of oxidation, nitridation and carburisation resistance with good fabrication, making it a go-to alloy for furnace and hot gas path hardware. HR-120® (Fe–Ni–Cr with Co, Mo, W) targets carburising and sulphidising atmospheres while retaining higher strength than many Fe–Ni–Cr grades.
Age-hardenable high-strength alloys (242®, 263, 282®):
Gamma-prime strengthened (Ni–Co–Cr–Mo with Al/Ti) 263 and 282® deliver age-hardened strength; 282® is optimised for superior creep performance around 650–925 °C (1202–1697 °F) with excellent fabricability, while 263 balances strength and weldability to around 900 °C (1652 °F).
Long-range ordering (Ni–Mo–Cr) 242® achieves high strength in the 650–705 °C (1202–1301 °F) band and very low thermal expansion after ageing; ideal where dimensional stability matters.
Supplied as precision strip and wire, HAYNES® alloys are extensively used in aerospace propulsion, industrial gas turbines, power generation, and petrochemical processing—applications including combustor liners, transition ducts, combustors, transition ducts, vanes, seals and hot-gas-path components, heat exchangers, high-temperature furnace components, and chemical processing equipment.
HAYNES® alloys are the preferred choice when your application demands exceptional high-temperature performance, superior oxidation resistance, and proven reliability in the harshest environments—available in precision strip and wire forms. They offer unmatched performance for critical applications where failure is not an option.
HAYNES® alloys are registered trademarks of Haynes International, Inc.
Choose MONEL® 400 when you need broad corrosion resistance in seawater and brackish service, strong performance in reducing acids (including hydrofluoric), and good toughness from cryogenic temperatures upward. It is a single-phase nickel-copper solid solution that hardens only through cold work—ideal for springs, pump and valve components, heat-exchanger hardware, and fasteners in marine and chemical applications.
Choose MONEL® K-500 when you need the same corrosion profile as 400 but with significantly higher strength and hardness from precipitation hardening (aluminium and titanium additions). K-500 is commonly used for shafts, fasteners, springs and down-hole tools; it is essentially non-magnetic to very low temperatures and is widely applied in sour-gas service where specified. Note: In some media, age-hardened K-500 shows a higher tendency to stress-corrosion cracking than 400—consider this in design.
Nickel-copper alloys are single-phase (face-centred cubic) solid solutions across the full Ni–Cu range. This metallurgy gives them excellent resistance to rapidly flowing seawater, excellent behaviour in reducing environments, and functional strength without heat treatment. MONEL 400 is the archetype, typically containing roughly one-third copper; MONEL K-500 adds controlled amounts of aluminium and titanium for precipitation strengthening, while retaining the 400 corrosion profile.
Seawater & marine service: Very low general corrosion in fast-flowing seawater (400 and K-500); proven for pump shafts, propeller shafts and fasteners.
Reducing acids & caustics: Outstanding resistance to hydrofluoric acid and good performance in many reducing media, making it suitable for alkali handling.
Cryogenic toughness: High strength with retention of ductility down to cryogenic temperatures.
Strength options: Alloy400 for cold-worked strength; K-500 for precipitation-hardened high strength and spring performance.
Non-magnetic options: Alloy K-500 is effectively non-magnetic down to very low temperatures, making it useful for instrumentation and down-hole tools.
Strengthening: 400 work-hardens only; K-500 is age-hardened (gamma-prime Ni₃(Al,Ti)) for much higher tensile and fatigue strength.
Corrosion: Similar overall resistance; K-500 can be more sensitive to stress-corrosion cracking in some conditions when age-hardened.
Typical uses: 400 for heat-exchanger hardware, marine fittings, tanks; K-500 for high-strength shafts, fasteners, springs, and sour-service components.
Within both the scientific and lighting industry, glass-to-metal seals present a key challenge to manufacturers. Controlled Expansion Alloys expansion characteristics match both borosilicate (or Pyrex) glasses and alumina ceramics and therefore provide an ideal solution for components that incorporate a hermetic (glass to metal) seal and require good thermal conductivity. Equally, these alloys offer some more unusual characteristics, including their high strength, a low coefficient of thermal expansion and resistance to shock and cracking. As a result, Controlled Expansion Alloys also have significant benefits to electronic manufacturers and can be found in many electrical components and devices such as semiconductors and circuits, thermostat strips and rods, electric bulbs and industrial lamps.
Nickel-Chromium-Cobalt Alloys were introduced in the 1940s for Aerospace applications and now is commonly found in industrial thermal processing, furnace components and heat-treatment equipment. These grades are best suited for applications requiring oxidation and scaling resistance coupled with medium strength at high operating temperatures. Alloy 75 or Nimonic 75 is a Nickel Chromium Alloy, strengthened with the addition of titanium. It provides excellent corrosion resistance at elevated temperatures and is primarily used in low-stress, elevated-temperature conditions, which require some oxidation resistance. This grade remains popular for aerospace applications such as fasteners, in part due to its ease of fabrication and formability. Alloy 90 or Nimonic 90 is another popular aerospace grade nickel-chromium alloy with the addition of cobalt. The alloy is precipitation hardenable and has high strength and corrosion resistance at very high temperatures (up to 950 °C). Other beneficial properties include high-stress rupture strength and high creep resistance at high temperatures making it suitable for a variety of applications in challenging environments.
The optimum condition for alloy 601 depends on the type of application and the service temperature involved. In general, the solution-treated condition is used for rupture-limited applications (temperatures of about 1000°F (540°C) and higher)
| Formula | Formula | Formula | Formula | Formula | Formula | Formula | Formula | Formula | Formula | Formula | Formula | Formula | Formula | Formula | Formula | Formula | Formula |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Commercially Pure Nickel Alloys | |||||||||||||||||
| Commercial Name (Nearest Fit) | UNS (Nearest) | Other Designations (Nearest Fit) | Applicable Specifications | Typical Chemical Composition % | |||||||||||||
| Al | C | Co | Cr | Cu | Fe | Mn | Mo | Ni | P | S | Si | Ti | Others | ||||
| Nickel Alloy 200 (Commercially Pure Nickel) | N02200 | Common Name: Nickel Alloy 200 (Commercially Pure Nickel) European Designation: 2.4066 Other designations may be available by request | European Specifications: DIN 17740 (Strip & Wire), DIN 17750 (Strip) British Specifications: BS NA11 ASTM Specifications: ASTM B162 (Strip) AMS Specifications: AMS 5553 (Strip) Additional specifications may be available by request | - | 0.15 max | - | - | 0.25 max | 0.40 max | 0.35 max | - | 99.0 min | - | 0.01 max | 0.35 max | - | - |
| Nickel Alloy 201 (Low Carbon Nickel) | N02201 | Common Name: Nickel Alloy 201 (Low Carbon Nickel) European Designation: 2.4068 Other designations may be available by request | European Specifications: DIN 17740 (Strip & Wire), DIN 17750 (Strip) British Specifications: BS NA12 ASTM Specifications: ASTM B162 (Strip) AMS Specifications: AMS 5553 (Strip) Additional specifications may be available by request | - | 0.02 max | - | - | 0.25 max | 0.40 max | 0.35 max | - | 99.0 min | - | 0.01 max | 0.35 max | - | - |
| Nickel-Manganese Alloy | |||||||||||||||||
| Nickel® 212 | N02212 | Common Name: Nickel Alloy 212 European Designation: 2.4110 Other designations may be available by request | Please contact us with your requirements. | - | 0.05 max | - | - | 0.30 max | 0.25 max | 1.50-2.20 | - | 97.0 min | - | - | 0.20 max | - | - |
| Legend: “bal.” = balance; “nom.” = nominal; “typ.” = typical; “–” = not typically stated as standard; however, some producers may include traces or add their own limits. The data shown are typical values for reference purposes only. Enforceable limits are set by the relevant standards and producer data sheets. The typical chemical composition is provided for general reference and identification only. It does not constitute a complete or enforceable product specification and should not replace consultation of the relevant standards. Official limits are defined in recognised product specifications (e.g. ASTM, AMS, EN, ISO), which may include tighter ranges, additional minor-element requirements, or restrictions based on product form and manufacturing practice. | |||||||||||||||||
| Inconel® Alloys | |||||||||||||||||
| Commercial Name (Nearest Fit) | UNS (Nearest) | Other Designations (Nearest Fit) | Applicable Specifications | Typical Chemical Composition % | |||||||||||||
| Al | C | Co | Cr | Cu | Fe | Mn | Mo | Ni | P | S | Si | Ti | Others | ||||
| INCONEL® Alloy 600 | N06600 | Common Name: Nickel Alloy 600 European Designation: 2.4816 Other designations may be available by request | British Specifications: BS NA14 ASTM Specifications: ASTM B168 (Strip), ASTM B166 (Wire) AMS Specifications: AMS 5540 (Strip), AMS 5565 (Wire) Additional specifications may be available by request | - | 0.15 max | - | 14.0 - 17.0 | 0.50 max | 6.0 - 10.0 | 1.0 max | - | 72.0 min (bal. with Co) | - | 0.015 max | 0.5 max | - | - |
| INCONEL® alloy 601 | N06601 | Common Name: Nickel Alloy 601 European Designation: 2.4851 Other designations may be available by request | European Specifications: DIN 17750 (Strip) British Specifications: BS NA49 ASTM Specifications: ASTM B168 (Strip), ASTM B166 (Wire) AMS Specifications: AMS 5870 (Strip) Additional specifications may be available by request | 1.0 - 1.70 | 0.10 max | - | 21.0 - 25.0 | 1.00 max | bal. | 1.0 max | - | 58.0 - 63.0 | - | 0.015 max | 0.5 max | - | - |
| INCONEL® alloy 625 | N06625 | Common Name: Nickel Alloy 625 European Designation: 2.4856 Other designations may be available by request | British Specifications: BS NA21 ASTM Specifications: ASTM B443 (Strip), ASTM B446 (Wire) AMS Specifications: AMS 5599 (Strip), AMS 5666 (Wire), AMS 5837 (Wire) Other Specifications: NACE MR0175 (ISO 15156-3) (Strip & Wire), NACE MR0103/ISO 17945 (Strip & Wire) Additional specifications may be available by request | 0.4 max | 0.10 max | - | 20.0 - 23.0 | - | 5.0 max | 0.5 max | 8.0 - 10.0 | bal. | 0.015 max | 0.015 max | 0.5 max | 0.40 max | Nb + Ta: 3.15 - 4.15 |
| INCONEL® alloy 718 | N07718 | Common Name: Nickel Alloy 718 European Designation: 2.4668 Other designations may be available by request | British Specifications: BS NA51 ASTM Specifications: ASTM B670 (Strip) AMS Specifications: AMS 5596 (Strip) AMS 5597(Strip), AMS 5832 (Wire), AMS 5962 (Wire), Other Specifications: NACE MR0175 (ISO 15156-3 (Wire) Additional specifications may be available by request | 0.20 - 0.80 | 0.08 max | 1.00 max | 17.0 - 21.0 | 0.30 max | bal. | 0.35 max | 2.80 - 3.30 | 50.0 - 55.0 | 0.015 max | 0.015 max | 0.35 max | 0.65 - 1.15 | Nb + Ta: 4.75 - 5.50 B: 0.006 max |
| INCONEL® X-750 | N07750 | Common Name: Nickel Alloy X750 European Designation: 2.4669 Other designations may be available by request | ASTM Specifications: ASTM B637 (Wire) AMS Specifications: AMS 5542 (Strip), AMS 5598 (Strip), AMS 5698 (Wire), AMS 5699 (Wire), AMS 5778 (Wire) Other Specifications: NACE MR0175 (ISO 15156-3 (Wire) Additional specifications may be available by request | 0.40 - 1.00 | 0.08 max | - | 14.0 - 17.0 | 0.5 max | 5.0 - 9.0 | 1.00 max | - | Ni + Co: 70.0 min | - | 0.01 max | 0.50 max | 2.25 - 2.75 | Nb + Ta: 0.70 - 1.20 |
| INCONEL® is a registered trademark of Special Metals Corporation®. Legend: “bal.” = balance; “nom.” = nominal; “typ.” = typical; “–” = not typically stated as standard; however, some producers may include traces or add their own limits. The data shown are typical values for reference purposes only. Enforceable limits are set by the relevant standards and producer data sheets. The typical chemical composition is provided for general reference and identification only. It does not constitute a complete or enforceable product specification and should not replace consultation of the relevant standards. Official limits are defined in recognised product specifications (e.g. ASTM, AMS, EN, ISO), which may include tighter ranges, additional minor-element requirements, or restrictions based on product form and manufacturing practice. | |||||||||||||||||
| Incoloy® Alloys | |||||||||||||||||
| Commercial Name (Nearest Fit) | UNS (Nearest) | Other Designations (Nearest Fit) | Applicable Specifications | Typical Chemical Composition % | |||||||||||||
| Al | C | Co | Cr | Cu | Fe | Mn | Mo | Ni | P | S | Si | Ti | Others | ||||
| INCOLOY® A-286 | S66286 | Common Name: Nickel A-286 European Designation: 1.4980 Other designations may be available by request | AMS Specifications: AMS 5525 (Strip) AMS 5858 (Strip), AMS 5726 (Wire), AMS 5731 (Wire), AMS 5732 (Wire), AMS 5734 (Wire), AMS 5737 (Wire), AMS 5804 (Wire), AMS 5805 (Wire), AMS 5810 (Wire), AMS 5853 (Wire) Other Specifications: NACE MR0175 (ISO 15156-3) (Wire) Additional specifications may be available by request | 0.35 max | 0.08 max | - | 13.5 – 16.0 | - | bal. | 2.0 max | 1.0 – 1.5 | 24.0 – 27.0 | 0.040 max | 0.030 max | 1.0 max | 1.90 – 2.35 | V: 0.1 – 0.5 B: 0.001 - 0.010 |
| INCOLOY® alloy 800 | N08800 | Common Name: Nickel Alloy 800 European Designation: 1.4876 Other designations may be available by request | British Specifications: BS NA15 ASTM Specifications: ASTM B409 (Strip), ASTM A240 (Strip) AMS Specifications: AMS 5871 (Strip) Additional specifications may be available by request | 0.15 - 0.60 | 0.10 max | - | 19.0 - 23.0 | 0.75 max | bal. | 1.5 max | - | 30.0 - 35.0 | - | 0.015 max | 1.0 max | 0.15 - 0.60 | - |
| INCOLOY® alloy 825 | N08825 | Common Name: Nickel Alloy 825 European Designation: 2.4858 Other designations may be available by request | British Specifications: BS NA16 ASTM Specifications: ASTM B424 (Strip) Other Specifications: NACE MR0175/ISO 15156 (Strip & Wire) , NACE MR0103 (Wire) Additional specifications may be available by request | 0.2 max | 0.05 max | - | 19.5 - 23.5 | 1.50 - 3.00 | bal. | 1.0 max | 2.5 - 3.5 | 38.0 - 46.0 | - | 0.03 max | 0.5 max | 0.60 - 1.20 | - |
| INCOLOY® 925 | N09925 | Common Name: Nickel Alloy 925 Other designations may be available by request | Other Specifications: NACE MR0175/ISO 15156 (Wire), NACE MR0103 (Wire) Additional specifications may be available by request | 0.1 – 0.5 | 0.03 max | - | 19.5 – 22.5 | 1.5 – 3.0 | 22.0 min | 1.0 max | 2.5 – 3.5 | 42.0 – 46.00 | - | 0.03 max | 0.5 max | 1.9 – 2.4 | Nb (Cb): 0.5 max |
| INCOLOY® 25-6MO Alloy | N08926 | Common Name: Nickel Alloy European Designation: 1.4529 Other designations may be available by request | Please contact us with your requirements. | – | 0.02 max | – | 19.0 – 21.0 | 0.5 – 1.5 | bal. | 2.0 max | 6.0 – 7.0 | 24.0 – 26.0 | 0.03 max | 0.010 max | 0.5 max | – | N: 0.15 – 0.25 |
| INCOLOY® is a registered trademark of Special Metals Corporation®. Legend: “bal.” = balance; “nom.” = nominal; “typ.” = typical; “–” = not typically stated as standard; however, some producers may include traces or add their own limits. The data shown are typical values for reference purposes only. Enforceable limits are set by the relevant standards and producer data sheets. The typical chemical composition is provided for general reference and identification only. It does not constitute a complete or enforceable product specification and should not replace consultation of the relevant standards. Official limits are defined in recognised product specifications (e.g. ASTM, AMS, EN, ISO), which may include tighter ranges, additional minor-element requirements, or restrictions based on product form and manufacturing practice. | |||||||||||||||||
| Hastelloy® Alloys | |||||||||||||||||
| Commercial Name (Nearest Fit) | UNS (Nearest) | Other Designations (Nearest Fit) | Applicable Specifications | Typical Chemical Composition % | |||||||||||||
| Al | C | Co | Cr | Cu | Fe | Mn | Mo | Ni | P | S | Si | Ti | Others | ||||
| HASTELLOY® B-3 | N10675 | Common Name: Nickel Alloy B3 European Designation: 2.4600 Other designations may be available by request | Please contact us with your requirements. | 0.50 max | 0.01 max | 3.00 max | 1.00 – 3.00 | 0.20 max | 1.00 – 3.00 | 3.00 max | 27.00 – 32.00 | bal. | - | - | 0.10 max | 0.2 max | Nb (Cb): 0.20 max Ta: 0.20 max V: 0.20 max Zr: 0.10 max |
| HASTELLOY® C-4 | N06455 | Common Name: Nickel Alloy C4 European Designation: 2.4610 Other designations may be available by request | ASTM Specifications: ASTM B575 (Strip) Other Specifications: NACE MR0175 (Strip), NACE MR0175 (ISO 15156-3) (Wire) Additional specifications may be available by request | - | 0.015 max | 2.0 max | 14.0 – 18.0 | - | 3.0 max | 1.0 max | 14.00 – 17.00 | bal. | 0.04 max | 0.030 max | 0.08 max | 0.7 max | - |
| HASTELLOY® C22® | N06022 | Common Name: Nickel Alloy C22 European Designation: 2.4602 Other designations may be available by request | ASTM Specifications: ASTM B575 (Strip) Other Specifications: NACE MR0175 (Strip), NACE MR0175 (ISO 15156-3) (Wire) Additional specifications may be available by request | - | 0.015 max | 2.5 max | 20.0 - 22.5 | - | 2.0 - 6.0 | 0.5 max | 12.50 - 14.50 | bal. | - | - | 0.08 max | - | W: 2.5-3.5 V: 0.35 max |
| HASTELLOY® C-276® | N10276 | Common Name: Nickel Alloy C 276 European Designation: 2.4819 Other designations may be available by request | European Specifications: DIN 17750 (Strip) ASTM Specifications: ASTM B575 (Strip), ASTM B906 (Strip) Other Specifications: NACE MR0175 (ISO 15156-3) (Wire) Additional specifications may be available by request | - | 0.02 max | 2.5 max | 14.5 - 16.5 | - | 4.0 - 7.0 | 1.0 max | 15.00 - 17.00 | bal. | 0.030 max | 0.030 max | 0.05 max | - | V: 0.35 max W: 3.0 - 4.5 |
