UNS Nickel Alloys

Maraging 250™(also referred to as Maraging C25™ and Vascomax 250™) is a vacuum induction melted plus vacuum arc melted, low-carbon, nickel-cobalt-molybdenum high temperature alloy capable of attaining yield strengths in excess of 240 KSI (1655 MPA) through a simple, low temperature heat treatment. Maraging 250™ exhibits good ductility at high strength levels and is readily welded. Maraging C250™ is one of a family of "maraging" nickel steels (including Maraging 300™ and 350™), which are ductile in the solution treated condition and attains ultrahigh tensile strength by aging at temperatures in the range of 850/950 °F (454/510 °C). Available forms are seamless pipe, welded pipe, seamless tube, welded tube, bar, wire, sheet, plate, forgings, pipe fittings and flanges.

Specification:

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .

SIZE 0.5MM TO 6MM DIA WIRE.

.AVAILABLE IN STOCK.

Additional Information:

• Minimum Order Quantity: 10 Kilogram

INCONEL® alloy 718 (UNS N07718/W.Nr. 2.4668) is a high-strength, corrosion-resistant nickel chromium material used at -423° to 1300°F. Typical composition limits are shown in Table 1. The age-hardenable alloy can be readily fabricated, even into complex parts. Its welding characteristics, especially its resistance to postweld cracking, are outstanding. The ease and economy with which INCONEL alloy 718 can be fabricated, combined with good tensile, fatigue, creep, and rupture strength, have resulted in its use in a wide range of applications. Examples of these are components for liquid fueled rockets, rings, casings and various formed sheet metal parts for aircraft and land-based gas turbine engines, and cryogenic tankage. It is also used for fasteners and instrumentation parts.

Chemical Compositiona , %

Nickel (plus Cobalt) .......................................................50.00-55.00 Chromium......................................................................17.00-21.00
Iron .....................................................................................Balance*
Niobium (plus Tantalum)............................................4.75-5.50
Molybdenum .....................................................................2.80-3.30 Titanium.............................................................................0.65-1.15
Aluminum ..........................................................................0.20-0.80
Cobalt ...............................................................................1.00 max. Carbon..............................................................................0.08 max.
Manganese .......................................................................0.35 max.
Silicon ...............................................................................0.35 max. Phosphorus.....................................................................0.015 max. Sulfur...............................................................................0.015 max.
Boron ..............................................................................0.006 max. Copper..............................................................................0.30 max

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.

AVAILABLE IN STOCK

Additional Information:

• Minimum Order Quantity: 10 Kilogram

INCONEL® alloy X-750 (UNS N07750/W. Nr. 2.4669) is a precipitation-hardenable nickel-chromium alloy used for its corrosion and oxidation resistance and high strength at temperatures to 1300°F. Although much of the effect of precipitation hardening is lost with increasing temperature over 1300°F, heat-treated material has useful strength up to 1800°F. Alloy X-750 also has excellent properties down to cryogenic termperatures. Composition is shown in Table 1. The economics of INCONEL alloy X-750 coupled with its availability in all standard mill forms has resulted in applications in a wide variety of industrial fields. In gas turbines, it is used for rotor blades and wheels, bolts, and other structural members. INCONEL alloy X-750 is used extensively in rocket-engine thrust chambers. Airframe applications include thrust reversers and hot-air ducting systems. Large pressure vessels are formed from INCONEL alloy X-750. Other applications are heat-treating fixtures, forming tools, extrusion dies, and test machine grips. For springs and fasteners, INCONEL alloy X-750 is used from sub-zero to 1200°F. Depending on the application and the properties desired, various heat treatments are employed. For service above 1100°F, particularly where loads are to be sustained for long times, optimum properties are achieved by solution treating (2100°F) plus stabilization treating (1550°F) plus precipitation treating (1300°F). For service below 1100°F, the alloy may be strengthened by precipitation treating after hot or cold working or by precipitation treating after equalizing or solution treating. A furnace-cooling treatment is also used to develop optimum properties for some applications.

Chemical Composition,

Nickel (plus Cobalt)....................................................70.00 min. Chromium...................................................................14.0-17.0 Iron..................................................................................5.0-9.0 Titanium.......................................................................2.25-2.75 Aluminum....................................................................0.40-1.00
Niobium (plus Tantalum)..............................................0.70-1.20 Manganese.................................................................1.00 max. Silicon.........................................................................0.50 max. Sulfur...........................................................................0.01 max. Copper........................................................................0.50 max. Carbon........................................................................0.08 max.
Cobalt1 .........................................................................1.00 max

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.

.AVAILABLE IN STOCK.

Additional Information:

• Minimum Order Quantity: 10 Kilogram

INCONEL® alloy 617 (UNS N06617/W.Nr. 2.4663a) is a solid-solution, strengthened, nickel-chromium-cobaltmolybdenum alloy with an exceptional combination of high-temperature strength and oxidation resistance. The alloy also has excellent resistance to a wide range of corrosive environments, and it is readily formed and welded by conventional techniques. The limiting chemical composition of INCONEL alloy 617 is listed in Table 1. The high nickel and chromium contents make the alloy resistant to a variety of both reducing and oxidizing media. The aluminum, in conjunction with the chromium, provides oxidation resistance at high temperatures. Solid-solution strengthening is imparted by the cobalt and molybdenum. The combination of high strength and oxidation resistance at temperatures over 1800°F (980°C) makes INCONEL alloy 617 an attractive material for such components as ducting, combustion cans, and transition liners in both aircraft and land-based gas turbines. Because of its resistance to high-temperature corrosion, the alloy is used for catalyst-grid supports in the production of nitric acid, for heat-treating baskets, and for reduction boats in the refining of molybdenum. INCONEL alloy 617 also offers attractive properties for components of power-generating plants, both fossilfueled and nuclear.

chemical in%
Nickel...........................................................................44.5 min. Chromium....................................................................20.0-24.0 Cobalt..........................................................................10.0-15.0
Molybdenum .................................................................8.0-10.0
Aluminum ........................................................................0.8-1.5
Carbon ........................................................................0.05-0.15 Iron................................................................................3.0 max.
Manganese ...................................................................1.0 max.
Silicon ...........................................................................1.0 max.
Sulfur ........................................................................0.015 max.
Titanium ........................................................................0.6 max. Copper..........................................................................0.5 max.
Boron ........................................................................0.006 max

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.

