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High nickel alloys, also known as nickel-based superalloys, are a family of materials renowned for their exceptional combination of strength, corrosion resistance, and high-temperature performance. Typically composed predominantly of nickel, with significant additions of other elements such as chromium, iron, cobalt, and molybdenum, these alloys exhibit remarkable properties that make them indispensable in demanding applications across various industries. High nickel alloys find widespread use in aerospace, chemical processing, marine engineering, and power generation, where they endure harsh conditions including high temperatures, corrosive environments, and mechanical stress. These alloys are known for their excellent resistance to oxidation, corrosion, and creep at elevated temperatures, making them ideal for critical components such as turbine blades, exhaust systems, chemical reactors, and heat exchangers. With their exceptional properties and versatility, high nickel alloys continue to push the boundaries of material performance and innovation in modern engineering.

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Manufacturing process of Plate

There are many variations you need to.

  • Raw Materials
  • Ironmaking
  • Steelmaking
  • Casting
  • Hot Rolling
  • Cooling and Conditioning
  • Finishing

Throughout the manufacturing process, quality control measures are implemented to ensure that the steel bars meet the required specifications for composition, mechanical properties, and surface finish. This involves regular testing and inspection of the raw materials, intermediate products, and finished bars to ensure consistency and quality.

Bars Manufacturing

Specifications of Other Plates

Dimensions ASTM, ASME and API
Standard ASTM A240 / ASME SA240
Width 1000mm, 1219mm, 1500mm, 1800mm, 2000mm, 2500mm, 3000mm, 3500mm,
Thickness 0.3mm to 240mm
Length 2000mm, 2440mm, 3000mm, 5800mm, 6000mm,
Form Coils, Foils, Rolls, Plain Sheet, Shim Sheet, Perforated Sheet, Chequered Plate, Strip, Flats, Blank (Circle), Ring (Flange) etc.
Surface Finish 2B, 2D, BA, NO.1, NO.4, NO.8, 8K, mirror, chequered, embossed, hairline, sand blast, Brush, etching, Hot rolled plate (HR), Cold rolled sheet (CR), SATIN (Met with Plastic Coated) etc
Hardness Soft, Hard, Half Hard, Quarter Hard, Spring Hard etc

Inconel Chemical Composition

Grade C Mn Si S Cu Fe Ni Cr
Inconel 600 0.15 max 1.00 max 0.50 max 0.015max 0.50 max 6.00 – 10.00 72.00 min 14.00 – 17.00
Inconel 601 0.10 max 1.00 max 0.50 max 0.015max 1.00 max Balance 58.0 – 63.0 21.0 – 25.0
Inconel 625 0.10 max 0.50 max 0.50 max 0.015max 5.0 max 58.0 min 20.0 – 23.0
Inconel 718 0.08 max 0.35 max 0.35 max 0.015max 0.30 max 50.00 – 55.00 17.00 – 21.00
Grade C Mn Si S Cu Fe Ni Cr Al Ti
800 0.10 max 1.50 max 1.00 max 0.015 max 0.75 max 39.50 min 30.00 – 35.00 19.00 – 23.00 0.15 – 0.60 0.15 – 0.60
800H 0.05 – 0.10 1.50 max 1.00 max 0.015 max 0.75 max 39.50 min 30.00 – 35.00 19.00 – 23.00 0.15 – 0.60 0.15 – 0.60
800HT 0.06 – 0.10 1.50 max 1.00 max 0.015 max 0.75 max 39.50 min 30.00 – 35.00 19.00 – 23.00 0.15 – 0.60ᴬ 0.15 – 0.60ᴬ
825 0.05 max 1.00 max 0.5 max 0.03 max 1.50 – 3.00 22.00 min 38.00 – 46.00 19.50 – 23.50 0.02 max 0.06 – 1.20
Grade Ni Cr Fe Si Mo Cu Mn C S Al
Incoloy 925 42 – 46 19.55 – 22.5 22 min 0.5 max 2.5 – 3.5 1.5 – 3.0 1.0 max 0.03 max 0.03 max 0.1 – 0.5
Grade C Mn Si S Cu Fe Ni Cr Sn Pb
330 0.08 max 2.00 max 0.75-1.50 0.03 max 1.00 max Balance 34.0-37.0 17.0-20.0 0.025 0.005 max

Inconel Mechanical Properties

Element Density Melting Point Tensile Strength Yield Strength (0.2%Offset) Elongation
Inconel 600 8.47 g/cm3 1413 °C (2580 °F) Psi – 95,000 , MPa – 655 Psi – 45,000 , MPa – 310 40 %
Inconel 601 8.1 g/cm3 1411 °C (2571 °F) Psi – 80,000 , MPa – 550 Psi – 30,000 , MPa – 205 30 %
Inconel 625 8.4 g/cm3 1350 °C (2460 °F) Psi – 1,35,000 , MPa – 930 Psi – 75,000 , MPa – 517 42.5 %
Inconel 718 8.2 g/cm3 1350 °C (2460 °F) Psi – 1,35,000 , MPa – 930 Psi – 75,000 , MPa – 482 45 %
800 / 800H / 800HT 7.94 g/cm3 1385 °C (2525 °F) Psi – 75,000 , MPa – 520 Psi – 30,000 , MPa – 205 30 %
825 8.14 g/cm3 1400 °C (2550 °F) Psi – 80,000 , MPa – 550 Psi – 32,000 , MPa – 220 30 %
925 8.14 g/cm3 1343°C 650 300 30 %