| HASTELLOY® alloy C 2000 | N06200 | Common Name: Nickel Alloy C2000 European Designation: 2.4675 Other designations may be available by request | ASTM Specifications: ASTM B575 (Strip) Other Specifications: NACE MR0175 (ISO 15156-3) (Wire) Additional specifications may be available by request | 0.5 max | 0.01 max | 2.0 max | 22.0 - 24.0 | 1.3 - 1.9 | 3.0 max | 0.5 max | 15.00 - 17.00 | bal. | - | - | 0.08 max | - | - |
| HASTELLOY® X | N06002 | Common Name: Nickel Alloy X European Designation: 2.4665 Other designations may be available by request | AMS Specifications: AMS 5536 (Strip), AMS 5798 (Wire) Other Specifications: DMD 0491 (Wire), GE B21B111 (Wire) Additional specifications may be available by request | - | 0.05 - 0.15 | 0.50 - 2.50 | 20.50 - 23.00 | 0.5 max | 17.00 - 20.00 | 1.0 max | 8.00 - 10.00 | bal. | 0.040 max | 0.030 max | 1.00 max | - | W: 0.20 - 1.00 |
| HASTELLOY®is a registered trademark of Haynes International Inc®. Legend: “bal.” = balance; “nom.” = nominal; “typ.” = typical; “–” = not typically stated as standard; however, some producers may include traces or add their own limits. The data shown are typical values for reference purposes only. Enforceable limits are set by the relevant standards and producer data sheets. The typical chemical composition is provided for general reference and identification only. It does not constitute a complete or enforceable product specification and should not replace consultation of the relevant standards. Official limits are defined in recognised product specifications (e.g. ASTM, AMS, EN, ISO), which may include tighter ranges, additional minor-element requirements, or restrictions based on product form and manufacturing practice. | |||||||||||||||||
| Haynes® Alloys | |||||||||||||||||
| Commercial Name (Nearest Fit) | UNS (Nearest) | Other Designations (Nearest Fit) | Applicable Specifications | Typical Chemical Composition % | |||||||||||||
| Al | C | Co | Cr | Cu | Fe | Mn | Mo | Ni | P | S | Si | Ti | Others | ||||
| Haynes® HR-120® Alloy | N08120 | European Designation: 2.4854 Other designations may be available by request | Please contact us with your requirements. | 0.40 max | 0.02-0.10 | 3.00 max | 23.0 – 27.0 | 0.50 max | bal. | 1.50 max | 2.50 max | 35.0 - 39.0 | 0.040 max | 0.03 max | 1.0 max | 0.20 max | W: 2.50 max B: 0.01 max Nb (Cb): 0.40 – 0.90 N: 0.15 – 0.30 |
| HAYNES® 214 | N07214 | Common Name: Nickel Alloy 214 European Designation: 2.4646 Other designations may be available by request | Please contact us with your requirements. | 4.5-5.0 | 0.05 | 2.0 max | 15.0 - 17.0 | - | 2.0 – 4.0 | 0.05 max | 0.05 max | bal. | 0.015 max | 0.015 max | 0.20 max | 0.50 max | W: 0.5 max B: 0.006 max Y: 0.002-0.004 Zr 0.05 max |
| HAYNES® 224 | - | Common Name: Nickel Alloy 224 Other designations may be available by request | Please contact us with your requirements. | 3.10 - 3.90 | 0.30-0.07 | 2.0 max | 19.0-21.0 | - | 25.0-30.0 | 0.20- 0.50 | 0.5 max | bal. | - | - | 0.30 - 0.50 | 0.20-0.50 | Zr: 0.025 nom. B: 0.004 nom. Nb (Cb): 0.15 nom. |
| HAYNES® 230 | N06230 | Common Name: Nickel Alloy 230 European Designation: 2.4733 Other designations may be available by request | ASTM Specifications: ASTM B435 (Strip) AMS Specifications: AMS 5878 (Strip) Additional specifications may be available by request | 0.20 – 0.50 | 0.05 – 0.15 | 5.0 max | 20.0 – 24.0 | - | 3.00 max | 0.30 – 1.00 | 1.00 – 3.00 | bal. | 0.030 max | 0.015 max | 0.25 – 0.75 | - | W: 13.0 – 15.0 La: 0.01 – 0.05 B: 0.015 max |
| HAYNES® 233 | N02233 | Common Name: Nickel Alloy 233 Other designations may be available by request | Please contact us with your requirements. | - | 0.15 max | - | - | 0.10 max | 0.10 max | 0.30 max | - | 99.00 min | - | 0.008 max | 0.10 max | 0.005 max | - |
| HAYNES® 242 | N10242 | Common Name: Nickel Alloy 242 European Designation: 2.4816 Other designations may be available by request | Please contact us with your requirements. | 0.50 max | 0.03 max | 1.0 max | 7.0 - 9.0 | 0.50 max | 2.0 max | 0.80 max | 24.0 – 26.0 | bal. | 0.03 max | 0.015 max | 0.80 max | - | B: 0.006 max |
| HAYNES® 263 | N07263 | Common Name: Nickel Alloy 263 European Designation: 2.4650 Other designations may be available by request | AMS Specifications: AMS 5872 (Strip) Additional specifications may be available by request | 0.30 – 0.60 | 0.04 – 0.08 | 19.0 – 21.0 | 19.0 – 21.0 | 0.20 max | 0.70 max | 0.60 max | 5.60 – 6.10 | bal. | 0.015 max | 0.007 max | 0.40 max | 1.90 – 2.40 | B: 0.005 max Tl+Al: 2.4-2.8 |
| HAYNES® 282 | N07208 | Common Name: Nickel Alloy 282 Other designations may be available by request | AMS Specifications: AMS 5951 (Strip) Additional specifications may be available by request | 1.38 – 1.65 | 0.04 – 0.08 | 9.0 – 11.0 | 18.5-20.5 | 0.1 max | 1.5 max | 0.30 max | 8.0 – 9.0 | bal. | 0.015 max | 0.015 max | 0.15 max | 1.90 – 2.30 | B: 0.003 – 0.010 |
| Haynes® 25 / L605 | R30605 | European Designation: 2.4964 / 2.4967 Other designations may be available by request | ASTM Specifications: ASTM F90 (Wire) AMS Specifications: AMS 5537 (Strip & Foil), AMS 5796 (Wire) Other Specifications: Rolls Royce MSRR 7053, NACE MR0175/ISO 15156-3, ISO 5832-5 Additional specifications may be available by request | - | 0.05 – 0.15 | bal. | 19.0 – 21.0 | - | 3.00 max | 2.0 max | - | 9.0 – 11.0 | - | - | 1.00 max | - | W: 14.0 – 16.0 |
| Haynes® 188 Alloy | R30188 | European Designation: 2.4683 Other designations may be available by request | AMS Specifications: AMS 5608 (Strip & Foil) Other Specifications: GE B50A712, PWA 1042, Rolls Royce MSRR 7165 Additional specifications may be available by request | - | 0.05 – 0.15 | bal. | 20.0 – 24.0 | - | 3.00 max | 1.25 max | - | 20.0 – 24.0 | - | - | 0.20 – 0.50 | - | W:13.0 – 16.0 La: 0.03 – 0.15 |
| Rene® | |||||||||||||||||
| Commercial Name (Nearest Fit) | UNS (Nearest) | Other Designations (Nearest Fit) | Applicable Specifications | Typical Chemical Composition % | |||||||||||||
| Al | C | Co | Cr | Cu | Fe | Mn | Mo | Ni | P | S | Si | Ti | Others | ||||
| RENE®41 | N07041 | Common Name: Nickel Alloy 41 European Designation: 2.4973 Other designations may be available by request | AMS Specifications: AMS 5545 (Strip), AMS 5800 (Wire) Other Specifications: GE B50T59 (Strip), GE B50TF109 (Strip) Additional specifications may be available by request | 1.40-1.80 | 0.12 max | 10.0-12.0 | 18.0-20.0 | - | 5.0 max | 0.10 max | 9.0-10.5 | bal. | - | 0.015 max | 0.50 max | 3.0-3.3 | B: 0.003-0.010 |
| RENE® is a registered trademark of General Electric Inc.® Legend: “bal.” = balance; “nom.” = nominal; “typ.” = typical; “–” = not typically stated as standard; however, some producers may include traces or add their own limits. The data shown are typical values for reference purposes only. Enforceable limits are set by the relevant standards and producer data sheets. The typical chemical composition is provided for general reference and identification only. It does not constitute a complete or enforceable product specification and should not replace consultation of the relevant standards. Official limits are defined in recognised product specifications (e.g. ASTM, AMS, EN, ISO), which may include tighter ranges, additional minor-element requirements, or restrictions based on product form and manufacturing practice. | |||||||||||||||||
| Waspaloy® | |||||||||||||||||
| Commercial Name (Nearest Fit) | UNS (Nearest) | Other Designations (Nearest Fit) | Applicable Specifications | Typical Chemical Composition % | |||||||||||||
| Al | C | Co | Cr | Cu | Fe | Mn | Mo | Ni | P | S | Si | Ti | Others | ||||
| WASPALOY® | N07001 | European Designation: 2.4654 Other designations may be available by request | AMS Specifications: AMS 5544 (Strip) AMS 5828 (Wire) Additional specifications may be available by request | 1.20 – 1.60 | 0.03-0.10 | 12.0 – 15.0 | 18.0 – 21.0 | 0.50 max | 2.0 max | 1.0 max | 3.50 – 5.00 | bal. | 0.030 max | 0.030 max | 0.75 max | 2.75 – 3.25 | B: 0.003 – 0.01 Zr: 0.02 – 0.12 |
| WASPALOY® is a registered trademark of United Technologies Corporation®. Legend: “bal.” = balance; “nom.” = nominal; “typ.” = typical; “–” = not typically stated as standard; however, some producers may include traces or add their own limits. The data shown are typical values for reference purposes only. Enforceable limits are set by the relevant standards and producer data sheets. The typical chemical composition is provided for general reference and identification only. It does not constitute a complete or enforceable product specification and should not replace consultation of the relevant standards. Official limits are defined in recognised product specifications (e.g. ASTM, AMS, EN, ISO), which may include tighter ranges, additional minor-element requirements, or restrictions based on product form and manufacturing practice. | |||||||||||||||||
| Monel® Alloys | |||||||||||||||||
| Commercial Name (Nearest Fit) | UNS (Nearest) | Other Designations (Nearest Fit) | Applicable Specifications | Typical Chemical Composition % | |||||||||||||
| Al | C | Co | Cr | Cu | Fe | Mn | Mo | Ni | P | S | Si | Ti | Others | ||||
| MONEL® alloy 400 | N04400 | Common Name: Nickel Alloy 400 European Designation: 2.4360 / 2.4361 Other designations may be available by request | British Specifications: BS NA13 (Wire) ASTM Specifications: ASTM B127 (Strip), ASTM B164 (Wire) AMS Specifications: AMS 4544 (Strip), AMS 4730 (Wire) Other Specifications: ASME SB-127 (Strip), NACE MR0175 (ISO 1516-3) (Wire) Additional specifications may be available by request | - | 0.30 max | - | - | bal. | 2.5 max | 2.0 max | - | 63.0–70.0 | - | 0.024 max | 0.50 max | - | - |
| MONEL® alloy K500 | N05500 | Common Name: Nickel Alloy K500 European Designation: 2.4375 Other designations may be available by request | British Specifications: BS NA18 (Wire) ASTM Specifications: ASTM B127 (Strip), ASTM B164 (Wire) AMS Specifications: AMS 4676 (Wire) Additional specifications may be available by request | 2.30 - 3.15 | 0.25 max | - | - | bal. | 2.0 max | 1.5 max | - | 63.0–70.0 | - | 0.01 max | 0.50 max | 0.35 - 0.85 | - |
| MONEL® is a registered trademark of Special Metals Corporation®. Legend: “bal.” = balance; “nom.” = nominal; “typ.” = typical; “–” = not typically stated as standard; however, some producers may include traces or add their own limits. The data shown are typical values for reference purposes only. Enforceable limits are set by the relevant standards and producer data sheets. The typical chemical composition is provided for general reference and identification only. It does not constitute a complete or enforceable product specification and should not replace consultation of the relevant standards. Official limits are defined in recognised product specifications (e.g. ASTM, AMS, EN, ISO), which may include tighter ranges, additional minor-element requirements, or restrictions based on product form and manufacturing practice. | |||||||||||||||||
| Nimonic® Alloys | |||||||||||||||||
| Commercial Name (Nearest Fit) | UNS (Nearest) | Other Designations (Nearest Fit) | Applicable Specifications | Typical Chemical Composition % | |||||||||||||
| Al | C | Co | Cr | Cu | Fe | Mn | Mo | Ni | P | S | Si | Ti | Others | ||||
| NIMONIC® alloy 75 | N06075 | Common Name: Nickel Alloy 75 European Designation: 2.4951 Other designations may be available by request | British Specifications: BS 2HR 203:2009 (Strip) Additional specifications may be available by request | - | 0.08 – 0.15 | - | 18.0 – 21.0 | 0.5 max | 5.0 max | 1.0 max | - | Bal. | - | - | 1.0 max | 0.20 – 0.60 | - |
| NIMONIC® alloy 90 | N07090 | Common Name: Nickel Alloy 90 European Designation: 2.4632 / 2.4969 Other designations may be available by request | British Specifications: BS NA19 (Wire), BS HR 501 (Wire), BS HR 502 (Wire), BS HR 503 (Wire) AMS Specifications: AMS 5829 (Wire) Other Specifications: NACE MR0175 / ISO 15156-3 (Wire), NACE MR0103 (Wire) Additional specifications may be available by request | 0.8 - 2.0 | 0.13 max | 15.0 - 21.0 | 18.0 - 21.0 | - | 3.0 max | 1.0 max | - | Bal. | - | - | 1.5 max | 1.80 - 3.00 | - |
| NIMONIC® is a registered trademark of Special Metals Corporation®. Legend: “bal.” = balance; “nom.” = nominal; “typ.” = typical; “–” = not typically stated as standard; however, some producers may include traces or add their own limits. The data shown are typical values for reference purposes only. Enforceable limits are set by the relevant standards and producer data sheets. The typical chemical composition is provided for general reference and identification only. It does not constitute a complete or enforceable product specification and should not replace consultation of the relevant standards. Official limits are defined in recognised product specifications (e.g. ASTM, AMS, EN, ISO), which may include tighter ranges, additional minor-element requirements, or restrictions based on product form and manufacturing practice. | |||||||||||||||||
| Nichrome Electrical Resistance Alloys | |||||||||||||||||
| Commercial Name (Nearest Fit) | UNS (Nearest) | Other Designations (Nearest Fit) | Applicable Specifications | Typical Chemical Composition % | |||||||||||||
| Al | C | Co | Cr | Cu | Fe | Mn | Mo | Ni | P | S | Si | Ti | Others | ||||
| Nichrome 40 37/18 Ni Cr Resistance Wire Ni Cr 37/18 (D Grade Family) | - | Common Name: Nichrome 40 37/18 Ni Cr Resistance Wire Ni Cr 37/18 (D Grade Family) Other designations may be available by request | Please contact us with your requirements. | - | - | - | 18.0 nom. | - | bal. | - | - | 37.0 nom. | - | - | ~ 2.0 | - | - |
| Nichrome 60 60/15/ Ni Cr Resistance Wire Ni Cr 60/15 (C Grade Family) | N06004 | Common Name: Nichrome 60 60/15/ Ni Cr Resistance Wire Ni Cr 60/15 (C Grade Family) European Designation: 2.4867 Other designations may be available by request | European Specifications: DIN 17470 (Wire) British Specifications: ASTM B344 (Wire) Additional specifications may be available by request | - | 0.15 max | - | 14.0 - 18.0 | - | bal. | 1.0 max | - | min 57.0 | - | 0.01 max | 0.75 - 1.6 | - | - |
| Nichrome 80 80/20 Ni Cr Resistance Wire Ni Cr 80/20 (A Grade Family) | N06003 | Common Name: Nichrome 80 80/20 Ni Cr Resistance Wire Ni Cr 80/20 (A Grade Family) European Designation: 2.4869 Other designations may be available by request | European Specifications: DIN 17470 (Wire) British Specifications: ASTM B344 (Wire) Additional specifications may be available by request | - | 0.15 max | - | 19.0 - 21.0 | - | 1.0 max | 2.5 max | - | bal. | - | 0.01 max | 0.75 - 1.6 | - | - |
| Nilo® Alloys (Controlled Expansion Alloys / Glass Sealing Nickel Alloys) | |||||||||||||||||
| Commercial Name (Nearest Fit) | UNS (Nearest) | Other Designations (Nearest Fit) | Applicable Specifications | Typical Chemical Composition % | |||||||||||||
| Al | C | Co | Cr | Cu | Fe | Mn | Mo | Ni | P | S | Si | Ti | Others | ||||
| Nilo® K / KOVAR® | K94610 | Common Name: Alloy 29/18 European Designation: 1.3981 Other designations may be available by request | European Specifications: DIN 17745 (Wire) ASTM Specifications: ASTM F15 (Strip & Wire) Additional specifications may be available by request | 0.10 max | 0.05 max | 17.0 nom. | 0.20 max | 0.20 max | 53.0 nom. | 0.50 max | 0.20 max | 29.0 nom. | - | - | 0.20 max | 0.10 max | Zr: 0.10 max Mg: 0.10 max Al + Mg + Zr + Ti 0.20 max |
| Nilo® 36 / Invar 36® | K93600 | Common Name: NiFe36 Alloy 36 European Designation: 1.3912 Other designations may be available by request | Please contact us with your requirements. | - | - | - | - | - | 64.0 | - | - | 36.0 | - | - | - | - | - |
| Nilo® 42 | K94100 | Common Name: NiFe42 Alloy 42 European Designation: 1.3917 Other designations may be available by request | European Specifications: DIN 17745 (Wire) ASTM Specifications: ASTM F30 (Wire) Additional specifications may be available by request | 0.10 max | 0.05 max | - | 0.25 max | - | bal. | 0.80 max | - | 41.0 nom. | 0.025 max | 0.025 max | 0.30 max | - | |
| Nilo® 48 | K94800 | Common Name: NiFe48 Alloy 48 European Designation: 1.3922 Other designations may be available by request | European Specifications: DIN 17745 (Wire) ASTM Specifications: ASTM F30 (Wire) Additional specifications may be available by request | 0.10 max | 0.05 max | - | 0.25 max | - | bal. | 0.80 max | - | 46.0 nom. | 0.025 max | 0.025 max | 0.30 max | - | - |
| Nilo® 52 | N14052 | Common Name: NiFe52 Alloy 52 European Designation: 2.4478 Other designations may be available by request | Please contact us with your requirements. | 0.10 max | 0.05 max | 0.50 max | 0.25 max | - | bal. | 0.60 max | - | 50.5 nom. | 0.025 max | 0.025 max | 0.30 max | - | - |
| NILO® is a registered trademark of Special Metals Corporation®. Legend: “bal.” = balance; “nom.” = nominal; “typ.” = typical; “–” = not typically stated as standard; however, some producers may include traces or add their own limits. The data shown are typical values for reference purposes only. Enforceable limits are set by the relevant standards and producer data sheets. The typical chemical composition is provided for general reference and identification only. It does not constitute a complete or enforceable product specification and should not replace consultation of the relevant standards. Official limits are defined in recognised product specifications (e.g. ASTM, AMS, EN, ISO), which may include tighter ranges, additional minor-element requirements, or restrictions based on product form and manufacturing practice. | |||||||||||||||||
| Ni-Span-C® | |||||||||||||||||
| Commercial Name (Nearest Fit) | UNS (Nearest) | Other Designations (Nearest Fit) | Applicable Specifications | Typical Chemical Composition % | |||||||||||||
| Al | C | Co | Cr | Cu | Fe | Mn | Mo | Ni | P | S | Si | Ti | Others | ||||