.AVAILABLE IN STOCK.

Additional Information:

• Minimum Order Quantity: 10 Kilogram

A-286 ALLOY

 

A-286 alloy is an age-hardenable iron base superalloy for applications requiring high strength from -320°F up to 1000°F long time, 1300-1500°F short time. Oxidation resistance is high for continuous service to 1500°F, intermittent to 1800°F. Aqueous corrosion resistance is comparable to 316/316L stainless. Heat treatment according to AMS 5525 requires a solution anneal at 1800°F, air cool. Age at 1325°F for 16 hours and then air cool.

Common Trade Names

A286 Stainless, A286 Alloy

Inventory

A-286 Sheet, A-286 Coil, A-286 Round Bar, A-286 Hex Bar

Specifications

UNS S66286, Werkstoff 1.4980, EN 1.4980
AMS: 5525, 5804, 5732, 5737
GE B50T1181, GE B50T12, GE B50T81

Chemical Composition, % Features

• High strength to 1000°F
• Oxidation resistant to 1500°F

Applications

• Jet engine components
• High temperature fasteners, springs
• Non-magnetic cryogenic equipment

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.

.AVAILABLE IN STOCK.

Additional Information:

• Minimum Order Quantity: 10 Kilogram

INCOLOY® alloy 925 (UNS N09925) is an agehardenable nickel-iron-chromium alloy with additions of molybdenum, copper, titanium and aluminum. The alloy’s chemical composition, listed in Table 1, is designed to provide a combination of high strength and excellent corrosion resistance. The nickel content is sufficient for protection against chloride-ion stresscorrosion cracking. The nickel, in conjunction with the molybdenum and copper, also gives outstanding resistance to reducing chemicals. The molybdenum aids resistance to pitting and crevice corrosion. The alloy’s chromium content provides resistance to oxidizing environments. The titanium and aluminum additions cause a strengthening reaction during heat treatment. INCOLOY alloy 925 is used in various applications requiring a combination of high strength and corrosion resistance. Because of the alloy’s resistance to sulfide stress cracking and stress-corrosion cracking in “sour” (H2S containing) crude oil and natural gas, it is used for down-hole and surface gaswell components including tubular products, valves, hangers, landing nipples, tool joints and packers. The alloy is also useful for fasteners, marine and pump shafting and high-strength piping systems.

Table 1 - Limiting Chemical Composition (UNS N09925) of INCOLOY alloy 925, % Nickel...........................................................................42.0-46.0
Chromium ....................................................................19.5-22.5 Iron...................................................................................22 min
Molybdenum ....................................................................2.5-3.5 Copper.............................................................................1.5-3.0
Titanium ...........................................................................1.9-2.4 Aluminum.........................................................................0.1-0.5
Manganese ...................................................................1.0 max.
Silicon ...........................................................................0.5 max. Niobium.........................................................................0.5 max.
Carbon ........................................................................0.03 max.
Sulfur ..........................................................................0.03 max.

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.

.AVAILABLE IN STOCK.

Additional Information:

• Minimum Order Quantity: 10 Kilogram

INCONEL™ 713C: FORGING FACTS & CHARACTERISTICS

Inconel 713C offers outstanding resistance to thermal fatigue and good castability while offering exceptional rupture strength at 1700°F (927°C). Inconel 713C is a nickel-chromium alloy that is ideally suited for jet engine gas turbine blades.

CHEMICAL COMPOSITION OF INCONEL™ 713C

• Carbon 0.20
• Manganese 1.0 max
• Sulfur 0.015 max
• Silicon 1.0 max
• Chromium 11.0-14.0
• Molybdenum 3.5-5.5
• Titanium 0.25-1.25
• Aluminum 5.5-6.5
• Iron 5.0 max
• Columbium + Ta 1.0-3.0
• Nickel remainder

APPLICATIONS OF INCONEL™ 713C

• Inconel 713C is most commonly used for jet engine gas turbine blades

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.

.AVAILABLE IN STOCK.

Additional Information:

• Minimum Order Quantity: 10 Kilogram

INCOLOY™ 901GENERAL CHARACTERISTICS OF INCOLOY™ 901

With a high creep and rupture strength to 1400°F (760°C), Incoloy™ 901is a nickel-iron-chromium alloy ideally suited for gas turbine and aircraft applications. Because of its high nickel content, it can be joined with ferritic alloy steels without thermal expansion provisions.

CHEMICAL COMPOSITION OF INCOLOY™ 901

• Carbon 0.05
• Manganese 0.48
• Silicon 0.22
• Chromium 12.8
• Molybdenum 5.7
• Titanium 2.4
• Iron 35
• Nickel 43

HEAT TREATMENT OF INCOLOY™ 901

• Anneal by holding at 2050°F (1121°C) for 2 hours before water quenching
• Age by holding at 1375°F (746°C) for 24 hours before air cooling; expect approximately 0.1% contraction

APPLICATIONS OF INCOLOY™ 901

• Gas turbine parts, including rotor and compressor discs, and structural components
• Aircraft applications

MACHINABILITY OF INCOLOY™ 901

• Use high-speed steel tools and cutting fluid
• Cut at 180 sfpm
• Use cobalt high-speed cutting tools with heavy feeds and slow speeds
• Grind high speed steel roughing tools to 8° side and back rake, 4-6° side clearance, 6-8° end clearance, 15-25° side cutting-edge angle, 1/32” nose radius
• 15-35 sfpm surface cutting speeds with 1/16-1/32” deep cuts and 0.010-0.015 in./rev. feed
• Finishing cuts to 35 sfpm; clorinated and sulfurized cutting oils
• Cemented carbide  tools
  • 30 to 60 sfpm
  • 0° to 5° back rake
  • 5° side rake
  • Chemical-active water soluble lubricants or plain soluble oil and water or lubricants.