Monel Chemical Composition

Grade C Mn Si S Cu Fe Ni
Monel 400 0.30 max 2.00 max 0.50 max 0.024 max 28.00 – 34.00 2.50 max 63.00 min
Monel K500 0.25 max 1.5 max 0.5 max 0.010 max 27.00 – 33.00 0.5 – 2 63.00 min

Monel Mechanical Properties

Element Density Melting Point Tensile Strength Yield Strength (0.2%Offset) Elongation
Monel 400 8.8 g/cm3 1350 °C (2460 °F) Psi – 80,000 , MPa – 550 Psi – 35,000 , MPa – 240 40 %
Monel K500 8.44 g/cm3 1350 °C (2460 °F) Psi – 160000 , MPa – 1100 Psi – 115000 , MPa – 790 20 %

Hastelloy Chemical Composition

Grade C Mn Si S Co Ni Cr Fe Mo P
C22 0.010 max 0.50 max 0.08 max 0.02 max 2.50 max 50.015 min* 20.00 – 22.50 2.00 – 6.00 12.50 – 14.50 0.02 max
C276 0.010 max 1.00 max 0.08 max 0.03 max 2.50 max 50.99 min* 14.50 – 16.50 4.00 – 7.00 15.00 – 17.00 0.04 max
B2 0.010 max 1.00 max 0.08 max 0.03 max 2.50 max 50.99 min* 14.50 – 16.50 4.00 – 7.00 15.00 – 17.00 0.04 max
Grade Ni Mo Cr Fe W Mn C Al Ti Si
Hastelloy B3 65.0 min 28.5 1.5 1.5 3.0 max 3.0 max 0.01 max 0.50 max 0.2 max 10 max
Grade Ni Mo Cr Fe Mn C Co Si P S
Hastelloy X Balance 8.00 – 10.00 20.50 – 23.00 17.00 – 20.00 1.00 max 0.05 – 0.15 0.50 – 2.50 1.00 max 0.04 max 0.03 max

Hastelloy Mechanical Properties

Element Density Melting Point Tensile Strength Yield Strength (0.2%Offset) Elongation
Hastelloy C22 8.69 g/cm3 1399 °C (2550 °F) Psi – 1,00,000 , MPa – 690 Psi – 45000 , MPa – 310 45 %
Hastelloy C276 8.89 g/cm3 1370 °C (2500 °F) Psi – 1,15,000 , MPa – 790 Psi – 52,000 , MPa – 355 40 %
Hastelloy B2 8.89 g/cm3 1370 °C (2500 °F) Psi – 1,15,000 , MPa – 790 Psi – 52,000 , MPa – 355 40 %
Hastelloy B3 9.2 g/cm3 1370 °C (2550 °F) Psi – 1,15,000 , MPa –760 Psi – 52,000 , MPa – 350 40%
Hastelloy X 8.22 g/cm³ 1355°C 655 MPa 240 MPa 35%

Nickel Chemical Composition

Grade C Mn Si S Cu Fe Ni
Nickel 200 0.15 max 0.35 max 0.35 max 0.01 max 0.25 max 0.40 max 99.0 min
Nickel 201 0.02 max 0.35 max 0.35 max 0.01 max 0.25 max 0.40 max 99.0 min

Nickel Mechanical Properties

Element Density Melting Point Tensile Strength Yield Strength (0.2%Offset) Elongation
Nickel 200 8.9 g/cm3 1446 °C (2635 °F) Psi – 67000 , MPa – 462 Psi – 21500 , MPa – 148 45 %
Nickel 201 8.9 g/cm3 1446 °C (2635 °F) Psi – 67000 , MPa – 462 Psi – 21500 , MPa – 148 45 %

Copper Nickel Chemical Composition

Grade Cu Mn Pb Ni Fe Zn
Cupro Nickel 90/10 88.6 min 1.0 max 0.05 max 9-11 max 1.8 max 1 max
Cupro Nickel 70/30 65 min 1.0 max 0.05 max 29-33 max 0.4-1.0 max 1 max

Copper Nickel Mechanical Properties

Density Melting Point Tensile Strength Yield Strength (0.2%Offset) Elongation
0.323 lb/in3 at 68 F 2260 F 50000 psi 20000 psi 30 %
0.323 lb/in3 at 68 F 2260 F 50000 psi 20000 psi 30 %