| NI-SPAN-C® ALLOY 902 | N09902 | Other designations may be available by request | AMS Specifications: AMS 5221 (Wire) AMS 5225 (Wire) Additional specifications may be available by request | 0.30 – 0.80 | 0.06 max | - | 4.90-5.75 | - | bal. | 0.80 max | - | 41.0-43.5 | 0.04 max | 0.040 max | 1.00 max | 2.20 – 2.75 | - |
| NI-SPAN® is a registered trademark of Special Metals Corporation®. Legend: “bal.” = balance; “nom.” = nominal; “typ.” = typical; “–” = not typically stated as standard; however, some producers may include traces or add their own limits. The data shown are typical values for reference purposes only. Enforceable limits are set by the relevant standards and producer data sheets. The typical chemical composition is provided for general reference and identification only. It does not constitute a complete or enforceable product specification and should not replace consultation of the relevant standards. Official limits are defined in recognised product specifications (e.g. ASTM, AMS, EN, ISO), which may include tighter ranges, additional minor-element requirements, or restrictions based on product form and manufacturing practice. | |||||||||||||||||
| Link to Cobalt F/A | Link to Resistance Nickel Alloys | English - Strip | ||||||||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| TYPICAL MECHANICAL PROPERTIES OF NICKEL ALLOY STRIP | ||||||||||||||||||
| COMMERCIALLY PURE NICKEL - STRIP MECHANICAL PROPERTIES | ||||||||||||||||||
| Designations | Applicable Specifications | Tempers Available | Tensile Strength | Proof Strength 0.2% | Elong. % Min. (50mm Gauge Length) | Hardness | ||||||||||||
| Commercial Name | Common Name (nearest fit | UNS (nearest fit) | European Designation (nearest fit) | European Standard (nearest fit) | British Standard (nearest fit) | ASTM (nearest fit) | AMS (nearest fit) | Other Standards | MPa | ksi | MPa | ksi | Vickers (VPN) | Rockwell (HRB) | ||||
| - | Nickel Alloy 200 (Commercially Pure Nickel) | N02200 | 2.4066 | DIN 17740 (Strip & Wire), DIN 17750 (Strip) | BS NA11 | ASTM B162 (Strip) | AMS 5553 (Strip) | - | Annealed | 380-520 | 55-75 | ≈105-310 | 15-45 | 40-55 | ≤117 | 64 max. | ||
| Spring Temper | 620-895 | 90-130 | 485-795 | 70-115 | 2-15 | ≥210 | 95 min. | |||||||||||
| - | Nickel Alloy 201 (Low Carbon Nickel) | N02201 | 2.4068 | DIN 17740 (Strip & Wire), DIN 17750 (Strip) | BS NA12 | ASTM B162 (Strip) | AMS 5553 (Strip) | - | Annealed | 340-520 | 49-75 | 70-170 | 10-25 | ≥50 | <125 | <55 | ||
| Spring Temper | 700-900 | 102-131 | 480-620 | 70-90 | 8-35 | <210 | 70–95 | |||||||||||
| NICKEL® 212 - STRIP MECHANICAL PROPERTIES | ||||||||||||||||||
| Nickel® 212 | Nickel Alloy 212 | N02212 | 2.4110 | - | - | - | - | - | Wire Grade | |||||||||
| INCONEL® - STRIP MECHANICAL PROPERTIES | ||||||||||||||||||
| Designations | Specifications | Tempers Available | Tensile Strength | Proof Strength 0.2% | Elong. % Min. (50mm Gauge Length) | Hardness | ||||||||||||
| Commercial Name | Common Name | UNS (nearest fit) | European Designation (nearest fit) | European Standard (nearest fit) | British Standard (nearest fit) | ASTM (nearest fit) | AMS (nearest fit) | Other Standards | MPa | ksi | MPa | ksi | Vickers (VPN) | Rockwell (HRB) | ||||
| Inconel® Alloy 600 | Nickel Alloy 600 | N06600 | 2.4816 | - | BS NA14 | ASTM B168 (Strip) ASTM B166 (Wire) | AMS 5540 (Strip) AMS 5565 (Wire) | - | Annealed | 552-758 | 80-110 | 241-345 | 35-50 | 30-45 | 160-190 | 80-95 HRB | ||
| Spring Temper | 862-1275 | 125-185 | 760-1100 | 110-160 | 5-15 | 200-230 | 80-95 HRB | |||||||||||
| INCONEL® alloy 601 | Nickel Alloy 601 | N06601 | 2.4851 | DIN 17750 (Strip) | BS NA49 | ASTM B168 (Strip) ASTM B166 (Wire) | AMS 5870 (Strip) | - | Annealed | 552 min | 80 min 95 typical | 270-380 | 39-55 | 30-40 | 170-200 | 82-98 | ||
| Spring Temper | 1240-1448 | 180-210 | 1000-1200 | 145-174 | 8-15 | 210-250 | 82-98 | |||||||||||
| INCONEL® alloy 625 | Nickel Alloy 625 | N06625 | 2.4856 | - | BS NA21 | ASTM B443 (Strip) ASTM B446 (Wire) | AMS 5599 (Strip) AMS 5666 (Wire) AMS 5837 (Wire) | NACE MR0175 (ISO 15156-3) (Strip & Wire) NACE MR0103/ISO 17945 (Strip & Wire) | Annealed | 830-1100 | 120-150 | 414-517 | 60-75 | 30-42 | 200-230 | 85-100 HRB | ||
| Hard | 1300-1600 | 189-232 | 1035-1380 | 150-200 | 10-20 | 350-500 | C20-25 (HRC) | |||||||||||
| Spring Temper | 1380-1724 | 200-250 | 1200-1450 | 174-210 | 5-12 | 240-310 | C38-45 (HRC) | |||||||||||
| INCONEL® alloy 718 | Nickel Alloy 718 | N07718 | 2.4668 | - | BS NA51 | ASTM B670 (Strip) | AMS 5596 (Strip) AMS 5597(Strip) AMS 5832 (Wire) AMS 5962 (Wire) | NACE MR0175 (ISO 15156-3 (Wire) | Annealed | 830-965 | 120-140 | 345-480 | 50-70 | 25-35 | 250-300 | C32-C40 (HRC) | ||
| Spring Temper | 1240-1585 | 180-230 | 800-1000 | 116-145 | 8-12 | 330-400 | C32-C40 | |||||||||||
| Precipitation Hardened | 1310-1655 | 190-240 | 1034-1310 | 150-190 | 10-20 | 370-450 | C38-C45 | |||||||||||
| INCONEL® X-750 | Nickel Alloy X750 | N07750 | 2.4669 | - | - | ASTM B637 (Wire) | AMS 5542 (Strip) AMS 5598 (Strip) AMS 5698 (Wire) AMS 5699 (Wire) AMS 5778 (Wire) | NACE MR0175 (ISO 15156-3 (Wire) | Annealed | 896 max | 130 max | 310-415 | 45-60 | 30 | 200-250 | B90-C22 | ||
| Spring Temper | 1100-1517 | 160-220 | 750-950 | 109-138 | 6-10 | 330-390 | C32-C40 (HRC) | |||||||||||
| Precipitation Hardened | 1100 min | 160 min | 760-1150 | 110-168 | 15-20 | 350-420 | C35-C42 (HRC) | |||||||||||
| INCONEL® IS A REGISTERED TRADEMARK OF SPECIAL METALS CORPORATION® | ||||||||||||||||||
| INCOLOY® - STRIP MECHANICAL PROPERTIES | ||||||||||||||||||
| Designations | Specifications | Strip Tempers Available | Tensile Strength | Proof Strength 0.2% | Elong. % Min. (50mm Gauge Length) | Hardness | ||||||||||||
| Commercial Name | Common Name | UNS (nearest fit) | European Designation (nearest fit) | European Standard (nearest fit) | British Standard (nearest fit) | ASTM (nearest fit) | AMS (nearest fit) | Other Standards | MPa | ksi | MPa | ksi | Vickers (VPN) | Rockwell (HRB) | ||||
| INCOLOY® A-286 | Nickel A-286 GE B50T12 (Strip) | S66286 | - | 1.4980 | - | - | AMS 5525 (Strip) AMS 5858 (Strip) AMS 5726 (Wire) AMS 5731 (Wire) AMS 5732 (Wire) AMS 5734 (Wire) AMS 5737 (Wire) AMS 5804 (Wire) AMS 5805 (Wire) AMS 5810 (Wire) AMS 5853 (Wire) | NACE MR0175 (ISO 15156-3) (Wire) | Annealed | 724 max | 105 max | 275-415 | 40-60 | 25-35 | 160-220 | 90 HRB | ||
| Aged | 965 min | 140 min | 760-1035 | 110-150 | 15-25 | 280-350 | 95 HRB | |||||||||||
| INCOLOY® alloy 800 | Nickel Alloy 800 | N08800 | - | 1.4876 | BS NA15 | ASTM B409 (Strip) ASTM A240 (Strip) | AMS 5871 (Strip) | - | Annealed | 515 min | 75 min | 205-345 | 30-50 | 30-40 | 140-190 | 80 HRB | ||
| INCOLOY® alloy 825 | Nickel Alloy 825 | N08825 | 2.4858 | BS NA16 | ASTM B424 (Strip) | - | NACE MR0175/ISO 15156 (Strip & Wire) NACE MR0103 (Wire) | Annealed | 586 min | 85 min | 241-379 | 35-55 | 30-40 | 150-200 | 80 HRB | |||
| INCOLOY® 925 | Nickel Alloy 925 | N09925 | - | - | - | - | - | NACE MR0175/ISO 15156 (Wire) NACE MR0103 (Wire) | supplied as wire only. | |||||||||
| INCOLOY® 25-6MO Alloy | Nickel Alloy | N08926 | - | 1.4529 | - | - | - | - | Information not available | |||||||||
| INCOLOY® IS A REGISTERED TRADEMARK OF SPECIAL METALS CORPORATION® | ||||||||||||||||||
| HASTELLOY® - STRIP MECHANICAL PROPERTIES | ||||||||||||||||||
| Designations | Specifications | Strip Tempers Available | Tensile Strength | Proof Strength 0.2% | Elong. % Min. (50mm Gauge Length) | Hardness | ||||||||||||
| Commercial Name | Common Name | UNS (nearest fit) | European Designation (nearest fit) | European Standard (nearest fit) | British Standard (nearest fit) | ASTM (nearest fit) | AMS (nearest fit) | Other Standards | MPa | ksi | MPa | ksi | Vickers (VPN) | Rockwell (HRB/HRC) | ||||
| HASTELLOY® B-3 | Nickel Alloy B3 | N10675 | 2.4600 | - | - | ASTM B333 (Strip) | - | - | Annealed | 760 min 860 typ | 110 min 125 typ | 345-517 | 50-75 | 50-60 | 220 | 92-95 | ||
| HASTELLOY® C-4 | Nickel Alloy C4 | N06455 | 2.4610 | - | - | ASTM B575 (Strip) | - | NACE MR0175 (Strip) NACE MR0175 (ISO 15156-3) (Wire) | Annealed | 760 min 860 typ | 110 min 125 typ | 310-483 | 45-70 | 50-60 | 210 | 90-102 | ||
| HASTELLOY® C22® | Nickel Alloy C22 | N06022 | 2.4602 | - | - | ASTM B575 (Strip) | - | NACE MR0175 (Strip) NACE MR0175 (ISO 15156-3) (Wire) | Annealed | 758-1034 | 110-150 | 345-517 | 50-75 | 40-50 | 200-280 | 88-102 | ||
| HASTELLOY® C 276® | Nickel Alloy C 276 | N10276 | 2.4819 | DIN 17750 (Strip) | - | ASTM B575 (Strip) ASTM B906 (Strip) | - | NACE MR0175 (ISO 15156-3) (Wire) | Annealed | 830-1100 | 120-160 | 310 min | 45 min | 40 min | 210-290 | 90-105 | ||
| Spring Temper | 1380-1655 | 200-240 | 520 | 75 | 30 | 340-440 | 105-120 | |||||||||||
| HASTELLOY® alloy C 2000 | Nickel Alloy C2000 | N06200 | 2.4675 | - | - | ASTM B575 (Strip) | - | NACE MR0175 (ISO 15156-3) (Wire) | Annealed | 760 min 860 typ | 110 min 125 typ | 310-483 | 45-70 | 40-50 | 190-270 | 85-100 | ||
| HASTELLOY® X | Nickel Alloy X | N06002 | 2.4665 | - | - | - | AMS 5536 (Strip) AMS 5798 (Wire) | DMD 0491 (Wire) GE B21B111 (Wire) | Annealed | 517 min 690 typ | 105 min | 345-517 | 50-75 | 35-45 | 200-280 | 88-102 | ||
| HASTELLOY® IS A REGISTERED TRADEMARK OF HAYNES INTERNATIONAL INC® | ||||||||||||||||||
| HAYNES® - STRIP MECHANICAL PROPERTIES | ||||||||||||||||||
| Designations | Specifications | Strip Tempers Available | Tensile Strength | Proof Strength 0.2% | Elong. % Min. (50mm Gauge Length) | Hardness | ||||||||||||
| Commercial Name | Common Name | UNS (nearest fit) | European Designation (nearest fit) | European Standard (nearest fit) | British Standard (nearest fit) | ASTM (nearest fit) | AMS (nearest fit) | Other Standards | MPa | ksi | MPa | ksi | Vickers (VPN) | Rockwell (HRB) | ||||
| Haynes® HR-120® Alloy | - | N08120 | 2.4854 | - | - | ASTM B409 (Strip) | - | - | Annealed | 621 min | 90 min | 328 | 47.5 | 46 | Information not available | |||
| HAYNES® 214 | Nickel Alloy 214 | N07214 | 2.4646 | - | - | - | - | - | Annealed | 790-1100 | 115-160 | 438 min | 65 min | 25 min | Information not available | |||
| HAYNES® 224 | Nickel Alloy 224 | - | - | - | - | - | - | - | Annealed | 758-965 | 110-140 | 395 | 57.4 | 50 | Information not available | |||
| HAYNES® 230 | Nickel Alloy 230 | N06230 | 2.4733 | - | - | ASTM B435 (Strip) | AMS 5878 (Strip) | - | Annealed | 793 min | 115 min | 310 min | 45 min | 40 min | Information not available | |||
| HAYNES® 233 | Nickel Alloy 233 | - | - | - | - | - | - | - | Annealed | 965 | 140 | Information not available | ||||||
| Aged | 1172 | 170 | Information not available | |||||||||||||||
| HAYNES® 242 | Nickel Alloy 242 | N10242 | 2.4816 | - | - | ASTM B434 (Strip) | - | - | Annealed | 725 min | 105 min | 310 min | 45 min | 40 min | Information not available | |||
| Annealed + Aged | 1288 typ | 187 typ | Information not available | |||||||||||||||
| HAYNES® 263 | Nickel Alloy 263 | N07263 | 2.465 | - | - | - | AMS 5872 (Strip) | - | Annealed | 882 typ | 128 typ | Information not available | ||||||
| Aged | 1130 typ | 164 typ | Information not available | |||||||||||||||
| HAYNES® 282 | Nickel Alloy 282 | N07208 | - | - | - | - | AMS 5951 (Strip) | - | Annealed | 758-965 | 110-140 | 384 | 56 | 59 | Information not available | |||
| Spring Temper | Up to 1450 | Up to 210 | Information not available | |||||||||||||||
| Aged | 1103-1450 | 160-210 | 699 | 101 | 30 | Information not available | ||||||||||||
| HAYNES® IS A REGISTERED TRADEMARK OF HAYNES INTERNATIONAL INC.® | ||||||||||||||||||
| RENE®41 - STRIP MECHANICAL PROPERTIES | ||||||||||||||||||
| Designations | Specifications | Strip Tempers Available | Tensile Strength | Proof Strength 0.2% | Elong. % Min. (50mm Gauge Length) | Hardness | ||||||||||||
| Commercial Name | Common Name | UNS (nearest fit) | European Designation (nearest fit) | European Standard (nearest fit) | British Standard (nearest fit) | ASTM (nearest fit) | AMS (nearest fit) | Other Standards | MPa | ksi | MPa | ksi | Vickers (VPN) | Rockwell (HRB) | ||||
| RENE®41 | Nickel Alloy 41 | N07041 | 2.4973 | - | - | - | AMS 5545 (Strip) AMS 5800 (Wire) | GE B50T59 (Strip) GE B50TF109 (Strip) | Annealed | 1172 max | 170 max | Information not available | 12 | 253 | 87 HRBW | |||
| Spring Temper | 1150 est | 167 est | Information not available | 6 | 350 | Information not available | ||||||||||||
| After Precipitation Heat Treatment | 1103 min | 160 min | 1034 | 150 | 15 | 321 | Information not available | |||||||||||
| RENE® IS A REGISTERED TRADEMARK OF GENERAL ELECTRIC INC.® | ||||||||||||||||||
| WASPALOY® - MECHANICAL PROPERTIES | ||||||||||||||||||
| Designations | Specifications | Strip Tempers Available | Tensile Strength | Proof Strength 0.2% | Elong. % Min. (50mm Gauge Length) | Hardness | ||||||||||||
| Commercial Name | Common Name | UNS (nearest fit) | European Designation (nearest fit) | European Standard (nearest fit) | British Standard (nearest fit) | ASTM (nearest fit) | AMS (nearest fit) | Other Standards | MPa | ksi | MPa | ksi | Vickers (VPN) | Rockwell (HRB) | ||||
| WASPALOY® | - | N07001 | 2.4654 | - | - | - | AMS 5544 (Strip) AMS 5828 (Wire) | - | Annealed | 1110 max | 160 max | Information not available | 15 | 250 | Information not available | |||
| Annealed + Aged | 1110 min | 170 min | 1070 | 155 | 13 | 350 | Information not available | |||||||||||
| Spring Temper | 1380 min | 200 min | Information not available | 8 | 370 | Information not available | ||||||||||||
| WASPALOY® IS A REGISTERED TRADEMARK OF UNITED TECHNOLOGIES CORPORATION® | ||||||||||||||||||
| MONEL® - STRIP MECHANICAL PROPERTIES | ||||||||||||||||||
| Designations | Specifications | Strip Tempers Available | Tensile Strength | Proof Strength 0.2% | Elong. % Min. (50mm Gauge Length) | Hardness | ||||||||||||
| Commercial Name | Common Name | UNS (nearest fit) | European Designation (nearest fit) | European Standard (nearest fit) | British Standard (nearest fit) | ASTM (nearest fit) | AMS (nearest fit) | Other Standards | MPa | ksi | MPa | ksi | Vickers (VPN) | Rockwell (HRB) | ||||
| MONEL® alloy 400 | Nickel Alloy 400 | N04400 | 2.4360 / 2.4361 | - | BS NA13 (Wire) | ASTM B127 (Strip) ASTM B164 (Wire) | AMS 4544 (Strip) AMS 4730 (Wire) | ASME SB-127 (Strip) (NACE MR0175 (ISO 1516-3) (Wire) | Annealed | 480-585 | 70-85 | 170–240 | 25–35 | 30-40 | 110 | 70–90 | ||
| Spring Temper | 827 | 120 | 480 | 70 | 8–15 | 150 | 90–100 | |||||||||||
| MONEL® alloy K500 | Nickel Alloy K500 | N05500 | 2.4375 | - | BS NA18 (Wire) | ASTM B127 (Strip) ASTM B164 (Wire) | Wire: AMS 4676 | - | Hard | 1240 | 180 | 1035 | 150 | 15 | 300 | 95 HRB | ||
| MONEL® IS A REGISTERED TRADEMARK OF SPECIAL METALS CORPORATION® | ||||||||||||||||||
| NIMONIC® - STRIP MECHANICAL PROPERTIES | ||||||||||||||||||
| Designations | Specifications | Strip Tempers Available | Tensile Strength | Proof Strength 0.2% | Elong. % Min. (50mm Gauge Length) | Hardness | ||||||||||||
| Commercial Name | Common Name | UNS (nearest fit) | European Designation (nearest fit) | European Standard (nearest fit) | British Standard (nearest fit) | ASTM (nearest fit) | AMS (nearest fit) | Other Standards | MPa | ksi | MPa | ksi | Vickers (VPN) | Rockwell (HRB) | ||||
| NIMONIC® alloy 75 | Nickel Alloy 75 | N06075 | 2.4951 | - | BS 2HR 203:2009 (Strip) | - | - | - | Annealed | 655-895 | 95-130 | 275-345 | 170-310 | 30 | 140-180 | 80-95 | ||
| NIMONIC® 90 | Nickel Alloy 90 | N07090 | 2.4632 / 2.4969 | - | BS NA19 BS HR 501 (Wire) BS HR 502 (Wire) BS HR 503 (Wire) | - | AMS 5829 (Wire) | NACE MR0175 / ISO 15156-3 (Wire) NACE MR0103 (Wire) | Supplied as Wire only | |||||||||
| NIMONIC® IS A REGISTERED TRADEMARK OF SPECIAL METALS CORPORATION® | ||||||||||||||||||
| NILO® - STRIP MECHANICAL PROPERTIES | ||||||||||||||||||
| CONTROLLED EXPANSION ALLOYS / GLASS SEALING NICKEL ALLOYS | ||||||||||||||||||
| Designations | Specifications | Strip Tempers Available | Tensile Strength | Proof Strength 0.2% | Elong. % Min. (50mm Gauge Length) | Hardness | ||||||||||||
| Commercial Name | Common Name | UNS (nearest fit) | European Designation (nearest fit) | European Standard (nearest fit) | British Standard (nearest fit) | ASTM (nearest fit) | AMS (nearest fit) | Other Standards | MPa | ksi | MPa | ksi | Vickers (VPN) | Rockwell (HRB) | ||||
| Nilo® K | Alloy 29/18 | K94610 | 1.3981 | Wire: DIN 17745 | - | ASTM F15 (Strip & Wire) | - | - | Annealed | 450-620 | 65-90 | 170-310 | 25-45 | 30 | 150-200 | 85-95 | ||
| Nilo® 36 | NiFe36 Alloy 36 | K93600 | 1.3912 | - | - | Wire: ASTM B388 | - | - | Supplied as wire. | |||||||||
| Nilo® 42 | NiFe42 Alloy 42 | K94100 | 1.3917 | Wire: DIN 17745 | - | ASTM F30 (Wire) | - | - | ||||||||||
| Nilo® 48 | NiFe48 Alloy 48 | K94800 | 1.3922 | Wire: DIN 17745 | - | ASTM F30 (Wire) | - | |||||||||||
| Nilo® 52 | NiFe52 Alloy 52 | N14052 | 2.4478 | - | - | ASTM F30 (Wire) | - | - | ||||||||||
| NILO® IS A REGISTERED TRADEMARK OF SPECIAL METALS CORPORATION® | ||||||||||||||||||
| NICHROME ELECTRICAL RESISTANCE ALLOYS | ||||||||||||||||||
| Designations | Specifications | Tempers Available | Tensile Strength | Proof Strength 0.2% | Elong. % Min. (50mm Gauge Length) | Hardness | ||||||||||||
| Commercial Name | Common Name | UNS (nearest fit) | European Designation (nearest fit) | European Standard (nearest fit) | British Standard (nearest fit) | ASTM (nearest fit) | AMS (nearest fit) | Other Standards | MPa | ksi | MPa | ksi | Vickers (VPN) | Rockwell (HRB) | ||||
| - | Ni Cr 37/18 / Ni Cr 3718 | - | - | - | - | - | - | - | Supplied as wire. | |||||||||
| - | Ni Cr 60/16/ Ni Cr 6015 | N06004 | 2.4867 | 2.4867 | - | - | - | - | ||||||||||
| - | Ni Cr 80/20/ Ni Cr 8020 | N06003 | 2.4869 | 2.4869 | - | - | - | - | ||||||||||
| NI-SPAN-C® | ||||||||||||||||||
| Designations | Specifications | Tempers Available | Tensile Strength | Proof Strength 0.2% | Elong. % Min. (50mm Gauge Length) | Hardness | ||||||||||||