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.

  .AVAILABLE IN STOCK.

Additional Information:

• Minimum Order Quantity: 10 Kilogram

NIMONIC® alloy 90 (UNS N07090/W. Nr. 2.4632) is a wrought nickel-chromium-cobalt base alloy strengthened by additions of titanium and aluminum. It has been developed as an age-hardenable creepresisting alloy for service at temperatures up to 920°C (1688°F. The alloy is used for turbine blades, discs, forgings, ring sections and hot-working tools.

Composition, %
Carbon........................................................................0.13 max.
Silicon ...........................................................................1.0 max. Copper..........................................................................0.2 max. Iron................................................................................1.5 max.
Manganese ...................................................................1.0 max. Chromium....................................................................18.0-21.0 Titanium...........................................................................2.0-3.0
Aluminum ........................................................................1.0-2.0 Cobalt..........................................................................15.0-21.0
Boron ..........................................................................0.02 max.
Sulfur ........................................................................0.015 max. Lead........................................................................0.0020 max. Zirconium....................................................................0.15 max. Nickel.............................................................................Balance

SIZE 6MM TO 200MM DIA ROUND BAR.

SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.

.AVAILABLE IN STOCK.

Additional Information:

• Minimum Order Quantity: 10 Kilogram

Introduction

Nitronic 50® stainless steel is an austenitic stainless steel with a blend of strength and corrosion resistance that is higher than stainless steel grades 316, 316/316L, 317, and 317/317L .

The high strength, corrosion resistance, and low magnetic permeability of this alloy allows it to be used as a material for medical implants.

The following sections will discuss in detail about stainless steel grade NITRONIC®50 (XM-19).

Chemical Composition

The chemical composition of stainless steel grade NITRONIC® 50 (XM-19) is outlined in the following table.

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.

  .AVAILABLE IN STOCK.

Additional Information:

• Minimum Order Quantity: 10 Kilogram

Applications

Valve stems, fasteners, screens, wear plates and pins

Description

Nitronic 60® is an austenitic stainless steel that has about twice the yield strength of 304 with better corrosion resistance. The alloy has excellent high temperature oxidation resistance. In addition Nitronic® 60 and has outstanding galling resistance.

Chemistry Typical

Carbon: 0.10 max
Manganese: 7.00-9.00
Silicon: 3.5-4.5
Chromium: 16.00-18.00
Nickel: 8.00-9.00
Nitrogen: 0.08-0.18

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.

.AVAILABLE IN STOCK.

Additional Information:

• Minimum Order Quantity: 10 Kg

Alloy steels comprise a wide variety of steels with compositions that exceed the limitations of Si, Va, Cr, Ni, Mo, Mn, B and C allocated for carbon steels. In comparison with carbon steels, alloy steels are more responsive to mechanical and heat treatments.

Alloy steels can be used in specific melting and deoxidization processes for particular applications. These steels have elements such as chromium, cobalt, nickel, etc.

Maraging 300 alloy steel is a very high strength iron base, molybdenum, cobalt and nickel alloy. The following datasheet provides an overview of maraging 300 alloy steel.

Chemical Composition

The chemical composition of maraging 300 alloy steel is outlined in the following table.

Additional Information:

• Minimum Order Quantity: 10 Kilogram

Waspaloy (UNS N07001/W. Nr. 2.4654) is a nickel base, age hardenable superalloy with excellent high temperature strength and good corrosion resistance, notably to oxidation, at service temperatures up to 1200°F (650°C) for critical rotating applications, and up to 1600°F (870°C) for other, less demanding, applications. The alloy’s high-temperature strength is derived from its solid solution strengthening elements, molybdenum, cobalt and chromium, and its agehardening elements, aluminum and titanium. Its strength and stability ranges are higher than those typically available for alloy 718. Special Metals offers Waspaloy made by vacuum induction melting and vacuum arc refining (VIM/VAR) or by vacuum induction melting and electroslag refining (VIM/ESR). The manufacturing process is selected to meet specific customer requirements and final service applications. An even higher strength “super Waspaloy” chemistry is available, a unique composition to provide higher strength properties for more demanding applications. Special Metals Waspaloy is used for gas turbine engine components that call for considerable strength and corrosion resistance at high operating temperatures. Current and potential applications include compressor and rotor discs, shafts, spacers, seals, rings and casings, fasteners and other miscellaneous engine hardware, airframe assemblies and missile systems. The alloy’s oxidation resistance is good under conditions of frequent thermal cycling, and in continuous exposure to temperatures up to 1900°F (1038°C). It has performed well in atmospheres found in gas turbine engine service and in salt spray environments. Solution-treated material offers the best levels of corrosion resistance.

Chemical Compositiona , %
Chromium................................................................18.00-21.00 Boron.........................................................................0.003-0.01
Zirconium ....................................................................0.02-0.12
Aluminum ....................................................................1.20-1.60 Titanium.......................................................................2.75-3.25
Molybdenum ...............................................................3.50-5.00 Cobalt......................................................................12.00-15.00 Copper........................................................................0.50 max. Iron..............................................................................2.00 max.
Sulfur ........................................................................0.030 max.
Silicon ........................................................................0.75 max.
Manganese .................................................................1.00 max.
Carbon ...............................................................0.02-0.10 max.
Phosphorus ..............................................................0.030 max. Nickel............................................................................Balance

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.

  .AVAILABLE IN STOCK.