Duplex Steel Chemical Composition

Grade C Mn Si P S Cr Mo Ni N Fe
S31803 0.030 max 2.00 max 1.00 max 0.030 max 0.020 max 22.0 – 23.0 3.0 – 3.5 4.50 – 6.50 0.14 – 0.20 63.72 min
S32205 0.030 max 2.00 max 1.00 max 0.030 max 0.020 max 21.0 – 23.0 2.50 – 3.50 4.50 – 6.50 0.8 – 0.20 63.54 min

Duplex Steel Mechanical Properties

Grades Density (g/cm 3) Density (lb/in 3) Melting Point (°C) Melting Point (°F)
S31803 / S32205 7.805 0.285 1420 – 1465 2588 – 2669

Super Duplex Chemical Composition

Grade C Mn Si P S Cr Mo Ni N Fe
S32750 0.030 max 1.20 max 0.80 max 0.035 max 0.020 max 24.00 – 26.00 3.00 – 5.00 6.00 – 8.00 0.24 – 0.32 58.095 min
S32760 0.05 max 1.00 max 1.00 max 0.030 max 0.010 max 24.00 – 26.00 3.00 – 4.00 6.00 – 8.00 0.20 – 0.30 57.61 min

Super Duplex Mechanical Properties

Grades Density (g/cm 3) Density (lb/in 3) Melting Point (°C) Melting Point (°F)
S32750 / S32760 7.8 0.281 1350 2460

Titanium Mechanical Properties

Density Melting Point Yield Strength (0.2%Offset) Tensile Strength Elongation
4.5 G/Cm3 1665 °C (3030 °F) Psi – 39900 , MPa – 275 Psi – 49900 , MPa – 344 20 %
4.43 G/Cm3 1632 °C (2970 °F) Psi – 128000 , MPa – 880 Psi – 138000 , MPa – 950 14 %

Titanium Chemical Composition

Grade C N O H Ti Fe
Titanium Grade 1 .08 Max .03 Max .18 Max .015 Max Bal .20 Max
Titanium Grade 4 .08 Max .05 Max .40 Max .015 Max Bal .50 Max
Titanium Grade 7 .08 Max .03 Max .25 Max .015 Max Bal .30 Max
Titanium Grade 9 .08 Max .03 Max .15 Max .015 Max .25 Max
Titanium Grade 12 .08 Max .03 Max .25 Max 0.15 Max .30 Max

Tantalum Chemical Composition

Element R05200
(%,Max)
R05400
(%,Max)
R05255
(Ta10W) / (%,Max)
R05252
(Ta2.5W) / (%,Max)
R05240
(Ta-40Nb) / (%,Max)
C 0.01 0.01 0.01 0.01 0.01
O 0.015 0.03 0.015 0.015 0.02
N 0.01 0.01 0.01 0.01 0.01
H 0.0015 0.0015 0.0015 0.0015 0.0015
Fe 0.01 0.01 0.01 0.01 0.01
Mo 0.02 0.02 0.02 0.02 0.02
Nb 0.1 0.1 0.1 0.5 35.0-42.0
Ni 0.01 0.01 0.01 0.01 0.01
Si 0.005 0.005 0.005 0.005 0.005
Ti 0.01 0.01 0.01 0.01 0.01
W 0.05 0.05 9.0-11.0 2.0-3.5 0.05

Tantalum Mechanical Properties

Grade Tensile strength δbpsi (MPa), ≥ Yield strength δ0.2, psi (MPa),≥  Elongation in 1″/2″ gage length, %, ≥
R05200/R05400 30000 (207) 20000 (138) 25
 R05252 40000 (276) 28000 (193)  20
 R05255 70000 (481) 60000 (414) 15
 R05240 40000 (276)  28000 (193) 20

Copper Chemical Composition

Copper Pipe (Incl. Silver) 99.85% Min.
Phosphorus 0.013 to 0.5%
Total Impurities 0.06% Max.

Copper Mechanical Properties

Density 8.89 g/cm3
Melting Point 1370 °C (2500 °F)
Tensile Strength Psi – 1,15,000 , MPa – 790
Yield Strength (0.2%Offset) Psi – 52,000 , MPa – 355
Elongation 40 %

Beryllium Copper Chemical Composition

Grade Be Co+Ni Co+Ni+Fe Cu
C17200 1.85-2.10% 0.20% Min. 0.60% Max. Balance

Beryllium Copper Mechanical Properties

Grade Density (g/cm3) Density before age hardening (g/cm3) Elastic Modulus (kg/mm2 (103)) Thermal Expansion Coefficient (20 °C to 200 °C m/m/°C) Thermal Conductivity (cal/(cm-s-°C)) Melting Range (°C)
C17200 8.36 8.25 13.40 17 x 10-6 0.25 870-980

Chromium Sheet Specifications

Material Chromium
Purity 99.8%, 99.95%, 99.98%, 99.99% 
Density 7.18 g/cm3
Melting Point 1857℃
Boiling Point 2672℃
Shape Sheet

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