| Commercial Name | Common Name | UNS (nearest fit) | European Designation (nearest fit) | European Standard (nearest fit) | British Standard (nearest fit) | ASTM (nearest fit) | AMS (nearest fit) | Other Standards | MPa | ksi | MPa | ksi | Vickers (VPN) | Rockwell (HRB) | ||||
| NI-SPAN-C® ALLOY 902 | - | N09902 | - | - | - | - | AMS 5221 (Wire) AMS 5225 (Wire) | - | Supplied as wire. | |||||||||
| Nickel Alloy Wire Typical Mechanical Properties | ||||||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Designations | Applicable Specifications | Temper Supplied | Tensile Strength (approx. at 20°C/70°F) | |||||||||||
| Commercial Name | Common Name (nearest fit | UNS (nearest fit) | European Designation (nearest fit) | European Standard (nearest fit) | British Standard (nearest fit) | ASTM (nearest fit) | AMS (nearest fit) | Other Standards | MPa | ksi | ||||
| COMMERCIALLY PURE NICKEL | ||||||||||||||
| - | Nickel Alloy 200 (Commercially Pure Nickel) | N02200 | 2.4066 | DIN 17740 (Strip & Wire), DIN 17750 (Strip) | BS NA11 | ASTM B162 (Strip) | AMS 5553 (Strip) | - | Annealed | 400-480 | 58-70 | |||
| Hard Drawn | 750- 900 | 109-131 | ||||||||||||
| - | Nickel Alloy 201 (Low Carbon Nickel) | N02201 | 2.4068 | DIN 17740 (Strip & Wire), DIN 17750 (Strip) | BS NA12 | ASTM B162 (Strip) | AMS 5553 (Strip) | - | Annealed | 400-480 | 58-70 | |||
| Hard Drawn | 750- 900 | 109-131 | ||||||||||||
| NICKEL-MANGANESE | ||||||||||||||
| Nickel® 212 | Nickel Alloy 212 | N02212 | 2.4110 | - | - | - | - | - | Annealed | 450-550 | 65-80 | |||
| INCONEL® | ||||||||||||||
| Designations | Specifications | Temper | Tensile Strength (approx. at 20°C/70°F) | |||||||||||
| Commercial Name | Common Name | UNS (nearest fit) | European Designation (nearest fit) | European Standard (nearest fit) | British Standard (nearest fit) | ASTM (nearest fit) | AMS (nearest fit) | Other Standards | MPa | ksi | ||||
| Inconel® Alloy 600 | Nickel Alloy 600 | N06600 | 2.4816 | - | BS NA14 | ASTM B168 (Strip) ASTM B166 (Wire) | AMS 5540 (Strip) AMS 5565 (Wire) | - | Annealed | 552-758 | 80-110 | |||
| Hard Drawn | 900-1250 | 130-181 | ||||||||||||
| Spring Temper | 1103-1379 | 160-200 | ||||||||||||
| INCONEL® alloy 601 | Nickel Alloy 601 | N06601 | 2.4851 | DIN 17750 (Strip) | BS NA49 | ASTM B168 (Strip) ASTM B166 (Wire) | AMS 5870 (Strip) | - | Annealed | 620-793 | 90-115 | |||
| Spring Temper | 1240–1448 | 180-210 | ||||||||||||
| INCONEL® alloy 625 | Nickel Alloy 625 | N06625 | 2.4856 | - | BS NA21 | ASTM B443 (Strip) ASTM B446 (Wire) | AMS 5599 (Strip) AMS 5666 (Wire) AMS 5837 (Wire) | NACE MR0175 (ISO 15156-3) (Strip & Wire) NACE MR0103/ISO 17945 (Strip & Wire) | Annealed | 830-1100 | 120-160 | |||
| Hard Drawn | 1300-1600 | 189-232 | ||||||||||||
| Spring Temper | 1380-1655 | 200-240 | ||||||||||||
| INCONEL® alloy 718 | Nickel Alloy 718 | N07718 | 2.4668 | - | BS NA51 | ASTM B670 (Strip) | AMS 5596 (Strip) AMS 5597(Strip) AMS 5832 (Wire) AMS 5962 (Wire) | NACE MR0175 (ISO 15156-3 (Wire) | Annealed | 790-1000 | 115-145 | |||
| Spring Temper | 1310-1515 | 190-220 | ||||||||||||
| Spring Temper + Aged | 1515 min | 220 min | ||||||||||||
| INCONEL® X-750 | Nickel Alloy X750 | N07750 | 2.4669 | - | - | ASTM B637 (Wire) | AMS 5542 (Strip) AMS 5598 (Strip) AMS 5698 (Wire) AMS 5699 (Wire) AMS 5778 (Wire) | NACE MR0175 (ISO 15156-3 (Wire) | Annealed | 896 max | 130 max | |||
| No.1 Temper | 896-1138 | 130-165 | ||||||||||||
| No.1 Temper + Aged | 1138-1517 | 165-220 | ||||||||||||
| Spring Temper | 1103-1517 | 160-220 | ||||||||||||
| Spring Temper + Aged | 1241-1793 | 180-250 | ||||||||||||
| Spring Temper + Solution + Aged | 1000-1310 | 145-190 | ||||||||||||
| INCONEL® IS A REGISTERED TRADEMARK OF Specialty METALS CORPORATION® | ||||||||||||||
| INCOLOY® | ||||||||||||||
| Designations | Specifications | Temper | Tensile Strength (approx. at 20°C/70°F) | |||||||||||
| Commercial Name | Common Name | UNS (nearest fit) | European Designation (nearest fit) | European Standard (nearest fit) | British Standard (nearest fit) | ASTM (nearest fit) | AMS (nearest fit) | Other Standards | MPa | ksi | ||||
| INCOLOY® A-286 | Nickel A-286 GE B50T12 (Strip) | S66286 | - | 1.4980 | - | - | AMS 5525 (Strip) AMS 5858 (Strip) AMS 5726 (Wire) AMS 5731 (Wire) AMS 5732 (Wire) AMS 5734 (Wire) AMS 5737 (Wire) AMS 5804 (Wire) AMS 5805 (Wire) AMS 5810 (Wire) AMS 5853 (Wire) | NACE MR0175 (ISO 15156-3) (Wire) | Annealed | 550-760 | 80-110 | |||
| Annealed + Aged | 1100-1310 | 160-190 | ||||||||||||
| Spring Temper | 1100-1310 | 160-190 | ||||||||||||
| Spring + Aged | 1379-1655 | 200-240 | ||||||||||||
| INCOLOY® alloy 800 | Nickel Alloy 800 | N08800 | NA15 | 1.4876 | - | ASTM B409 (Strip) ASTM A240 (Strip) | AMS 5871 (Strip) | - | Supplied as Strip Only. | |||||
| INCOLOY® alloy 825 | Nickel Alloy 825 | N08825 | NA16 | 2.4858 | - | ASTM B424 (Strip) | - | NACE MR0175/ISO 15156 (Strip & Wire) NACE MR0103 (Wire) | Annealed | 586-724 | 85-105 | |||
| Hard Drawn | 800-1100 | 116-160 | ||||||||||||
| Spring Temper | 1035 min | 150 min | ||||||||||||
| INCOLOY® 925 | Nickel Alloy 925 | N09925 | - | - | - | - | - | NACE MR0175/ISO 15156 (Wire) NACE MR0103 (Wire) | Annealed | 586-724 | 85-105 | |||
| Aged | 965 min | 140 min | ||||||||||||
| INCOLOY® 25-6MO Alloy | Nickel Alloy | N08926 | - | 1.4529 | - | - | - | - | Annealed | 620-827 | 90-120 | |||
| Spring Temper | 1034 min | 190 min | ||||||||||||
| INCOLOY® IS A REGISTERED TRADEMARK OF Specialty METALS CORPORATION® | ||||||||||||||
| HASTELLOY® | ||||||||||||||
| Designations | Specifications | Temper | Tensile Strength (approx. at 20°C/70°F) | |||||||||||
| Commercial Name | Common Name | UNS (nearest fit) | European Designation (nearest fit) | European Standard (nearest fit) | British Standard (nearest fit) | ASTM (nearest fit) | AMS (nearest fit) | Other Standards | MPa | ksi | ||||
| HASTELLOY® B-3 | Nickel Alloy B3 | N10675 | 2.46 | - | - | ASTM B333 (Strip) | - | - | Annealed | 827-1035 | 120-150 | |||
| Spring Temper | 1379 min | 200 min | ||||||||||||
| HASTELLOY® C-4 | Nickel Alloy C4 | N06455 | 2.461 | - | - | ASTM B575 (Strip) | - | NACE MR0175 (Strip) NACE MR0175 (ISO 15156-3) (Wire) | Annealed | 758-1034 | 110-150 | |||
| Spring Temper | 1310-1517 | 190-220 | ||||||||||||
| HASTELLOY® C22® | Nickel Alloy C22 | N06022 | 2.4602 | - | - | ASTM B575 (Strip) | - | NACE MR0175 (Strip) NACE MR0175 (ISO 15156-3) (Wire) | Annealed | 758-1034 | 110-150 | |||
| Formula | Formula | Formula | Formula | Formula | Formula | Formula | Formula | Formula |
|---|---|---|---|---|---|---|---|---|
| Nickel Alloy Material Characteristics and Applications | ||||||||
| Commercial Name (Nearest Fit) | UNS (Nearest) | Other Designations (Nearest Fit) | Applicable Specifications | Classifications | Notable Properties | Alloy Description | Key Markets | Applications |
| Commercially Pure Nickel Alloys | ||||||||
| Nickel Alloy 200 (Commercially Pure Nickel) | N02200 | Common Name: Nickel Alloy 200 (Commercially Pure Nickel) European Designation: 2.4066 Other designations may be available by request | European Specifications: DIN 17740 (Strip & Wire), DIN 17750 (Strip) British Specifications: BS NA11 ASTM Specifications: ASTM B162 (Strip) AMS Specifications: AMS 5553 (Strip) Additional specifications may be available by request | High Performance Alloy Corrosion-Resistant Alloy Resistance Nickel Alloy | Chemical Properties: Excellent resistance to caustic alkalis and reducing chemicals. Physical Properties: High thermal and electrical conductivity. Workability: Easily cold and hot worked. Temperature Range: Suitable for cryogenic and up to 315 °C (599 °F) service. Typical suggested operating range -184°C- 540°C (-300°F - 1000°F). For Temperatures above 315°C (599°F), Nickel alloy 201 (UNS N02201) is recommended. | Alloy 200 is a commercially pure nickel grade (≥99.0% Nickel) with excellent mechanical properties. It has excellent resistance to caustic solutions, particularly caustic alkalis up to 80%, and good resistance to reducing acids; however, it has poor resistance to oxidising acids. This alloy possesses high thermal and electrical conductivity. It can be shaped through all hot and cold working practices. Alloy 200 has excellent ductility, allowing for severe forming, and is readily weldable using GTAW/GMAW methods. The maximum operating temperature for Alloy 200 is 315°C (599°F) for prolonged service, though higher for shorter durations. This grade is ferromagnetic at room temperature. Typical composition: ~99.0% Ni | Aerospace, Defence, Food and Beverage, Automotive, Chemical Processing, Electronics | pressure-safety components e.e bursting discs / explosion panels, battery contacts, food processing, chemical containers and components, aerospace and defence components, chemical processing equipment, caustic handling systems |
| Nickel Alloy 201 (Low Carbon Nickel) | N02201 | Common Name: Nickel Alloy 201 (Low Carbon Nickel) European Designation: 2.4068 Other designations may be available by request | European Specifications: DIN 17740 (Strip & Wire), DIN 17750 (Strip) British Specifications: BS NA12 ASTM Specifications: ASTM B162 (Strip) AMS Specifications: AMS 5553 (Strip) Additional specifications may be available by request | High Performance Alloy Corrosion-Resistant Alloy Resistance Nickel Alloy | Chemical Properties: Improved thermal stability at elevated temperatures. Physical Properties: Retains ductility above 315°C (599°F). Workability: Excellent formability and weldability. Temperature Range: Suggested operating range -184°C- 540°C (-300°F - 1000°F). Maximum service temperature: 650°C (1202°F). | Alloy 201 is the low-carbon (max. 0.15%) version of commercially pure Alloy 200. It was engineered to have a lower carbon content to prevent embrittlement at high temperatures. It maintains good ductility even after high-temperature exposure. It is typically specified for temperatures above 315°C (599°F), with a maximum operating temperature of 650°C (1202°F). It does not suffer embrittlement due to its low carbon content. It exhibits excellent weldability and is particularly well-suited for spinning, deep drawing operations, and cold forming, owing to its lower work-hardening rate. Typical composition: ~99.0% Ni | Automotive, Chemical Processing, Aerospace, Electronics | electronic components, chemical industry components, aerospace components, pressure-safety components e.e bursting discs / explosion panels, heat exchangers, high-temperature electronics, spark plug electrodes |
| Nickel-Manganese Alloy | ||||||||
| Commercial Name (Nearest Fit) | UNS (Nearest) | Other Designations (Nearest Fit) | Applicable Specifications | Classifications | Notable Properties | Alloy Description | Key Markets | Applications |
| Nickel® 212 | N02212 | Common Name: Nickel Alloy 212 European Designation: 2.4110 Other designations may be available by request | Please contact us with your requirements. | Corrosion-Resistant Alloy Resistance Nickel Alloy | Chemical Properties: Retains workability and corrosion resistance similar to Alloy 200. Physical Properties: Enhanced tensile strength over Alloy 200. Good electrical resistivity and thermal conductivity. Work hardens more rapidly than pure nickel grades. Temperature Range: Up to 315°C (599°F). | Nickel Alloy 212 is a manganese-strengthened commercially pure nickel offering higher tensile strength than Nickel 200 while retaining good corrosion resistance and higher electrical resistivity (≈ 10.9 µΩ·cm at 20 °C / (4.29 μΩ·in at 70°F). This grade has good formability properties, but it work-hardens more rapidly than Alloy 200. It is a good thermal conductor. It is readily weldable. At temperatures above 315°C (599°F), tensile strength and elongation are significantly reduced. Higher electrical resistivity than 200/201 Typical composition: ~97.0% Mn 1.5-2.50% | Electronics, Automotive | electrical wires, lead wires, lamp components and electrode support wire, electronic valves, cold tail connectors for heating cables and mats, heating elements for specialised applications |
| The information provided is for reference only. Typical properties and application guidance should not be used as a substitute for the full requirements specified in recognised standards (ASTM, DIN, EN). Producer datasheets may apply narrower limits or additional restrictions depending on form, processing, and intended use. Always confirm material suitability with technical support before final selection. | ||||||||
| Inconel® Alloys | ||||||||
| Commercial Name (Nearest Fit) | UNS (Nearest) | Other Designations (Nearest Fit) | Applicable Specifications | Classifications | Notable Properties | Alloy Description | Key Markets | Applications |
| INCONEL® Alloy 600 | N06600 | Common Name: Nickel Alloy 600 European Designation: 2.4816 Other designations may be available by request | British Specifications: BS NA14 ASTM Specifications: ASTM B168 (Strip), ASTM B166 (Wire) AMS Specifications: AMS 5540 (Strip), AMS 5565 (Wire) Additional specifications may be available by request | High Performance Alloy Heat Resistant Alloy / High Temperature Alloy Corrosion-Resistant Alloy Resistance Nickel Alloy | Chemical Properties: Excellent resistance to oxidation and corrosion. Resists chloride-ion stress corrosion cracking. Physical Properties: Maintains strength at elevated temperatures. Non-magnetic and weldable. Workability: Weldable. Temperature Range: Cryogenic levels to elevated temperatures up to approximately 1093°C (2000°F), suggested operating temperature -184°C - 370°C (300°F - 700°F). | This nickel alloy resists oxidation up to 1200°C (2192°F) and has good corrosion resistance, with excellent resistance to caustic corrosion at high temperatures. Its high nickel content (~72%) makes it highly resistant to chloride-ion stress corrosion cracking, while its chromium content (14-17%) enhances its oxidation resistance. The alloy is not precipitation-hardenable but can be strengthened through cold working. It maintains good mechanical properties across a wide temperature range, from cryogenic levels to elevated temperatures up to approximately 1093°C (2000°F). Additionally, Alloy 600 is readily weldable by conventional processes. Typical composition: ~72% Ni, 14-17% Cr, 6-10% Fe | Chemical, Nuclear, Aerospace, Heat Treating, Automotive, Oil & Gas, Power Generation (especially nuclear) Electronics, Environment & Energy Engineering, Paper & Pulp | flexible tubing, furnace equipment, insulation blankets, heat treating components, chemical processing equipment, food processing, seals, nuclear reactor components, steam generator tubes, catalyst grid supports in chemical plants, heater elements for industrial furnaces, vacuum applications in electronics |
| INCONEL® alloy 601 | N06601 | Common Name: Nickel Alloy 601 European Designation: 2.4851 Other designations may be available by request | European Specifications: DIN 17750 (Strip) British Specifications: BS NA49 ASTM Specifications: ASTM B168 (Strip), ASTM B166 (Wire) AMS Specifications: AMS 5870 (Strip) Additional specifications may be available by request | Heat Resistant Alloy / High Temperature Alloy Corrosion-Resistant Alloy High Strength Alloy Resistance Nickel Alloy | Chemical Properties: Excellent oxidation resistance to 1200°C (2200°F). Resists carburisation and nitridation. Physical Properties: Superior thermal stability under cycling conditions. High mechanical strength. Temperature Range: Up to 1200°C (2200°F). Suggested operating temperature (in the annealed condition): -184°C - 1000°C (300°F - 1830°F) for strip / -184°C - 340°C (300°F - 645°F) for wire. | With a lower nickel content than Alloy 600, Alloy 601 contains 21-25% Cr and 1.0-1.7% Al, enhancing its oxidation resistance and providing exceptional resistance to oxidation at high temperatures. It also possesses good resistance to aqueous corrosion, carburisation and sulfidation. However, alloy 601 is not recommended for use in strongly reducing, sulfur-bearing environments. It possesses good mechanical strength and can be easily formed, machined, and welded. It exhibits high tensile strength at room temperature and retains a significant level of strength at elevated temperatures. Alloy 601 is not embrittled by prolonged exposure to elevated temperatures, retaining good impact strength and good creep-rupture strength. The optimal condition for alloy 601 depends on the specific application and the operating temperatures it will encounter. In scenarios where rupture resistance is critical, the solution-treated condition is the ideal choice, particularly at elevated temperatures of around 1000°F (540°C) or more. This condition not only enhances the alloy’s strength and durability but also ensures it performs reliably under demanding industrial environments. Typical composition: 58-63% Ni, 21-25% Cr, 1-1.7% Al | Chemical, Thermal Engineering, Aerospace, Power Generation, Petrochemical, Automotive Waste Treatment | petrochemical processing equipment, including radiant tubes in petrochemical plants, furnace equipment, gas turbine components, gaskets, condenser tubes, insulating cans, combustion chambers, heat shields, thermal reactors and mufflers |