Additional Information:

• Minimum Order Quantity: 10 Kilogram

17-4 PH® is a martensitic precipitation-hardening stainless steel that provides an outstanding combination of high strength, good corrosion resistance, good mechanical properties at temperatures up to 600°F (316°C), good toughness in both base metal and welds, and shorttime, low-temperature heat treatments that minimize warpage and scaling. This versatile material is widely used in the aerospace, chemical, petrochemical, food processing, paper and general metalworking industries.

COMPOSITION %
Carbon 0.07 max.
Manganese 1.00 max.
Phosphorus 0.040 max.
Sulfur 0.030 max.
Silicon 1.00 max.
Chromium 15.00 - 17.50
Nickel 3.00 - 5.00
Copper 3.00 - 5.00
Columbium plus Tantalum 0.15 - 0.45

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.

.AVAILABLE IN STOCK.

Additional Information:

• Minimum Order Quantity: 10 Kilogram

Alloy 28 (Wst 1.4563)
Technical Data Sheet

Alloy 28 (UNS N08028, W. Nr. 1.4563) is a nickel-iron-chromium alloy with additions of molybdenum and copper. It has excellent resistance to both reducing and oxidizing acids, to stress-corrosion cracking, and to localise attack such as pitting and crevice corrosion. The alloy are especially resistant to sulphuric and phosphoric acid. Used for chemical processing, pollution control equipment, oil and gas well piping, nuclear fuel reprocessing, acid production and pickling equipment.

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.

.AVAILABLE IN STOCK.

Additional Information:

• Minimum Order Quantity: 10 Kilogram

STAINLESS STEEL 422GENERAL CHARACTERISTICS OF STAINLESS 422

With better strength at higher temperatures, Stainless steel 422 is an appealing alternative to Stainless 403. It offers ductility and strength from room temperature to 1200°F (649°C) and resists scaling and oxidation to 1400°F (760°C).

CHEMICAL COMPOSITION OF STAINLESS STEEL 422

• Carbon 0.20-0.25
• Manganese 1.00 max
• Molybdenum 0.75-1.25
• Chromium 12.00-14.00
• Silicon 1.00 max
• Sulfur 0.03 max
• Nickel 0.40-1.00
• Tungsten 0.75-1.25
• Vanadium 0.20-0.50
• Phosphorus 0.04 max
• Iron balance

HEAT TREATMENT OF STAINLESS 422

• To anneal, heat to 1600° to 1650°F (871° to 899°C), then slowly cool in furnace
• For stress relief, heat to 1100° to 1150°F (593° to 621°C) before furnace or air cooling
• Harden by heating to 1875° to 1925°F (1024° to 1052°C) before oil quenching and tempering

APPLICATIONS OF STAINLESS STEEL 422

• Aircraft parts
• Steam and gas turbine components
• High heat components.

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.

  .AVAILABLE IN STOCK.

Additional Information:

• Minimum Order Quantity: 10 Kilogram

NIMONIC® alloy 263 (UNS N07263/W. Nr. 2.4650), an air melted nickel-base alloy, was developed by RollsRoyce (1971) Ltd. to provide a sheet material which could be readily fabricated and would offer improved ductility in welded assemblies to replace NIMONIC alloy 80A. It was designed as sheet material to meet specific design criteria in terms of proof stress and creep strength. It is now available in all standard forms. The welding techniques for this alloy are similar to those in common use for other age-hardenable nickelbase alloys. During salvage welding operations, a preweld heat-treatment is not necessary on age-hardened assemblies but a subsequent age-hardening treatment is desirable after all salvage welding is completed. Material will age in service if temperatures are above 750°C.
Composition, %
Carbon ........................................................................0.04-0.08
Silicon .........................................................................0.40 max.
Manganese .................................................................0.60 max.
Sulfur ........................................................................0.007 max. Silver.......................................................................0.0005 max. Aluminum....................................................................0.60 max.
Boron ........................................................................0.005 max. Bismuth...................................................................0.0001 max. Cobalt..........................................................................19.0-21.0 Chromium....................................................................19.0-21.0 Copper........................................................................0.20 max. Iron................................................................................0.7 max.
Molybdenum ...................................................................5.6-6.1 Lead........................................................................0.0020 max. Titanium...........................................................................1.9-2.4
Aluminum and titanium ...................................................2.4-2.8 Nickel............................................................................Balance*

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.

.AVAILABLE IN STOCK.

Additional Information:

• Minimum Order Quantity: 10 Kilogram

INCOLOY® alloy A-286 (UNS S66286/W. Nr. 1.4980) is an iron-nickel-chromium alloy with additions of molybdenum and titanium. It is agehardenable for high mechanical properties. The alloy maintains good strength and oxidation resistance at temperatures up to about 1300°F (700°C). The limiting chemical composition is given in Table 1. The alloy is austenitic in all metallurgical conditions. The high strength and excellent fabrication characteristics of INCOLOY alloy A-286 make the alloy useful for various components of aircraft and industrial gas turbines. It is also used for fastener applications in automotive engine and manifold components subject to high levels of heat and stress and in the offshore oil and gas industry.

Table 1 - Limiting Chemical Composition, % Nickel.........................................................................24.0-27.0
Iron .............................................................................Balance* Chromium..................................................................13.5-16.0 Titanium.....................................................................1.90-2.35 Molybdenum..................................................................1.0-1.5 Vanadium...................................................................0.10-0.50
Carbon ......................................................................0.08 max.
Manganese .................................................................2.0 max.
Silicon .........................................................................1.0 max. Aluminum..................................................................0.35 max. Sulfur.......................................................................0.030 max. Boron.......................................................................0.001-0.01

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.

.AVAILABLE IN STOCK.