| INCONEL® alloy 625 | N06625 | Common Name: Nickel Alloy 625 European Designation: 2.4856 Other designations may be available by request | British Specifications: BS NA21 ASTM Specifications: ASTM B443 (Strip), ASTM B446 (Wire) AMS Specifications: AMS 5599 (Strip), AMS 5666 (Wire), AMS 5837 (Wire) Other Specifications: NACE MR0175 (ISO 15156-3) (Strip & Wire), NACE MR0103/ISO 17945 (Strip & Wire) Additional specifications may be available by request | High Performance Alloy Superalloy Heat Resistant Alloy / High Temperature Alloy Corrosion-Resistant Alloy High Strength Alloy Resistance Nickel Alloy | Chemical Properties: Excellent resistance to pitting, crevice, and chloride-ion corrosion. Maintains mechanical integrity in seawater. Physical Properties: High strength without heat treatment. Good thermal fatigue resistance. Workability: Good weldability. Temperature Range: From cryogenic to 982°C (1800°F). Suggested operating range (in the annealed condition) -184°C - 980°C (300°F - 1800°F) | Nickel Alloy 625 is a high-temperature nickel-chromium-molybdenum-niobium alloy renowned for its exceptional strength and outstanding resistance to a wide range of corrosive environments. This high-strength alloy is tougher than alloy 600 due to its increased molybdenum content (~9%) and niobium plus tantalum (3.15-4.15%), which significantly improves strength through solid solution strengthening while eliminating the need for precipitation-hardening treatments. It exhibits good creep and rupture strength. Alloy 625 offers excellent resistance to oxidation and corrosion across a broad range of environments, including severe aqueous conditions, making it suitable for applications in the marine and chemical processing industries. Its composition provides outstanding resistance to localised corrosion forms such as pitting and crevice corrosion, particularly in chloride-containing environments. It is resistant to caustics and seawater and immune to chloride ion stress corrosion cracking, a common failure in stainless steels under similar conditions. This alloy can be readily welded by conventional processes, maintaining its corrosion resistance and mechanical properties in welded structures. Service temperatures range from cryogenic to 982°C (1800°F) for continuous service; suitable for higher temperatures in shorter duration applications Typical composition: ~58% Ni, 20-23% Cr, 8-10% Mo, 3.15-4.15% Nb+Ta | Automotive, Chemical, Marine, Aerospace, Power Generation, Nuclear, Waste Treatment | specialised aerospace components, honeycomb, seals, bellows, diaphragms, springs, heat exchangers, aircraft exhausts, marine components, compressor vanes, pollution control equipment, propulsion components, reactors, submarine equipment, waste treatment and pollution control equipment |
| INCONEL® alloy 718 | N07718 | Common Name: Nickel Alloy 718 European Designation: 2.4668 Other designations may be available by request | British Specifications: BS NA51 ASTM Specifications: ASTM B670 (Strip) AMS Specifications: AMS 5596 (Strip) AMS 5597(Strip), AMS 5832 (Wire), AMS 5962 (Wire), Other Specifications: NACE MR0175 (ISO 15156-3 (Wire) Additional specifications may be available by request | High Performance Alloy Superalloy Corrosion-Resistant Alloy High Strength Alloy | Chemical Properties: High strength and corrosion resistance. Resistant to sulphide and chloride stress corrosion. Physical Properties: Slow age-hardening for improved weldability. Excellent fatigue and creep resistance. Temperature Range: Recommended maximum continuous service temperature is approximately 704°C (1300°F) | Alloy 718 is a high-strength, precipitation-hardened, corrosion-resistant nickel-chromium alloy known for its exceptional mechanical properties at temperatures ranging from cryogenic levels up to 704°C (1300°F). It has a slow age-hardening response, enabling annealing and welding without spontaneous hardening during heating and cooling processes. It exhibits excellent resistance to oxidation and corrosion in various environments, including resistance to chloride-ion stress-corrosion cracking and sulfur-induced stress corrosion cracking. Titanium and niobium additions overcome strain age cracking problems in welding, enhancing the alloy’s weldability compared to other nickel-based superalloys. The recommended maximum continuous service temperature is approximately 704°C (1300°F), though higher temperatures are possible for intermittent service. Its excellent mechanical properties and corrosion resistance make it a popular choice in the aerospace industry, marine, and chemical processing industries, particularly for applications exposed to high stresses and corrosive environments at elevated temperatures. Typical composition: ~52% Ni, 17-21% Cr, 4.75-5.5% Nb+Ta, 2.8-3.3% Mo | Oil & Gas, Power Generation, Nuclear, Aerospace, Space Exploration, Defence, Automotive. Offshore & Marine Engineering, Medical | high-temperature springs, bellows, seals, valves, fasteners, mandrels, gaskets, clamps, surgical instruments and implants, rocket motors and thrust reversers, nuclear fuel element spacers, downhole tools in oil and gas wells |
| INCONEL® X-750 | N07750 | Common Name: Nickel Alloy X750 European Designation: 2.4669 Other designations may be available by request | ASTM Specifications: ASTM B637 (Wire) AMS Specifications: AMS 5542 (Strip), AMS 5598 (Strip), AMS 5698 (Wire), AMS 5699 (Wire), AMS 5778 (Wire) Other Specifications: NACE MR0175 (ISO 15156-3 (Wire) Additional specifications may be available by request | High Performance Alloy Superalloy Heat Resistant Alloy / High Temperature Alloy Corrosion-Resistant Alloy High Strength Alloy | Chemical Properties: Excellent oxidation resistance. Physical Properties: High-temperature strength to 982°C (1800°F). Excellent relaxation resistance. Maintains ductility after prolonged exposure. Superior performance in high-stress environments. Temperature Range: From sub-zero temperatures up to a maximum of 982°C (1800°F). | Alloy X-750 is a precipitation-hardenable nickel-chromium alloy known for its excellent strength and corrosion resistance. The addition of aluminium and titanium enhances its mechanical properties, and this alloy maintains high strength at temperatures up to 704°C (1300°F), retaining functional strength up to 982°C (1800°F). This alloy also retains its ductility after prolonged exposure to elevated temperatures and possesses excellent relaxation resistance, making it ideal for high-temperature spring applications. This alloy is a popular choice for applications that require both high-temperature strength and corrosion resistance, particularly in industries such as aerospace, energy, and nuclear. Its corrosion resistance is generally considered excellent; however, due to a lower chromium content, alloy X-750 has lower oxidation resistance compared to other nickel-chromium alloys, such as alloy 718, which benefits from a higher chromium content and the addition of molybdenum. Typical composition: ~70% Ni, 14-17% Cr, 2.25-2.75% Ti, 0.4-1.0% Al | Oil & Gas, Nuclear, Power Generation, Aerospace, Space Exploration, Automotive, Medical | high-temperature springs, diaphragms, gas turbines, jet engines, medical equipment, nuclear reactor core components, high-temperature fasteners, rocket engine components |
| Inconel® is a registered trademark of Special Metals Corporation®. The information provided is for reference only. Typical properties and application guidance should not be used as a substitute for the full requirements specified in recognised standards (ASTM, DIN, EN). Producer datasheets may apply narrower limits or additional restrictions depending on form, processing, and intended use. Always confirm material suitability with technical support before final selection. | ||||||||
| Incoloy® Alloys | ||||||||
| Commercial Name (Nearest Fit) | UNS (Nearest) | Other Designations (Nearest Fit) | Applicable Specifications | Classifications | Notable Properties | Alloy Description | Key Markets | Applications |
| INCOLOY® A-286 | S66286 | Common Name: Nickel A-286 European Designation: 1.4980 Other designations may be available by request | AMS Specifications: AMS 5525 (Strip) AMS 5858 (Strip), AMS 5726 (Wire), AMS 5731 (Wire), AMS 5732 (Wire), AMS 5734 (Wire), AMS 5737 (Wire), AMS 5804 (Wire), AMS 5805 (Wire), AMS 5810 (Wire), AMS 5853 (Wire) Other Specifications: NACE MR0175 (ISO 15156-3) (Wire) Additional specifications may be available by request | High Performance Alloy Superalloy High Strength Alloy | Chemical Properties: Maintains corrosion resistance to 700°C (1300°F). Physical Properties: Maintains strength to 700°C (1300°F). Age-hardenable for high tensile performance. Good creep resistance. Workability: Excellent fabricability and weldability. Temperature Range: Up to 700°C (1300°F) | INCOLOY® A‑286 is a high-strength, iron-nickel-chromium alloy designed for service at elevated temperatures. Classified as a precipitation-hardenable superalloy, it combines age-hardening capability with excellent corrosion and oxidation resistance, particularly in high-temperature environments up to 700°C (1300°F). Its strength is derived from additions of molybdenum, titanium, and vanadium, which enable exceptional creep and stress rupture performance during long-term exposure. A‑286 is widely specified in critical aerospace, power generation, and cryogenic service where consistent mechanical performance and resistance to thermal fatigue are essential. The alloy exhibits good fabricability and can be readily cold- or hot-formed. It maintains non-magnetic properties after heat treatment and offers good weldability using standard methods, with post-weld ageing recommended to restore mechanical properties. Typical composition: ~25% Ni, 14.5% Cr, 1.25% Mo, 2.1% Ti, 0.3% V, balance Fe | Automotive, Aerospace, Power Generation, Chemical Processing, Oil & Gas, Cryogenic | turbine engine components, afterburner parts, non-magnetic cryogenic equipment, oil & gas manifolds, fasteners springs |
| INCOLOY® alloy 800 | N08800 | Common Name: Nickel Alloy 800 European Designation: 1.4876 Other designations may be available by request | British Specifications: BS NA15 ASTM Specifications: ASTM B409 (Strip), ASTM A240 (Strip) AMS Specifications: AMS 5871 (Strip) Additional specifications may be available by request | Heat Resistant Alloy / High Temperature Alloy Corrosion-Resistant Alloy | Chemical Properties: Excellent stress corrosion resistance. Resists oxidation and scaling at high temperatures. Physical Properties: Good mechanical strength at elevated temperatures. Stable structure under thermal cycling. Temperature Range: Stable during prolonged exposure to temperatures up to 816 °C (1500 °F). | INCOLOY® alloy 800 is an iron-nickel-chromium alloy engineered for high-temperature structural stability and corrosion resistance. With a typical nickel content of 30–35% and chromium content around 19–23%, it resists oxidation, carburisation, and chloride stress corrosion cracking, making it suitable for use in heat exchangers, furnace components, and reformer tubing. It maintains excellent creep strength and metallurgical stability during prolonged exposure to temperatures up to 816°C (1500°F). Alloy 800 is typically supplied in the solution-annealed condition. Variants include 800H and 800HT, which feature tighter carbon and aluminium-titanium controls for enhanced high-temperature strength and improved resistance to stress rupture and creep. These alloys are extensively used in chemical processing, thermal engineering, and nuclear applications that require long-term strength and corrosion resistance. Typical composition: ~32% Ni, 21% Cr, balance Fe, with minor additions of Al and Ti | Chemical, Thermal Engineering, Food and Beverage, Nuclear, Petrochemical, Chemical Processing | electrical heating elements, heat exchangers, furnace equipment, petrochemical process tubing, domestic appliances |
| INCOLOY® alloy 825 | N08825 | Common Name: Nickel Alloy 825 European Designation: 2.4858 Other designations may be available by request | British Specifications: BS NA16 ASTM Specifications: ASTM B424 (Strip) Other Specifications: NACE MR0175/ISO 15156 (Strip & Wire) , NACE MR0103 (Wire) Additional specifications may be available by request | High Performance Alloy Corrosion-Resistant Alloy Resistance Nickel Alloy | Chemical Properties: Excellent resistance to sulphuric and phosphoric acids. Resists chloride-induced stress corrosion. Stable in oxidising and reducing media. Suitable for acid processing environments. Temperature Range: From cryogenic temperature up to 540 °C (1000 °F), at temperatures above this range, microstructural changes can occur. | INCOLOY® alloy 825 is a corrosion-resistant nickel-iron-chromium alloy further alloyed with molybdenum, copper, and titanium. Its composition offers superior resistance to both oxidising and reducing environments compared to alloy 800. With approximately 2.5–3.5% molybdenum and 0.5–1.5% copper, the alloy provides exceptional resistance to sulphuric and phosphoric acids, stress corrosion cracking, pitting, and crevice corrosion. Widely used in chemical processing, pollution control, oil and gas production, and marine environments, INCOLOY® 825 maintains excellent mechanical properties in both ambient and elevated temperature service. It is well-suited to precision strip and wire applications in heat exchanger tubing, seals, springs, and chemical processing equipment. The alloy is readily fabricated and exhibits good weldability by all conventional processes. Typical composition: ~42% Ni, 21.5% Cr, 2.5% Mo, 3% Cu, 0.9% Ti, balance Fe | Chemical, Petrochemical, Oil & Gas, Nuclear, Chemical Processing, Marine, Pollution Control | tubing, pipework in petrochemical, industry, seals, gaskets, heat exchangers |
| INCOLOY® 925 | N09925 | Common Name: Nickel Alloy 925 Other designations may be available by request | Other Specifications: NACE MR0175/ISO 15156 (Wire), NACE MR0103 (Wire) Additional specifications may be available by request | Corrosion-Resistant Alloy High Strength Alloy Resistance Nickel Alloy | Chemical Properties: Superior corrosion resistance in sour and marine environments. Suitable for offshore and downhole service. Physical Properties: High strength with age-hardening. Maintains ductility under stress. | INCOLOY® 925 is a high-strength, corrosion-resistant nickel-iron-chromium alloy specifically designed for demanding environments such as sour gas and marine conditions, making it valuable in offshore, chemical processing, and sour service applications. This alloy combines excellent mechanical properties with superior corrosion resistance in both oxidising and reducing conditions. Significant additions of molybdenum, copper, titanium, and aluminium enhance its strength and corrosion performance. Age-hardenable through heat treatment, INCOLOY® 925 exhibits mechanical properties comparable to INCONEL® 718, while providing improved corrosion resistance in chloride-bearing and hydrogen sulphide environments typical of oil and gas operations. It resists pitting, crevice corrosion, and chloride stress corrosion cracking. Typical composition: ~42% Ni, 21% Cr, 2.6% Mo, 1.5% Cu, 1.9% Ti, 0.1% Al, balance Fe | Oil & Gas, Chemical Processing, Marine | well components, tubing, valves, hangers, tool joints, marine/pump shafts, high-strength pipe |
| INCOLOY® 25-6MO Alloy | N08926 | Common Name: Nickel Alloy European Designation: 1.4529 Other designations may be available by request | Please contact us with your requirements. | Corrosion-Resistant Alloy Resistance Nickel Alloy | Chemical Properties: Excellent resistance to pitting and crevice corrosion. High performance in acidic and chloride-rich environments. Stable under fluctuating thermal and chemical conditions. Workability: Good weldability and formability. | Although often categorised as a super-austenitic stainless steel, INCOLOY® 25-6MO (also known by DIN 1.4529 or UNS N08926) is frequently grouped with high-performance nickel alloys due to its elevated nickel content (~24–26%) and robust corrosion resistance. It is engineered for aggressive environments involving strong chlorides, seawater, and mineral acids, particularly sulphuric acid. The alloy's composition includes high molybdenum (~6.5–7.5%) and nitrogen, enhancing its resistance to pitting and crevice corrosion. The copper content (~0.5–1.5%) further improves resistance in acidic conditions. INCOLOY® 25-6MO outperforms standard austenitic grades such as 316L (1.4404) and 904L (1.4539) in both general and localised corrosion. Despite its advanced performance, it remains more economical than fully nickel-based alloys like Alloy C-276. Well-suited for precision strip and wire, it is employed in desalination plants, heat exchangers, offshore systems, and springs. The alloy exhibits good formability and weldability and maintains strength and ductility after cold work or welding. Typical composition: ~25% Ni, 20% Cr, 6.5% Mo, 0.9% Cu, 0.2% N, balance Fe | Chemical Processing, Oil & Gas, Nuclear Power Generation, Food Processing, Springs | marine/offshore platform equipment, desalination equipment, heat exchangers, pipes, paper processing equipment, caustic chloride systems, springs |
| Incoloy® is a registered trademark of Special Metals Corporation®. The information provided is for reference only. Typical properties and application guidance should not be used as a substitute for the full requirements specified in recognised standards (ASTM, DIN, EN). Producer datasheets may apply narrower limits or additional restrictions depending on form, processing, and intended use. Always confirm material suitability with technical support before final selection. | ||||||||
| Hastelloy® | ||||||||
| Commercial Name (Nearest Fit) | UNS (Nearest) | Other Designations (Nearest Fit) | Applicable Specifications | Classifications | Notable Properties | Alloy Description | Key Markets | Applications |
| HASTELLOY® B-3 | N10675 | Common Name: Nickel Alloy B3 European Designation: 2.4600 Other designations may be available by request | ASTM Specifications: ASTM B333 (Strip) Additional specifications may be available by request | Corrosion-Resistant Alloy | Chemical Properties: Outstanding resistance to hydrochloric acid. Superior resistance to stress corrosion cracking and pitting. Physical Properties: Improved thermal stability vs earlier B-series alloys. Workability: Excellent formability and weldability. | HASTELLOY® B-3 is a nickel-molybdenum alloy specifically engineered to provide excellent resistance to hydrochloric acid across all concentrations and temperatures. It retains the key corrosion-resistant features of earlier HASTELLOY® B-series alloys while offering significantly improved thermal stability and fabrication characteristics. This material resists pitting, stress corrosion cracking, and attack by other aggressive media such as sulphuric, acetic, formic, and phosphoric acids, as well as non-oxidising salt solutions. Typical Composition: ~65% Ni, 28.5-30.5% Mo, ≤1.5% Fe, ≤3% Co, ≤3% Cr | Chemical Processing | chemical processing, vacuum furnaces, mechanical components, reaction vessels, welding wire, fittings, rings, springs, bellows |