Additional Information:

• Minimum Order Quantity: 10 Kilogram

The INCOLOY® 800 series of alloys, invented by the Special Metals Corporation Group of Companies, is the result of years of monitoring and maintaining the ultimate chemical properties for high-temperature strength and resistance to oxidation, carburization and other types of high-temperature corrosion. Each one a refinement of the one before, these alloys have set the industry standard in hightemperature applications requiring optimum creep and rupture properties. INCOLOY nickel-iron-chromium alloy 800 was introduced to the market in the 1950s to fill the need for a heat- and corrosion-resistant alloy with a relatively low nickel content since nickel was, at the time, designated a “strategic” metal. Over the past forty years it has been widely used for its strength at high temperatures and its ability to resist oxidation, carburization, and other types of high-temperature corrosion. Applications include furnace components and equipment, petrochemical furnace cracker tubes, pigtails and headers, and sheathing for electrical heating elements.

CHEMICAL% 800 800H 800HT
Nickel 30.0-35.0 30.0-35.0 30.0-35.0
Chromium 19.0-23.0 19.0-23.0 19.0-23.0
Iron 39.5 min. 39.5 min. 39.5 min.
Carbon 0.10 max. 0.05-0.10 0.06-0.10
Aluminum 0.15-0.60 0.15-0.60 0.25-0.60
Titanium 0.15-0.60 0.15-0.60 0.25-0.60
Aluminum + Titanium 0.30-1.20 0.30-1.20 0.85-1.20

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.
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Nickel 200 (UNS N02200/W.Nr. 2.4060 & 2.4066) is commercially pure (99.6%) wrought nickel. It has good mechanical properties and excellent resistance to many corrosive environments. Other useful features of the alloy are its magnetic and magnetostrictive properties, high thermal and electrical conductivities, low gas content and low vapor pressure. Chemical composition is shown in Table 1. The corrosion resistance of Nickel 200 makes it particularly useful for maintaining product purity in the handling of foods, synthetic fibers, and caustic alkalies; and also in structural applications where resistance to corrosion is a prime consideration. Other applications include chemical shipping drums, electrical and electronic parts, aerospace and missile components.

Chemical Composition, % 
Nickel (plus cobalt) ......................................................99.0 min. Copper........................................................................0.25 max. Iron..............................................................................0.40 max. 
Manganese .................................................................0.35 max. Carbon........................................................................0.15 max. 
Silicon .........................................................................0.35 max. 
Sulfur ..........................................................................0.01 max.

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.

.AVAILABLE IN STOCK.

Additional Information:

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Nitronic 60 is truly an all purpose metal. This fully austenitic alloy was originally designed as a temperature alloy, and subsequently has good high temperature properties for temperatures around 1800ºF. The oxidation resistance of Nitronic 60 is similar to Type 309 S.S., and far superior to Type 304S.S. This grade is best known for its wear and galling resistance.

The additions of Silicon and Manganese have given this alloy a matrix to inhibit wear, galling, and fretting even in the annealed condition. Higher strengths are attainable through cold working the material and is still fully austenitic after severe cold-working. This working does not enhance the anti-galling properties as is normal for carbon steels and some stainless steels. The benefit to the cold or hot work put into the material is added strength and hardness, and the wear resistance does not decrease noticeably. Chromium and Nickel additions give it comparable corrosion to 304 and 316 stainless steels, while having approximately twice the yield strength. The high mechanical strength in annealed parts permits use of reduced cross sections for weight, and cost reductions through the use of thinner stock.

Alloy Composition

Iron (Fe)59.1 to 65.4 %

Chromium (Cr)16 to 18 %

Nickel (Ni)8.0 to 9.0 %

Manganese (Mn)7.0 to 9.0 %

Silicon (Si)3.5 to 4.5 %

Nitrogen (N)0.080 to 0.18 %

Carbon (C)0 to 0.1 %

Phosphorus (P)0 to 0.060 %

Sulfur (S)0 to 0.030 %

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NIMONIC® alloy 263 (UNS N07263/W. Nr. 2.4650), an air melted nickel-base alloy, was developed by RollsRoyce (1971) Ltd. to provide a sheet material which could be readily fabricated and would offer improved ductility in welded assemblies to replace NIMONIC alloy 80A. It was designed as sheet material to meet specific design criteria in terms of proof stress and creep strength. It is now available in all standard forms. The welding techniques for this alloy are similar to those in common use for other age-hardenable nickelbase alloys. During salvage welding operations, a preweld heat-treatment is not necessary on age-hardened assemblies but a subsequent age-hardening treatment is desirable after all salvage welding is completed. Material will age in service if temperatures are above 750°C.

Composition, %
Carbon ........................................................................0.04-0.08
Silicon .........................................................................0.40 max.
Manganese .................................................................0.60 max.
Sulfur ........................................................................0.007 max. Silver.......................................................................0.0005 max. Aluminum....................................................................0.60 max.
Boron ........................................................................0.005 max. Bismuth...................................................................0.0001 max. Cobalt..........................................................................19.0-21.0 Chromium....................................................................19.0-21.0 Copper........................................................................0.20 max. Iron................................................................................0.7 max.
Molybdenum ...................................................................5.6-6.1 Lead........................................................................0.0020 max. Titanium...........................................................................1.9-2.4
Aluminum and titanium ...................................................2.4-2.8 Nickel............................................................................Balance*

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NIMONIC® alloy 75 (UNS N06075/W.Nr. 2.4951 & 2.4630) is an 80/20 nickel-chromium alloy with controlled additions of titanium and carbon. First introduced in the 1940s for turbine blades in the prototype Whittle jet engines, it is now mostly used for sheet applications calling for oxidation and scaling resistance coupled with medium strength at high operating temperatures. It is still used in gas turbine engineering and also for industrial thermal processing, furnace components and heat-treatment equipment. It is readily fabricated and welded. Some physical properties for NIMONIC alloy 75 are given in Tables 2-4. Thermal expansion data in Table 3 were determined on fully heat-treated material. The data are subject to a variation of approximately ±5% according to processing variables. The dynamic modulus data in Table 4 were obtained from fully heattreated cylindrical specimens vibrated in the flexural mode. The recommended heat treatments are quoted in the Heat Treatment section of this bulletin. Physical Properties Table 1 - Limiting
Chemical Composition, % (as in BS HR 203)
Carbon ........................................................................0.08-0.15 Chromium....................................................................18.0-21.0 Copper..........................................................................0.5 max. Iron................................................................................5.0 max.
Manganese ...................................................................1.0 max.
Silicon ...........................................................................1.0 max. Titanium...........................................................................0.2-0.6 Nickel............................................................................Balance*

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Nickel 200 and Nickel 201 are solid solution strengthened, commercially pure wrought materials. Typically, the elemental restrictions of both alloys are combined into one, dual-certified chemistry resulting in a single alloy with the desired characteristics of both alloys. Applications where Nickel 200/201 can be used include chemical processing and storage, synthetic fiber production, and processes where sodium hydroxide and fluorine is used. Other applications include aerospace and defense as well as food processing. Nickel 200/201 has exceptional resistance to caustic alkalies at various temperatures and concentrations.

Chemical Composition %
Ni .............99.0 Min. 
Si ................0.35 Max. 
Fe ..............0.40 Max. 
Cu ..............0.25 Max. 
C ...............0.15 Max. 
S .................0.01 Max. 
Mn.............0.35 Max. 

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Applications

Superior resistance to hydrochloric acid, aluminum chloride catalysts and other strongly reducing chemicals. Excellent high-temperature strength in inert and vacuum atmospheres.

Hastelloy B2 is a nickel-molybdenum alloy particularly suited for equipment handling reducing chemical environments .

Applications in the chemical process industry involving sulfuric, phosphoric, hydrochloric and acetic acid. Temperature uses vary from ambient temperature to 1500°F depending on the environments (please call for technical advice).

 

Chemistry

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• Excellent corrosion resistance in reducing environments
• Exceptional resistance to strong solutions of oxidizing salts, such as ferric and cupric chlorides
• High nickel and molybdenum contents providing good corrosion resistance in reducing environments
• Low carbon content which minimizes grain-boundary carbide precipitation during welding to maintain resistance to corrosion in heat-affected zones of welded joints
• Resistance to localized corrosion such as pitting and stress-corrosion cracking
• One of few materials to withstand the corrosive effects of wet chlorine gas, hypochlorite and chlorine dioxide

Chemical Composition, %

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MONEL® alloy K-500 (UNS N05500/ W.Nr. 2.4375) is a nickel-copper alloy which combines the excellent corrosion resistance of MONEL alloy 400 with the added advantages of greater strength and hardness. The increased properties are obtained by adding aluminum and titanium to the nickel-copper base, and by heating under controlled conditions so that submicroscopic particles of Ni3 (Ti, Al) are precipitated throughout the matrix. The thermal processing used to effect precipitation is commonly called age hardening or aging. The composition of the alloy is given in Table 1. Typical applications for MONEL alloy K-500 products are chains and cables, fasteners and springs for marine service; pump and valve components for chemical processing; doctor blades and scrapers for pulp processing in paper production; oil well drill collars and instruments, pump shafts and impellers, non-magnetic housings, safety lifts and valves for oil and gas production; and sensors and other electronic components.

Table 1 - Limiting Chemical Composition, %, of MONEL Alloy K-500
Nickel (plus Cobalt) .....................................................63.0 min. Carbon........................................................................0.25 max.
Manganese ...................................................................1.5 max. Iron................................................................................2.0 max.
Sulfur ..........................................................................0.01 max.
Silicon ...........................................................................0.5 max.
Copper ......................................................................27.0 - 33.0
Aluminum ..................................................................2.30 - 3.15
Titanium ....................................................................0.35 - 0.85

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NIMONIC® alloy 90 (UNS N07090/W. Nr. 2.4632) is a wrought nickel-chromium-cobalt base alloy strengthened by additions of titanium and aluminum. It has been developed as an age-hardenable creepresisting alloy for service at temperatures up to 920°C (1688°F. The alloy is used for turbine blades, discs, forgings, ring sections and hot-working tools.

Composition, %
Carbon........................................................................0.13 max.
Silicon ...........................................................................1.0 max. Copper..........................................................................0.2 max. Iron................................................................................1.5 max.
Manganese ...................................................................1.0 max. Chromium....................................................................18.0-21.0 Titanium...........................................................................2.0-3.0
Aluminum ........................................................................1.0-2.0 Cobalt..........................................................................15.0-21.0
Boron ..........................................................................0.02 max.
Sulfur ........................................................................0.015 max. Lead........................................................................0.0020 max. Zirconium....................................................................0.15 max.
Nickel.............................................................................Balance

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Nitronic 50® stainless steel is an austenitic stainless steel with a blend of strength and corrosion resistance that is higher than stainless steel grades 316, 316/316L, 317, and 317/317L .

The high strength, corrosion resistance, and low magnetic permeability of this alloy allows it to be used as a material for medical implants.

The following sections will discuss in detail about stainless steel grade NITRONIC®50 (XM-19).

Chemical Composition

The chemical composition of stainless steel grade NITRONIC® 50 (XM-19) is outlined in the following table.

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NIMONIC® alloy 80A (UNS N07080/W. Nr. 2.4952 & 2.4631) is a wrought, age-hardenable nickel-chromium alloy, strengthened by additions of titanium, aluminum and carbon, developed for service at temperatures up to 815°C (1500°F). It is produced by high-frequency melting and casting in air for forms to be extruded. Electroslag refined material is used for forms to be forged. Vacuum refined versions are also available. NIMONIC alloy 80A is currently used for gas turbine components (blades, rings and discs), bolts, nuclear boiler tube supports, die casting.