| HASTELLOY® C-4 | N06455 | Common Name: Nickel Alloy C4 European Designation: 2.4610 Other designations may be available by request | ASTM Specifications: ASTM B575 (Strip) Other Specifications: NACE MR0175 (Strip), NACE MR0175 (ISO 15156-3) (Wire) Additional specifications may be available by request | High Performance Alloy Corrosion-Resistant Alloy | Chemical Properties: Excellent resistance to oxidising media. Superior stress corrosion cracking resistance. High resistance to chemical attack at elevated temperatures. Physical Properties: Outstanding thermal stability and ductility. | HASTELLOY® C-4 is a nickel-chromium-molybdenum alloy with exceptional resistance to oxidising atmospheres at high temperatures and superior stress corrosion cracking resistance. It performs reliably in chemical processing environments, particularly those involving strong oxidisers, hot contaminated mineral acids, and solvents. C-4 offers improved thermal stability, stress rupture properties, and fabrication performance compared to other high-Mo alloys. Typical Composition: ~65% Ni, 14-18% Mo, 16% Cr, ≤2% Fe | Chemical Processing, Nuclear Processing, Marine | springs and components for chemical processing, nuclear fuel processing, marine applications, heat exchangers, reactor systems |
| HASTELLOY® C22® | N06022 | Common Name: Nickel Alloy C22 European Designation: 2.4602 Other designations may be available by request | ASTM Specifications: ASTM B575 (Strip) Other Specifications: NACE MR0175 (Strip), NACE MR0175 (ISO 15156-3) (Wire) Additional specifications may be available by request | High Performance Alloy Corrosion-Resistant Alloy | Chemical Properties: Exceptional resistance to oxidising and reducing agents. Superior pitting and crevice corrosion resistance. Outstanding versatility across chemical industries. Physical Properties: Maintains strength and corrosion resistance after welding. | HASTELLOY® C-22® is a versatile nickel-chromium-molybdenum-tungsten alloy designed for superior corrosion resistance in a wide range of aggressive media. It offers outstanding protection against pitting, crevice corrosion, and stress corrosion cracking. Its high chromium content provides excellent oxidising acid resistance, while molybdenum and tungsten enhance performance in reducing environments. Typical Composition: ~56% Ni, 20-22.5% Cr, 12.5-14.5% Mo, 2.5-3.5% W, ≤3% Fe | Chemical, Nuclear, Environment & Energy Engineering, Oil & Gas, Waste Management | expansion bellows, industrial equipment, chemical processing, waste treatment equipment, process tanks, chemical transfer systems |
| HASTELLOY® C-276® | N10276 | Common Name: Nickel Alloy C 276 European Designation: 2.4819 Other designations may be available by request | European Specifications: DIN 17750 (Strip) ASTM Specifications: ASTM B575 (Strip), ASTM B906 (Strip) Other Specifications: NACE MR0175 (ISO 15156-3) (Wire) Additional specifications may be available by request | High Performance Alloy Corrosion-Resistant Alloy | Chemical Properties: Broad-spectrum corrosion resistance. Resistant to pitting, crevice corrosion, and oxidisers. Physical Properties: Maintains mechanical properties across temperature extremes. Workability: Excellent weldability and formability. | HASTELLOY® C-276® is one of the most corrosion-resistant alloys available, offering protection against both oxidising and reducing chemicals. It is especially effective in handling strong oxidisers, chlorides, wet chlorine gas, hypochlorite, and chlorine dioxide. Its high chromium and molybdenum contents provide outstanding pitting and crevice corrosion resistance in chloride-bearing environments. Typical Composition: ~57% Ni, 15.5% Cr, 15-17% Mo, 4-7% Fe, 3.5-4.5% W | Chemical, Marine, Aerospace, Oil & Gas, Environment & Energy Engineering, Pharmaceutical | diaphragms, marine engineering and equipment, chemical vessels, pulp and paper production, ducts, heat exchangers, processing lines |
| HASTELLOY® alloy C 2000 | N06200 | Common Name: Nickel Alloy C2000 European Designation: 2.4675 Other designations may be available by request | ASTM Specifications: ASTM B575 (Strip) Other Specifications: NACE MR0175 (ISO 15156-3) (Wire) Additional specifications may be available by request | High Performance Alloy Corrosion-Resistant Alloy | Chemical Properties: High resistance to mixed acid environments. Enhanced protection from stress corrosion cracking. Performs well in chloride-bearing media. Physical Properties: Good mechanical integrity. Workability: Good weldability. | HASTELLOY® C-2000® combines high levels of molybdenum and copper with nickel-chromium to offer outstanding corrosion resistance in both oxidising and reducing environments. This alloy resists sulphuric, hydrochloric, hydrofluoric, nitric, and phosphoric acids, and is highly versatile in multi-chemical process environments. Furthermore, it is easy to form and weld and provides excellent resistance to stress corrosion cracking. Typical Composition: ~59% Ni, 23% Cr, 16% Mo, 1.6% Cu, ≤2% Fe | Chemical, Waste Treatment | heat exchangers, reactors, acid storage vessels, scrubber systems |
| HASTELLOY® X | N06002 | Common Name: Nickel Alloy X European Designation: 2.4665 Other designations may be available by request | AMS Specifications: AMS 5536 (Strip), AMS 5798 (Wire) Other Specifications: DMD 0491 (Wire), GE B21B111 (Wire) Additional specifications may be available by request | High Performance Alloy Heat Resistant Alloy / High Temperature Alloy Corrosion-Resistant Alloy | Chemical Properties: Outstanding resistance to hydrochloric acid. Superior resistance to stress corrosion cracking and pitting. Physical Properties: Improved thermal stability vs earlier B-series alloys. Workability: Excellent formability and weldability. | HASTELLOY® X is a high-performance nickel-chromium-iron-molybdenum alloy offering exceptional strength and oxidation resistance at high temperatures up to 1170°C (2138°F). It remains stable under cyclic thermal stress and is widely used in demanding aerospace applications, including combustion zones and engine components. HASTELLOY® X is ideal for heat-intensive and corrosive service environments. Typical Composition: ~47% Ni, 22% Cr, 18.5% Fe, 9% Mo, 1.5% Co | Aerospace, Automotive, Power Generation, Chemical Processing | turbine engine components, combustion liners, high-temperature springs, seals, and honeycomb structures |
| HASTELLOY® is a registered trademark of HAYNES INTERNATIONAL INC®. The information provided is for reference only. Typical properties and application guidance should not be used as a substitute for the full requirements specified in recognised standards (ASTM, DIN, EN). Producer datasheets may apply narrower limits or additional restrictions depending on form, processing, and intended use. Always confirm material suitability with technical support before final selection. | ||||||||
| Haynes® | ||||||||
| Commercial Name (Nearest Fit) | UNS (Nearest) | Other Designations (Nearest Fit) | Applicable Specifications | Classifications | Notable Properties | Alloy Description | Key Markets | Applications |
| Haynes® HR-120® Alloy | N08120 | European Designation: 2.4854 Other designations may be available by request | ASTM Specifications: ASTM B409 (Strip) Additional specifications may be available by request | Heat Resistant Alloy / High Temperature Alloy | Chemical Properties: High temperature strength and oxidation resistance. Excellent carburisation and sulfidation resistance. Physical Properties: Thermal stability to 1204°C (2200°F). Workability: Good formability and weldability. | HAYNES® HR-120 is a solid-solution strengthened, iron-nickel-chromium alloy developed for high strength and oxidation resistance in extreme heat environments. This heat-resistant alloy demonstrates excellent thermal stability and high creep strength, especially at elevated service temperatures reaching up to 1204°C (2200°F). Unlike traditional Fe-Ni-Cr alloys, HR-120® offers superior carburisation and sulfidation resistance, making it an excellent choice for demanding applications involving aggressive industrial atmospheres. With outstanding resistance to hot corrosion in molten salt and mixed chemical environments, this alloy is especially suited for industrial heat treating, waste processing, and high-temperature structural applications. It can be hot or cold formed and exhibits good weldability, ensuring reliable integration into complex assemblies. Typical composition: ~37% Ni, 25% Cr, 2% Mn, 1.2% Si, 1.4% Mo, 0.6% Nb, balance Fe | Industrial Heat Treating, Chemical Processing, Waste Management, Food Processing | heat treatment baskets, wire mesh belts, basket liners, mufflers, recuperators, waste incinerators, turbine engine parts, heat treat furnaces and fixtures, radiant tubes |
| HAYNES® 214 | N07214 | Common Name: Nickel Alloy 214 European Designation: 2.4646 Other designations may be available by request | Please contact us with your requirements. | High Performance Alloy Heat Resistant Alloy / High Temperature Alloy | Chemical Properties: Outstanding oxidation resistance above 955°C (1750°F). Forms protective alumina scale. Resistant to carburisation and chlorine-bearing gases. Workability: Suitable for thin-section fabrication. Temperature Range: Intended for service at temperatures above 955°C (1750°F). | HAYNES® 214 is a nickel-aluminium-iron-chromium alloy engineered for exceptional oxidation resistance in high-temperature, low-stress environments. Intended principally for continuous service at temperatures of 955°C (1750°F) and above, it exhibits superior oxidation resistance compared to conventional alloys at these temperatures. Its unique ability to form a protective aluminium oxide (Al²O³) scale provides superior resistance to carburisation, nitriding, and chlorine-bearing oxidising gases above 955°C (1750°F). It is ideal for structural applications such as burner components, flame hoods, and catalytic converter substrates. The alloy can be processed into complex components and is widely used in industrial and aerospace environments where extreme oxidation and corrosive gases are present. Typical composition: ~75% Ni, 16% Cr, 4.5% Al, 3% Fe | Aerospace, Automotive, Industrial Heating, Medical, Land-Based Gas Turbines | honeycomb seals, catalytic converters, flame hoods, rotary calciners burners, mesh belts, catalytic converters, chlorine-contaminated incinerator systems |
| HAYNES® 224 | - | Common Name: Nickel Alloy 224 Other designations may be available by request | Please contact us with your requirements. | Heat Resistant Alloy / High Temperature Alloy | Chemical Properties: High oxidation resistance up to 1093°C (2000°F). Physical Properties: Stable under thermal cycling. Strengthened by solid solution additions. Workability: Good weldability and formability. Temperature Range: Up to 1093°C (2000°F). | HAYNES® 224 is a solid-solution strengthened, nickel-chromium-aluminium alloy developed for enhanced oxidation resistance and thermal stability up to 1093°C (2000°F). The inclusion of tungsten and molybdenum contributes to improved high-temperature strength and stability during thermal cycling. This alloy offers excellent forming and welding characteristics, making it suitable for critical components in heat-treating furnaces and chemical plants operating under cyclical thermal loads. Typical composition: ~64% Ni, 21% Cr, 3% Mo, 3% W, 1.5% Al | Aerospace, Automotive, Chemical Processing, Industrial Heating | furnace components, basket liners, radiant heating systems, heat recuperators, automotive catalytic converters, heat shields, strand annealing furnace tubes, gas separation units, fuel cells |
| HAYNES® 230 | N06230 | Common Name: Nickel Alloy 230 European Designation: 2.4733 Other designations may be available by request | ASTM Specifications: ASTM B435 (Strip) AMS Specifications: AMS 5878 (Strip) Additional specifications may be available by request | High Performance Alloy Heat Resistant Alloy / High Temperature Alloy | Chemical Properties: Oxidation resistance to 1149°C (2100°F). Physical Properties: Outstanding high-temperature stability. Excellent creep and fatigue strength. Resists grain coarsening. Temperature Range: Up to 1149°C (2100°F). | HAYNES® 230 is a high-temperature, solid-solution nickel-chromium-tungsten-molybdenum alloy with outstanding oxidation resistance up to 2100°F (1149°C) for prolonged exposures and long-term stability in extreme heat applications; higher temperatures are possible for shorter durations. This alloy has lower thermal expansion characteristics than most high-temperature alloys and resists grain coarsening, maintaining mechanical integrity during prolonged exposure to elevated temperatures. With excellent creep and fatigue resistance, HAYNES® 230® is ideal for demanding applications such as combustion liners, furnace hardware, and industrial gas turbines. Typical composition: ~57% Ni, 22% Cr, 14% W, 2% Mo | Aerospace, Industrial Heating, Power Generation, Chemical Processing | gas turbine components, high-temperature bellows, furnace components, catalyst grid supports |
| HAYNES® 233 | N02233 | Common Name: Nickel Alloy 233 Other designations may be available by request | Please contact us with your requirements. | Heat Resistant Alloy / High Temperature Alloy | Chemical Properties: Excellent oxidation resistance above 980°C (1800°F). Resistant to hot corrosion and thermal fatigue. Physical Properties: High strength with good ductility. Maintains mechanical integrity during cycling. Temperature Range: Above 980°C 1800°F). | HAYNES® 233 is a next-generation, solid-solution nickel-based alloy providing excellent creep strength (similar to HAYNES® 230) and oxidation resistance above 980°C (1800°F) (close to the resistance of HAYNES® 214). With high levels of chromium, molybdenum, tungsten, and aluminium, it offers improved hot corrosion and thermal cycling resistance compared to traditional alloys. This alloy exhibits good hot workability, cold formability and is readily weldable and fabricable. When age hardened by heat treatment, HAYNES® 233 can be strengthened. HAYNES® 233 is engineered for structural stability and long-term reliability during thermal cycling. It offers exceptional resistance to hot corrosion, making it suitable for the most severe industrial heating and power generation environments. Typical composition: ~63% Ni, 22% Cr, 3% Al, 4% Mo, 2% W | Aerospace, Industrial Heating, Power Generation, | gas turbine components, structural components, retorts, furnace components, heat exchangers |
| HAYNES® 242 | N10242 | Common Name: Nickel Alloy 242 European Designation: 2.4816 Other designations may be available by request | ASTM Specifications: ASTM B434 (Strip) Additional specifications may be available by request | Superalloy Heat Resistant Alloy / High Temperature Alloy Corrosion-Resistant Alloy | Chemical Properties: Good oxidation resistance. Physical Properties: Age-hardenable with low thermal expansion. Excellent strength at elevated temperatures. Outstanding dimensional stability. | HAYNES® 242 is a controlled expansion, age-hardenable nickel-molybdenum-chromium alloy offering a combination of low thermal expansion, high strength, and good oxidation resistance. Its excellent strength-to-expansion ratio makes it ideal for dimensional stability in elevated-temperature environments. Typical composition: ~60% Ni, 25% Mo, 8% Cr | Aerospace, Industrial Heat Treating, Power Generation, Chemical Processing, Nuclear Fuel Processing | springs, seal rings, containment rings, rocket nozzles, pumps, high temperature fluoride bearing environments, duct segments, casings, fasteners, acid processing equipment |
| HAYNES® 263 | N07263 | Common Name: Nickel Alloy 263 European Designation: 2.4650 Other designations may be available by request | AMS Specifications: AMS 5872 (Strip) Additional specifications may be available by request | Heat Resistant Alloy / High Temperature Alloy High Strength Alloy | Chemical Properties: Resistant to strain-age cracking. Physical Properties: Excellent aged strength properties. Good ductility at intermediate temperatures. Workability: Superior weldability. | HAYNES® 263 is an age-hardenable nickel-cobalt-chromium-molybdenum alloy known for excellent strength and ductility at elevated temperatures. It features superior weldability in the annealed condition and does not typically exhibit strain-age cracking, a common issue with other gamma prime-strengthened alloys. Though offering lower strength at high temperatures than Waspaloy® or R-41, HAYNES® 263 is significantly easier to form or weld in comparison. It is often chosen for turbine and combustor components where weld integrity and mechanical stability are critical. Typical composition: ~50% Ni, 20% Cr, 6% Mo, 2% Co, 0.6% Ti, 0.5% Al | Aerospace, Land Based Turbines | air and land-based turbines, low temperature combustors, transition liners, rings |
| HAYNES® 282 | N07208 | Common Name: Nickel Alloy 282 Other designations may be available by request | AMS Specifications: AMS 5951 (Strip) Additional specifications may be available by request | High Performance Alloy Superalloy Heat Resistant Alloy / High Temperature Alloy High Strength Alloy | Chemical Properties: Excellent oxidation resistance. Physical Properties: Superior creep strength at 649–927°C (1200°F to 1700°F). Microstructurally stable during long-term exposure. Workability: Good weldability and fabricability. | HAYNES® 282 is a precipitation-hardenable nickel superalloy offering a breakthrough combination of high-temperature strength, fabricability, and weldability. Designed for long-term service at temperatures between 649°C and 927°C (1200°F to 1700°F), superior to Waspaloy® and approaching that of R-41. It exhibits exceptional creep resistance while allowing for easier forming and joining processes. Modest gains in physical properties are possible when HAYNES® 282 is aged from the annealed condition or cold-reduced condition. Its microstructural stability and mechanical performance make it a top candidate for high-efficiency turbine engines and exhaust systems. Typical composition: ~57% Ni, 20% Cr, 10% Co, 8.5% Mo, 1.5% Al, 2.1% Ti | Aerospace, Automotive, Land Based Turbines | air/ land-based turbines, aerospace exhaust nozzles and seals, high-temperature automotive gaskets and seals |