Chemical Composition, % by Weight
Carbon........................................................................0.10 max. Chromium....................................................................18.0-21.0
Silicon ............................................................................1.0 max Copper..........................................................................0.2 max. Iron................................................................................3.0 max.
Manganese ...................................................................1.0 max. Titanium...........................................................................1.8-2.7
Aluminum ........................................................................1.0-1.8
Cobalt ...........................................................................2.0 max.
Boron ........................................................................0.008 max. Zirconium....................................................................0.15 max. Lead........................................................................0.0025 max.
Sulfur ........................................................................0.015 max. Nickel............................................................................Balance*

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MONEL® nickel-copper alloy 400 (UNS N04400/ W.Nr. 2.4360 and 2.4361) is a solid-solution alloy that can be hardened only by cold working. It has high strength and toughness over a wide temperature range and excellent resistance to many corrosive environments. Composition is shown in Table 1. Alloy 400 is widely used in many fields, especially marine and chemical processing. Typical applications are valves and pumps; pump and propeller shafts; marine fixtures and fasteners; electrical and electronic components; springs; chemical processing equipment; gasoline and fresh water tanks; crude petroleum stills, process vessels and piping; boiler feedwater heaters and other heat exchangers; and deaerating heaters.

Chemical Composition, %, of MONEL Alloy 400
Nickel (plus Cobalt) .....................................................63.0 min. Carbon..........................................................................0.3 max.
Manganese ...................................................................2.0 max. Iron................................................................................2.5 max.
Sulfur ........................................................................0.024 max.
Silicon ...........................................................................0.5 max.
Copper ......................................................................28.0 - 34.0

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Product Details:

INCONEL® nickel-chromium-iron alloy 601 (UNS N06601/W.Nr. 2.4851) is a general-purpose engineering material for applications that require resistance to heat and corrosion. An outstanding characteristic of INCONEL alloy 601 is its resistance to high temperature oxidation. The alloy also has good resistance to aqueous corrosion, has high mechanical strength, and is readily formed, machined and welded. The limiting chemical composition of INCONEL alloy 601 is listed in Table 1. The composition is a facecentered-cubic solid solution with a high degree of metallurgical stability. The alloy's nickel base, in conjunction with substantial chromium content, provides resistance to many corrosive media and high temperature environments. Oxidation resistance is further enhanced by the aluminum content.

CHEMICAL %
Nickel ..........................................................................58.0-63.0 Chromium....................................................................21.0-25.0
Iron ............................................................................Remainder
Aluminum ........................................................................1.0-1.7 Carbon........................................................................0.10 max.
Manganese ...................................................................1.0 max.
Sulfur ........................................................................0.015 max.
Silicon .........................................................................0.50 max. Copper..........................................................................1.0 max.

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INCOLOY® alloy 945 (UNS N09945) is a high-strength, corrosion-resistant alloy designed for demanding applications in the oil and gas industry. The properties of this age hardenable nickel-iron-chromium alloy are enhanced by its contents of molybdenum, copper, niobium, titanium, and aluminum. The chemical composition of alloy 945 is seen in Table 1. The alloy’s nickel content results in resistance to chlorideinduced stress corrosion cracking. Nickel, in conjunction with the molybdenum and copper, also gives alloy 945 outstanding resistance to general corrosion in reducing media. Molybdenum also imparts resistance to localized attack (pitting and crevice corrosion). The alloy’s content of chromium provides resistance in oxidizing environments. Niobium, titanium and aluminum participate in the age hardening reaction that occurs during heat treatment. Their interaction forms gamma prime and gamma double prime precipitates, which strengthen the alloy. INCOLOY alloy 945 is suitable for downhole oil and gas applications requiring high strength and corrosion resistance in aggressive sour wells containing high levels of hydrogen sulfide and chorides. Because of the alloy’s resistance to stress cracking in environments rich in hydrogen sulfide, it is suitable for downhole and surface gas-well components including tubular products, valves, hangers, landing nipples, tool joints and packers. The alloy can also be used for fasteners, pump shafting and high strength piping systems.

Chemical Composition of INCOLOY alloy 945, wt %

Nickel ......…………………………………..…..45.0-55.0

Chromium ..…………………………………….19.5-23.0

Iron ……………….………………………………Balance

Molybdenum …….………………………………..3.0-4.0

Niobium .…………………………………………..2.5-4.5

Copper …………………………………………….1.5-3.0

Titanium ….………………………………………..0.5-2.5

Aluminum ….…………………………………….0.01-0.7

Manganese ...……………………………………1.0 max.

Silicon …..………………………………………..0.5 max.

Sulfur …..……………………………………….0.03 max.

Phosphorous .………………………………….0.03 max.

Carbon …..…………………………………0.005 to 0.04

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INCONEL® nickel-chromium alloy 625 (UNS N06625/W.Nr. 2.4856) is used for its high strength, excellent fabricability (including joining), and outstanding corrosion resistance. Service temperatures range from cryogenic to 1800°F (982°C). . The properties of INCONEL alloy 625 that make it an excellent choice for sea-water applications are freedom from local attack (pitting and crevice corrosion), high corrosion-fatigue strength, high tensile strength, and resistance to chloride-ion stress-corrosion cracking. It is used as wire rope for mooring cables, propeller blades for motor patrol gunboats, submarine auxiliary propulsion motors, submarine quickdisconnect fittings, exhaust ducts for Navy utility boats, sheathing for undersea communication cables, submarine transducer controls, and steam-line bellows. Potential applications are springs, seals, bellows for submerged controls, electrical cable connectors, fasteners, flexure devices, and oceanographic instrument components.

Table 1 – Limiting Chemical Composition, %
Nickel…………………………………………….…………58.0 min.
Chromium………………………………………..…………20.0-23.0
Iron………………………………………………..………….5.0 max.
Molybdenum……………………………….……...…………8.0-10.0
Niobium (plus Tantalum)………………………..………….3.15-4.15
Carbon……………………………………………..……….0.10 max.
Manganese………………………………………....……….0.50 max.
Silicon……………………………….…………...…………0.50 max.
Phosphorus……………………………………….………..0.015 max.
Sulfur…………………………………..……….…..……..0.015 max.
Aluminum…………………………………………………..0.40 max.
Titanium……………………………….……………………0.40 max.
Cobalta ……………………………………………………….1.0 max

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INCONEL® (nickel-chromium-iron) alloy 600 (UNS N06600/W.Nr. 2.4816) is a standard engineering material for applications which require resistance to corrosion and heat. The alloy also has excellent mechanical properties and presents the desirable combination of high strength and good workability. The limiting chemical composition of INCONEL alloy 600 is shown in Table 1. The high nickel content gives the alloy resistance to corrosion by many organic and inorganic compounds and also makes it virtually immune to chloride-ion stress-corrosion cracking. Chromium confers resistance to sulfur compounds and also provides resistance to oxidizing conditions at high temperatures or in corrosive solutions. The alloy is not precipitation hardenable; it is hardened and strengthened only by cold work. The versatility of INCONEL alloy 600 has led to its use in a variety of applications involving temperatures from cryogenic to above 2000°F (1095°C).

Table 1 - Limiting Chemical Composition, %
Nickel (plus Cobalt)....................................................72.0 min. Chromium..................................................................14.0-17.0
Iron ..........................................................................6.00-10.00
Carbon ......................................................................0.15 max.
Manganese ................................................................1.00 max Sulfur.......................................................................0.015 max.
Silicon .......................................................................0.50 max. Copper......................................................................0.50 max

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Chemical Composition Alloy 800 (UNS N08800) Chemical Composition, %

The chemical composition of Alloy 800 is:

Alloy 800H (UNS N08810) Chemical Composition, %

The chemical composition of alloy 800H is:

Alloy 800HT (UNS N08811) Chemical Composition, %

The chemical composition of Alloy 800HT is :

Forms of INCOLOY 800H/800HT

The forms of INCOLOY 800H/800HT are:

• Sheet
• Plate
• Bar
• Pipe & Tube (welded & seamless)
• Fittings (i.e., flanges, slip-ons, blinds, weld-necks, lap joints, long welding necks, socket welds, elbows, tees, stub-ends, returns, caps, crosses, reducers, and pipe nipples)
• Wire.

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Chemical Composition Alloy 800 (UNS N08800) Chemical Composition, %

The chemical composition of Alloy 800 is:

Alloy 800H (UNS N08810) Chemical Composition, %

The chemical composition of alloy 800H is:

Alloy 800HT (UNS N08811) Chemical Composition, %

The chemical composition of Alloy 800HT is :

Forms of INCOLOY 800H/800HT

The forms of INCOLOY 800H/800HT are:

• Sheet
• Plate
• Bar
• Pipe & Tube (welded & seamless)
• Fittings (i.e., flanges, slip-ons, blinds, weld-necks, lap joints, long welding necks, socket welds, elbows, tees, stub-ends, returns, caps, crosses, reducers, and pipe nipples)
• Wire.

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HASTELLOY Alloy C-22 is a nickel-chromium-molybdenum alloy with enhanced resistance to pitting, crevice corrosion and stress corrosion cracking. It resists the formation of grain boundary precipitates in the weld-heat affected zone making it suitable for use in the as-welded condition. C-22 has outstanding resistance to both reducing and oxidizing media and because of its resistibility can be used where "upset" conditions are likely to occur. It is proven to possess excellent weldability and high corrosion resistance as consumable filler wires and electrodes. The alloy has proven results as a filler wire in many applications. As filler wire use when other corrosion resistant wires have failed. C-22 can easily be cold-worked because of its ductility and cold-forming is the preferred method of forming. More energy is required because the alloy is generally stiffer than austenitic stainless steels. 0.28" thick sheet in the heat-treated at 2050F, rapid quenched condition, has an average olsen cup depth of 0.49". Specifications UNS Bar ASTM B574 Wire Sheet ASTM B575 Plate ASTM B575 Fitting ASME SB-366 Forging ASME SB-564 Weld Wire Weld Electrode Chemistry Chemical Requirements Ni Cr Mn C Mo Si Fe Max Bal. 22.5 0.50 0.015 14.5 0.08 6.0 Min 20.0 12.5 2.0 SIZE 6MM TO 200MM DIA ROUND BAR. SIZE 1MM TO 100MM THICKNESS PLATE. SIZE 6MM TO 350MM OD PIPE . SIZE 0.5MM TO 6MM DIA WIRE. .AVAILABLE IN STOCK.

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INCOLOY® alloy 825 (UNS N08825/W.Nr. 2.4858) is a nickel-iron-chromium alloy with additions of molybdenum, copper, and titanium. The alloy’s chemical composition, given in Table 1, is designed to provide exceptional resistance to many corrosive environments. The nickel content is sufficient for resistance to chloride-ion stress-corrosion cracking. The nickel, in conjunction with the molybdenum and copper, also gives outstanding resistance to reducing environments such as those containing sulfuric and phosphoric acids. The molybdenum also aids resistance to pitting and crevice corrosion. The alloy’s chromium content confers resistance to a variety of oxidizing substances such as nitric acid, nitrates and oxidizing salt. The titanium addition serves, with an appropriate heat treatment, to stabilize the alloy against sensitization to intergranular corrosion. The resistance of INCOLOY alloy 825 to general and localized corrosion under diverse conditions gives the alloy broad usefulness. Applications include chemical processing, pollution control, oil and gas recovery, acid production, pickling operations, nuclear fuel reprocessing, and handling of radioactive wastes. Applications for alloy 825 are similar to those for INCOLOY alloy 020. Table 1 - Limiting Chemical Composition, % of

INCOLOY alloy 825
Nickel ..........................................................................38.0-46.0 Iron...............................................................................22.0 min. Chromium....................................................................19.5-23.5
Molybdenum ...................................................................2.5-3.5
Copper ............................................................................1.5-3.0 Titanium...........................................................................0.6-1.2 Carbon........................................................................0.05 max.
Manganese ...................................................................1.0 max.
Sulfur ..........................................................................0.03 max.
Silicon ...........................................................................0.5 max. Aluminum......................................................................0.2 max

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