| Haynes® 25 / L605 | R30605 | European Designation: 2.4964 / 2.4967 Other designations may be available by request | ASTM Specifications: ASTM F90 (Wire) AMS Specifications: AMS 5537 (Strip & Foil), AMS 5796 (Wire) Other Specifications: Rolls Royce MSRR 7053, NACE MR0175/ISO 15156-3, ISO 5832-5 Additional specifications may be available by request | Superalloy Heat Resistant Alloy / High Temperature Alloy Corrosion-Resistant Alloy: High Strength Alloy | Chemical Properties: Excellent oxidation resistance up to 1093°C (2000°F). Outstanding resistance to sulfidation and carburisation. Good resistance to acids, including hydrochloric and nitric acid. Physical Properties: Solid-solution strengthened with excellent high-temperature strength. Good wear and galling resistance. Non-magnetic properties. Workability: Good forming and welding characteristics. Responds well to cold working (work-hardens rapidly). Excellent formability amongst cobalt alloys. SERVICE Temperature Range: Continuous service up to 980°C (1795°F), intermittent to 1093°C (2000°F). | Alloy L605, also known as Haynes® Alloy 25, is a high-performance, Cobalt-Chromium-Tungsten solid-solution strengthened superalloy. It is known for its exceptional strength, corrosion resistance, and high-temperature stability. This versatile material offers a wide range of benefits, making it an attractive choice for manufacturers in various industries. Alloy L605 boasts remarkable strength, making it suitable for applications that require high load-bearing capacity and resistance to deformation. This alloy exhibits excellent resistance to various types of corrosion, including oxidation, carburisation and sulfidation, particularly in harsh environments and under extreme conditions. Even at temperatures up to 1093°C (2000°F), this alloy demonstrates excellent oxidation resistance, ensuring a long service life in challenging environments. Mechanical properties are maintained at elevated temperatures, making it suitable for high-temperature applications, such as jet engines and gas turbines. Good fatigue, galling, and exceptional wear resistance make it well-suited for applications where components are subjected to friction and wear. This alloy can also be easily formed and machined and offers good weldability. | Medical, Aerospace, Land-Based Turbines, Power Generation, Electronics | Bearings, shafts, springs, combustor liners, furnace liners, gas turbine rotors, nozzle diaphragm valves, springs, heart valves and surgical fixation wire, seal rings for gas turbines, jet engine components, high temperature ball bearings |
| Haynes® 188 Alloy | R30188 | European Designation: 2.4683 Other designations may be available by request | AMS Specifications: AMS 5608 (Strip & Foil) Other Specifications: GE B50A712, PWA 1042, Rolls Royce MSRR 7165 Additional specifications may be available by request | High Performance Alloy Heat Resistant Alloy / High Temperature Alloy Corrosion-Resistant Alloy: | Chemical Properties: Excellent oxidation resistance up to 1095°C (2000°F). Outstanding sulfidation resistance. Excellent resistance to hot corrosion and thermal fatigue. Physical Properties: Excellent high-temperature strength and stability. Good ductility is maintained at elevated temperatures. Superior thermal fatigue resistance. Workability: Good forming and welding characteristics. Not age-hardenable but strengthened through cold working. Easily formed and machined. SERVICE Temperature Range: Long-term continuous exposure up to 1095°C (2000°F), intermittent to 1149°C (2100°F). | Haynes® 188 Alloy is a high-performance, cobalt-nickel-chromium-tungsten alloy known for its excellent strength, oxidation resistance, high-temperature stability and exceptional wear resistance. Haynes® Alloy 188 is not age hardenable but may be cold-worked to achieve higher tensile and yield strength. In addition to its remarkable strength, this alloy exhibits excellent oxidation resistance, even at temperatures up to 1149°C (2100°F), ensuring a long service life in challenging environments. Haynes® 188 maintains its mechanical properties at elevated temperatures, making it suitable for high-temperature applications. Sulfidation resistance is another key benefit, making it ideal for applications where components are exposed to sulfur-containing environments. The alloy is also known for its good weldability and can be easily formed and machined. | Aerospace, Chemical Processing, Land-Based Gas Turbines, Nuclear Energy | Combustor liners and cans, furnace liners, flame hoods, gas turbine rotors, and nozzle diaphragm valves, heat exchangers, transition ducts, afterburner components |
| Haynes® is a registered trademark of HAYNES INTERNATIONAL INC®. The information provided is for reference only. Typical properties and application guidance should not be used as a substitute for the full requirements specified in recognised standards (ASTM, DIN, EN). Producer datasheets may apply narrower limits or additional restrictions depending on form, processing, and intended use. Always confirm material suitability with technical support before final selection. | ||||||||
| Rene® | ||||||||
| Commercial Name (Nearest Fit) | UNS (Nearest) | Other Designations (Nearest Fit) | Applicable Specifications | Classifications | Notable Properties | Alloy Description | Key Markets | Applications |
| RENE®41 | N07041 | Common Name: Nickel Alloy 41 European Designation: 2.4973 Other designations may be available by request | AMS Specifications: AMS 5545 (Strip), AMS 5800 (Wire) Other Specifications: GE B50T59 (Strip), GE B50TF109 (Strip) Additional specifications may be available by request | High Performance Alloy Superalloy High Strength Alloy | Chemical Properties: Excellent oxidation resistance. Physical Properties: Precipitation-hardenable high-strength alloy. Relaxation resistance to 815°C (1500°F). Excellent creep resistance. Ideal for fasteners and springs. | RENE® 41 is a precipitation-hardenable nickel-chromium alloy engineered for high strength and oxidation resistance at elevated temperatures. It is specifically formulated for structural and fastener applications requiring reliable mechanical performance at temperatures 649°C to 982°C (1200°F-1800°F). The alloy’s capability to resist stress relaxation makes it ideal for spring and fastening components in high-temperature aerospace and automotive systems. The mechanical properties of RENE® 41 can be further tailored by combinations of annealing and ageing treatments. With excellent creep resistance and thermal stability, RENE® 41 maintains mechanical properties over long service durations in demanding environments. It is typically supplied in wire and strip form for precision components. Typical composition: ~56% Ni, 19% Cr, 11% Co, 10% Mo, 1.6% Ti, 1.5% Al, balance Fe | Aerospace, Automotive | springs, turbine blades, fasteners, pumps, combustion chamber liners, structural hardware |
| Rene® is a registered trademark of General Electric Inc.®. The information provided is for reference only. Typical properties and application guidance should not be used as a substitute for the full requirements specified in recognised standards (ASTM, DIN, EN). Producer datasheets may apply narrower limits or additional restrictions depending on form, processing, and intended use. Always confirm material suitability with technical support before final selection. | ||||||||
| WASPALOY® | ||||||||
| Commercial Name (Nearest Fit) | UNS (Nearest) | Other Designations (Nearest Fit) | Applicable Specifications | Classifications | Notable Properties | Alloy Description | Key Markets | Applications |
| WASPALOY® | N07001 | European Designation: 2.4654 Other designations may be available by request | AMS Specifications: AMS 5544 (Strip) AMS 5828 (Wire) Additional specifications may be available by request | High Performance Alloy Superalloy High Strength Alloy | Chemical Properties: Outstanding oxidation resistance. Physical Properties: High-temperature strength to 870°C (1600°F). Outstanding fatigue resistance. Excellent relaxation and creep resistance. Suitable for critical rotating components. | WASPALOY® is a nickel-based, precipitation-hardenable superalloy developed for high mechanical strength and oxidation resistance at elevated temperatures. It offers superior resistance to relaxation and thermal fatigue, surpassing the performance of alloy 718, making it a preferred material choice for aerospace and gas turbine applications. With exceptional creep and rupture strength maintained up to 870°C (1600°F), WASPALOY® is frequently used in environments that demand both structural reliability and long-term thermal stability. It demonstrates good weldability when processed under controlled conditions and is supplied in strip and wire forms ideal for precision-engineered components. Typical composition: ~58% Ni, 19.5% Cr, 13.5% Co, 4.3% Mo, 3% Ti, 1.4% Al, balance Fe | Aerospace, Automotive, Defence, Land-Based Gas Turbines, Oil & Gas | gas turbine components, seals, springs, fasteners, compressor and rotator discs, shafts, spacers, rings and casings, airframe assemblies, missile systems |
| WASPALOY® is a registered trademark of United Technologies Corporation®. The information provided is for reference only. Typical properties and application guidance should not be used as a substitute for the full requirements specified in recognised standards (ASTM, DIN, EN). Producer datasheets may apply narrower limits or additional restrictions depending on form, processing, and intended use. Always confirm material suitability with technical support before final selection. | ||||||||
| MONEL® | ||||||||
| Commercial Name (Nearest Fit) | UNS (Nearest) | Other Designations (Nearest Fit) | Applicable Specifications | Classifications | Notable Properties | Alloy Description | Key Markets | Applications |
| MONEL® alloy 400 | N04400 | Common Name: Nickel Alloy 400 European Designation: 2.4360 / 2.4361 Other designations may be available by request | British Specifications: BS NA13 (Wire) ASTM Specifications: ASTM B127 (Strip), ASTM B164 (Wire) AMS Specifications: AMS 4544 (Strip), AMS 4730 (Wire) Other Specifications: ASME SB-127 (Strip), NACE MR0175 (ISO 1516-3) (Wire) Additional specifications may be available by request | Corrosion-Resistant Alloy | Chemical Properties: Outstanding corrosion resistance in seawater. Resistant to hydrofluoric and sulfuric acids. Physical Properties: High strength and good ductility. Non-magnetic in the annealed condition. | MONEL® 400 is a solid-solution nickel-copper alloy known for its excellent corrosion resistance, especially in marine and chemical processing environments. With high strength, toughness, and resistance to a broad range of corrosive conditions—including seawater, sulfuric acid and hydrochloric acid—this alloy is widely used in demanding structural applications. It retains ductility at subzero temperatures and oxidation resistance at cryogenic temperatures to 260°C (500°F). MONEL® 400 also exhibits resistance to stress corrosion cracking in fresh water. This alloy does not require age-hardening treatments to obtain its high-strength properties and is hardened only through cold working. MONEL® 400 retains its mechanical properties across a broad temperature range and is available in both cold-worked and annealed tempers, supplied in precision strip and wire. Typical composition: ~67% Ni, 30% Cu, small amounts of Fe, Mn, and Si | Aerospace, Oil & Gas, Marine, Chemical Processing, Petrochemical Processing | bellows, heat exchangers, propeller shafts, marine fixtures and fasteners, braiding, components for marine engineering and chemical processing, packed columns, pressure vessels and reactors, brine heaters, salt production equipment pump and valve components pipe work and pipe spools |
| MONEL® alloy K500 | N05500 | Common Name: Nickel Alloy K500 European Designation: 2.4375 Other designations may be available by request | British Specifications: BS NA18 (Wire) ASTM Specifications: ASTM B127 (Strip), ASTM B164 (Wire) AMS Specifications: AMS 4676 (Wire) Additional specifications may be available by request | High Performance Alloy Corrosion-Resistant Alloy High Strength Alloy | Chemical Properties: Non-magnetic and corrosion-resistant. Maintains mechanical integrity in marine and chemical environments. Physical Properties: Precipitation-hardened for superior strength. High fatigue strength in seawater. | MONEL® K500 is a precipitation-hardened nickel-copper alloy that builds upon the corrosion resistance of MONEL® 400 with increased strength and hardness. The age-hardening process introduces intermetallic compounds, resulting in a non-magnetic alloy with excellent fatigue and erosion resistance in marine and chemical environments. The alloy is particularly suited to high-strength components exposed to seawater and harsh industrial media. It is supplied in precision wire and strip forms. Typical composition: ~63% Ni, 30% Cu, 2.7-3.3% Al, 0.35-0.85% Ti, balance Fe and other elements | Oil & Gas, Chemical, Power Generation, Marine, Medical, Electronics | propellers, fasteners, gyroscopes, medical blades, pump shafts, drill collars, valve components, springs, blades and scrapers, oil-weld tools and chains |
| Monel® is a registered trademark of Special Metals Corporation®. Typical properties and application guidance should not be used as a substitute for the full requirements specified in recognised standards (ASTM, DIN, EN). Producer datasheets may apply narrower limits or additional restrictions depending on form, processing, and intended use. Always confirm material suitability with technical support before final selection. | ||||||||
| Nimonic® | ||||||||
| Commercial Name (Nearest Fit) | UNS (Nearest) | Other Designations (Nearest Fit) | Applicable Specifications | Classifications | Notable Properties | Alloy Description | Key Markets | Applications |
| NIMONIC® alloy 75 | N06075 | Common Name: Nickel Alloy 75 European Designation: 2.4951 Other designations may be available by request | British Specifications: BS 2HR 203:2009 (Strip) Additional specifications may be available by request | Superalloy | Chemical Properties: Excellent oxidation resistance to 1000°C (1832 °F). Physical Properties: Good ductility and workability. Stable under thermal cycling. Workability: Easily formed and welded. Temperature Range: Up to 1000°C (1832°F). | NIMONIC® 75 is a nickel-chromium alloy offering moderate high-temperature strength with excellent oxidation and scaling resistance. It is widely recognised for its ease of fabrication and good weldability, making it suitable for cold deformation processes. The alloy maintains good mechanical properties up to 1000°C (1832°F), and its stable structure under thermal cycling makes it well-suited for sheet and wire applications in heat-treating and aerospace systems. Typical composition: ~80% Ni, 20% Cr, with minor amounts of Ti, Mn, and C | Aerospace, Industrial Heating, Thermal Engineering | turbine blades, furnace components, heat treatment equipment, exhaust systems |
| NIMONIC® alloy 90 | N07090 | Common Name: Nickel Alloy 90 European Designation: 2.4632 / 2.4969 Other designations may be available by request | British Specifications: BS NA19 (Wire), BS HR 501 (Wire), BS HR 502 (Wire), BS HR 503 (Wire) AMS Specifications: AMS 5829 (Wire) Other Specifications: NACE MR0175 / ISO 15156-3 (Wire), NACE MR0103 (Wire) Additional specifications may be available by request | Superalloy High Strength Alloy | Physical Properties: Excellent high-temperature strength and creep resistance. Precipitation hardened via gamma (γ) phase. Good fatigue strength. Reliable performance in elevated service conditions. | NIMONIC® 90 is a precipitation-hardenable nickel-chromium-cobalt alloy designed for high tensile and creep strength at elevated temperatures. Reinforced with titanium and aluminium for γ′ precipitation strengthening, it is extensively used in aircraft engine components and other high-temperature applications where fatigue resistance and structural stability are essential. The alloy is supplied in precision wire form and is optimised for demanding spring and fastener applications in extreme service environments. Typical composition: ~58% Ni, 19.5% Cr, 17% Co, 2.5% Ti, 1.4% Al | Aerospace, Power Generation | aerospace springs and components, turbine discs, hot section engine components, combustion system parts |
| Nimonic® is a registered trademark of Special Metals Corporation®. Typical properties and application guidance should not be used as a substitute for the full requirements specified in recognised standards (ASTM, DIN, EN). Producer datasheets may apply narrower limits or additional restrictions depending on form, processing, and intended use. Always confirm material suitability with technical support before final selection. | ||||||||
| Nichrome Electrical Resistance Alloys | ||||||||
| Commercial Name (Nearest Fit) | UNS (Nearest) | Other Designations (Nearest Fit) | Applicable Specifications | Classifications | Notable Properties | Alloy Description | Key Markets | Applications |
| Nichrome 40 37/18 Ni Cr Resistance Wire Ni Cr 37/18 (D Grade Family) | - | Common Name: Nichrome 40 37/18 Ni Cr Resistance Wire Ni Cr 37/18 (D Grade Family) Other designations may be available by request | Please contact us with your requirements. | Resistance Nickel Alloy | Chemical Properties: Excellent resistance to oxidising environments. Physical Properties: Stable in dry furnace conditions. Temperature Range: Up to 1050°C (1922°F). | NiCr 37/18 is a nickel-chromium alloy with a balance primarily of iron, suitable for continuous service in oxidising furnace atmospheres up to 1050°C (1922°F). Its composition helps prevent dry corrosion where higher-nickel content materials might fail, making it especially valuable for resistance heating in challenging atmospheres. | Power Generation, Chemical Processing, Heat Treatment | electric heaters, electric furnaces (with atmospheres). |
| Nichrome 60 60/15/ Ni Cr Resistance Wire Ni Cr 60/15 (C Grade Family) | N06004 | Common Name: Nichrome 60 60/15/ Ni Cr Resistance Wire Ni Cr 60/15 (C Grade Family) European Designation: 2.4867 Other designations may be available by request | European Specifications: DIN 17470 (Wire) British Specifications: ASTM B344 (Wire) Additional specifications may be available by request | Resistance Nickel Alloy | Physical Properties: Long life in high-temperature use. Suitable for less critical electrical resistance applications. Temperature Range: Up to 1100°C (2012°F). | NiCr 60/16 is a nickel-chromium alloy with a significant iron balance and life-extending alloying elements. With operating limits up to 1100°C (2012°F), it offers durability in high-temperature conditions and is ideal for heating elements and resistive components. | Power Generation, Chemical Processing, Heat Treatment | electric heaters, heavy duty resistors, electric furnaces |
| Nichrome 80 80/20 Ni Cr Resistance Wire Ni Cr 80/20 (A Grade Family) | N06003 | Common Name: Nichrome 80 80/20 Ni Cr Resistance Wire Ni Cr 80/20 (A Grade Family) European Designation: 2.4869 Other designations may be available by request | European Specifications: DIN 17470 (Wire) British Specifications: ASTM B344 (Wire) Additional specifications may be available by request | Resistance Nickel Alloy | Physical Properties: Exceptional resistance to thermal shock. Excellent for control and resistive heating applications. Temperature Range: Up to 1150°C (2102°F). | NiCr 80/20 is a high-performance heating alloy containing 80% nickel and 20% chromium. Its high temperature capability, up to 1150°C (2102°F) and resilience to frequent thermal cycling make it ideal for heating elements subject to repeated on/off switching. | Power Generation, Chemical Processing, Heat Treatment | control resistors, high temperature furnaces, soldering irons |
| The information provided on Nichrome electrical resistance alloys is for reference only. Typical properties and application guidance should not be used as a substitute for the full requirements specified in recognised standards (ASTM, DIN, EN). Producer datasheets may apply narrower limits or additional restrictions depending on form, processing, and intended use. Always confirm material suitability with technical support before final selection. | ||||||||
| Controlled Expansion Alloys / Glass Sealing Nickel Alloys | ||||||||
| Nilo® | ||||||||
| Commercial Name (Nearest Fit) | UNS (Nearest) | Other Designations (Nearest Fit) | Applicable Specifications | Classifications | Notable Properties | Alloy Description | Key Markets | Applications |
| Nilo® K / KOVAR® | K94610 | Common Name: Alloy 29/18 European Designation: 1.3981 Other designations may be available by request | European Specifications: DIN 17745 (Wire) ASTM Specifications: ASTM F15 (Strip & Wire) Additional specifications may be available by request | Resistance Nickel Alloy Glass Sealing Alloy / Low Thermal Expansion Alloy | Controlled Expansion Alloys - Thermal Characteristics: CTE: ~4.9 ×10⁻⁶/°C at 20-400°C (2.7 ×10⁻⁶/°F at 68–752°F), ~ 5.3 ×10⁻⁶/°C at 20–450°C (~ 2.9 ×10⁻⁶/°F at 68–842°F): matches borosilicate glasses. Material Selection: Optimised for hermetic seals to borosilicate glasses and alumina ceramics, the oxide layer promotes adhesion. Inflection point ~450°C (840°F). Glass Sealing: Optimised for borosilicate glasses with thermal expansion matching. Hermetic Sealing: All Nilo® alloys form reliable metal-glass bonds through intermediate oxide layers. Electrical Resistivity: 43.0 µΩ·cm / 0.43 μΩ·m at 20°C (16.93 µΩ·in / 1.41 µΩ·ft at 70°F). | Nilo® K (Alloy 29/18) is a controlled-expansion nickel-cobalt-iron alloy whose chemical composition is controlled within narrow limits to ensure precise and uniform thermal expansion characteristics. The alloy provides excellent thermal expansion matching with borosilicate glasses and alumina ceramics, exhibiting a coefficient of expansion that decreases with increasing temperature to match the expansion rates of these materials. Nilo® K exhibits exceptional reliability in glass-to-metal sealing applications and demonstrates excellent resistance to thermal shock. The alloy offers good machinability and deep-drawing properties while maintaining dimensional stability over a wide temperature range. This sealing alloy forms strong metallurgical bonds with glass through intermediate oxide layers, providing long-term hermetic integrity. | Electronics, Telecommunications, Automotive, Aerospace, Scientific Instruments | glass-to-metal seals, hermetic seals, electronics, vacuum tubes, microwave tubes, transistor leads and headers, diodes, integrated circuit lead frames, photography flash bulbs, cathode ray tubes, scientific instruments, lighting |
| Nilo® 36 / Invar 36® | K93600 | Common Name: NiFe36 Alloy 36 European Designation: 1.3912 Other designations may be available by request | ASTM Specifications: ASTM B388 (Strip) Additional specifications may be available by request | Resistance Nickel Alloy Glass Sealing Alloy / Low Thermal Expansion Alloy | Physical Properties: Low thermal expansion (to ~230°C / 430°F). High-dimensional stability. Suitable for cryogenic and precision environments. Controlled Expansion Alloys - Thermal Characteristics: Ultra-low expansion: ~1.5 ×10⁻⁶/°C at 20–100°C (0.8 ×10⁻⁶/°F at 68–212°F), ~2.6 × 10⁻⁶/°C at 20-200°C (1.4 × 10⁻⁶/°F at 68-392°F), ~5.5 ×10⁻⁶/°C at 20–300°C (~3.1 ×10⁻⁶/°F at 68–572°F) - amongst the lowest of all engineering alloys. Inflection point ~220°C (430°F). Material Selection: Best choice for applications requiring minimal thermal expansion near room temperature. Hermetic Sealing: All Nilo® alloys form reliable metal-glass bonds through intermediate oxide layers. Electrical Resistivity: 80.0 µΩ·cm / 0.80 μΩ·m at 20°C (31.50 µΩ·in / 2.63 µΩ·ft at 70°F). Temperature Range: Cryogenic to approximately 230°C (450°F). | Nilo® 36 (NiFe36) is a low-expansion nickel-iron alloy that maintains near-constant dimensions over normal atmospheric temperatures. The alloy exhibits an exceptionally low coefficient of thermal expansion (≤ 1.3 × 10⁻⁶/°C) from cryogenic temperatures to approximately 200°C (392°F) , providing unparalleled dimensional stability. Nilo® 36 (NiFe36) retains excellent strength and toughness at cryogenic temperatures whilst demonstrating superior resistance to thermal shock and thermal cycling. The alloy offers good machinability and formability using conventional processing techniques similar to austenitic stainless steels. This controlled expansion alloy is weldable and maintains its ultra-low expansion characteristics after welding when following recommended practice. | Precision Engineering, Aerospace, Cryogenics, Telecommunications, Scientific Instruments | precision measuring instruments, thermostat rods, laser components, cryogenic storage tanks, composite tooling, seismic instruments, clock pendulums, optical devices, scientific and optical instrumentation |
| Nilo® 42 | K94100 | Common Name: NiFe42 Alloy 42 European Designation: 1.3917 Other designations may be available by request | European Specifications: DIN 17745 (Wire) ASTM Specifications: ASTM F30 (Wire) Additional specifications may be available by request | Resistance Nickel Alloy Glass Sealing Alloy / Low Thermal Expansion Alloy | Physical Properties: Stable at elevated temperatures. Compatible with soft glass. Maintains structural integrity during thermal cycling. Controlled Expansion Alloys - Thermal Characteristics: Controlled expansion ~ 5.3 × 10⁻⁶/°C at 20-300°C (~ 2.9 × 10⁻⁶/°C at 68-572°F) typically ~ 6.2 ×10⁻⁶/°C at 20-400°C (~ 3.4 ×10⁻⁶/°F at 68-752°F): for specific glass matching. Inflection point ~370°C (700°F). Material Selection: Intermediate expansion alloy for moderate temperature glass sealing applications. Hermetic Sealing: All Nilo® alloys form reliable metal-glass bonds through intermediate oxide layers. Electrical Resistivity: 61.0 µΩ·cm / 0.61 μΩ·m at 20°C (24.02 µΩ·in / 2.00 µΩ·ft at 68°F). | Nilo® 42 (NiFe42) is a controlled expansion nickel-iron alloy designed to provide a constant low rate of thermal expansion up to temperatures approaching 350°C (662°F). The alloy offers excellent thermal expansion matching characteristics with specific glasses and ceramics, making it suitable for glass-to-metal sealing applications where moderate expansion control is required. Nilo® 42 (NiFe42) demonstrates good machinability and formability with processing characteristics similar to austenitic stainless steels. The alloy maintains structural integrity and dimensional stability under thermal cycling conditions whilst offering reliable weldability. This sealing alloy provides consistent expansion properties and forms reliable hermetic seals in electronic and vacuum applications whilst exhibiting controlled magnetic properties. | Electronics, Telecommunications, Scientific Instruments, Glass industry | glass-to-metal seals, electronic tube seals, hermetic packaging, transformer cores, relay components, magnetic shielding applications, electronic components and semiconductors |
| Nilo® 48 | K94800 | Common Name: NiFe48 Alloy 48 European Designation: 1.3922 Other designations may be available by request | European Specifications: DIN 17745 (Wire) ASTM Specifications: ASTM F30 (Wire) Additional specifications may be available by request | Resistance Nickel Alloy Glass Sealing Alloy / Low Thermal Expansion Alloy | Controlled Expansion Alloys - Thermal Characteristics: Intermediate expansion characteristics between Nilo® 42 and Nilo® 52, ~8.6-8.7 ×10⁻⁶/°C across 20–300°C (~4.8 ×10⁻⁶/°F across 68–572°F); suited to soda-lime/soft-glass seals. Inflection point ~460°C (860°F). Material Selection: Specialised alloy for specific glass expansion matching requirements. Good mechanical stability. Hermetic Sealing: All Nilo® alloys form reliable metal-glass bonds through intermediate oxide layers. Electrical Resistivity: 47.0 µΩ·cm / 0.47 μΩ·m at 20°C (18.50 µΩ·in / 1.54 µΩ·ft at 70°F). | Nilo® 48 (NiFe48) is a controlled expansion nickel-iron alloy developed for applications requiring specific thermal expansion characteristics intermediate between Nilo® 42 (NiFe42) and Nilo® 52 (NiFe52). The alloy provides controlled thermal expansion properties closely matching those of soft glasses and ceramics, with expansion rates requiring this intermediate nickel content, making it ideal for precision sealing applications. Nilo® 48 (NiFe48) offers good machinability and can be processed using conventional metalworking techniques whilst maintaining dimensional stability. The alloy demonstrates reliable weldability and maintains consistent expansion properties after welding operations. This sealing alloy provides reliable performance under thermal cycling whilst offering the magnetic properties associated with nickel-iron alloys in this composition range. | Electronics, Scientific Instruments, Telecommunications | glass-to-metal seals, electronic packaging, vacuum tube applications, scientific instrument components, magnetic applications |
| Nilo® 52 | N14052 | Common Name: NiFe52 Alloy 52 European Designation: 2.4478 Other designations may be available by request | ASTM Specifications: ASTM F30 (Wire) Additional specifications may be available by request | Corrosion-Resistant Alloy Resistance Nickel Alloy Glass Sealing Alloy / Low Thermal Expansion Alloy | Physical Properties: High nickel content for expansion control. Reliable glass sealing performance. Controlled Expansion Alloys - Thermal Characteristics: Stable expansion ~10.2 ×10⁻⁶/°C across 20–300°C ( ~5.7 ×10⁻⁶/°F across 68–572°F). Material Selection: Ideal for soft glass sealing and magnetic reed switch applications. Hermetic Sealing: All Nilo® alloys form reliable metal-glass bonds through intermediate oxide layers. Magnetic Properties: High magnetic permeability and saturation induction are ideal for electromagnetic applications. Electrical Resistivity: 38.0 µΩ·cm / 0.38 μΩ·m at 20°C (14.96 µΩ·in / 1.25 µΩ·ft at 70°F). | Nilo® 52 (NiFe52) is a controlled expansion nickel-iron alloy, containing 52% nickel, designed for glass-to-metal sealing applications with soft glasses and selected ceramics. The alloy exhibits a virtually constant coefficient of thermal expansion up to approximately 565°C (1050°F), providing excellent dimensional stability over a wide temperature range. Nilo® 52 (NiFe52) demonstrates high magnetic permeability and saturation magnetic induction, making it suitable for magnetic applications including reed switches and electromagnetic devices. The alloy offers good machinability and can be formed using conventional processing techniques whilst maintaining its controlled expansion characteristics. This sealing alloy exhibits excellent resistance to thermal shock and maintains structural integrity under repeated thermal cycling conditions. | Electronics, Telecommunications, Automotive | glass-to-metal seals, magnetic reed switches, electronic packaging, soft glass sealing applications, electromagnetic components, microwave cavity resonators, shadow masks |
| Nilo® is a registered trademark of Special Metals Corporation®. Kovar® is a registered trademark of CRS Holdings. Invar® is a registered trademark of Aperam Alloys Imphy. Typical properties and application guidance should not be used as a substitute for the full requirements specified in recognised standards (ASTM, DIN, EN). Producer datasheets may apply narrower limits or additional restrictions depending on form, processing, and intended use. Always confirm material suitability with technical support before final selection. | ||||||||
| Ni-Span-C® | ||||||||
| Commercial Name (Nearest Fit) | UNS (Nearest) | Other Designations (Nearest Fit) | Applicable Specifications | Classifications | Notable Properties | Alloy Description | Key Markets | Applications |
| NI-SPAN-C® ALLOY 902 | N09902 | Other designations may be available by request | AMS Specifications: AMS 5221 (Wire), AMS 5225 (Wire) Additional specifications may be available by request | Resistance Nickel Alloy | Physical Properties: Low magnetostriction. Controlled thermoelastic coefficient. Cryogenic performance. Temperature Range: Cryogenic applications. | NI-SPAN-C® Alloy 902 is a precipitation-hardenable nickel-iron alloy offering low magnetostrictive properties. It benefits from thermoelastic coefficient and mechanical properties that can be controlled by the amount of cold work and the heat treatment temperature, allowing it to meet the requirements of many applications, including those at cryogenic temperatures. NI-SPAN-C® Alloy 902 is ideal for vibration-sensitive and cryogenic applications | Precision Equipment Manufacturing, Industrial Heat Treatment, Chemical/Waste Processing, Food Processing | Precision instruments, resonant vibration systems, tuning forks, springs, cryogenic applications |
| Ni-Span® is a registered trademark of Special Metals Corporation®. Typical properties and application guidance should not be used as a substitute for the full requirements specified in recognised standards (ASTM, DIN, EN). Producer datasheets may apply narrower limits or additional restrictions depending on form, processing, and intended use. Always confirm material suitability with technical support before final selection. | ||||||||
| NOTES: All data is provided for informational purposes only. In no event will the Knight Group and its subsidiaries be liable for any action taken by any third party arising from using the information taken from our online or printed sources. Information should not be used to assess suitability for a particular use or application. Always confirm material suitability with technical support before final selection. The information and data provided are deemed to be accurate to the best of our knowledge and may be revised anytime without notice, and we assume no duty to update - Temperature limits refer to continuous service unless otherwise specified. - Actual service temperatures depend on specific application conditions, stress levels, and environmental factors. - Consult the manufacturer’s specifications for critical applications. - Composition ranges shown are typical; refer to applicable specifications for precise requirements. | ||||||||
Looking for nickel alloys in precision strip, sheet or wire?
Unlock the limitless potential of nickel alloys with the Knight Group. Contact us today to discuss your requirements and receive a tailored quotation.
Let our alloys propel your projects to new heights of success.
Use the links below or contact us directly at:
Precision Strip: +44 (0)121 322 8400
Precision Wire: +44 (0)1707 645261
All data is provided for informational purposes only. In no event will the Knight Group and its subsidiaries, be liable for in respect of any action taken by any third party arising from using the information taken from our online or printed sources. Chemical and Mechanical Properties should not be construed as maximum or minimum values for specifications, nor should information be used to assess suitability for a particular use or application. The information and data provided is deemed to be accurate to the best of our knowledge and may be revised anytime without notice and assume no duty to update
Error: Contact form not found.