Hastelloy Plates

AMS-5840, is typically used as a filler metal for gas tungsten arc & gas metal arc welding of steel of similar composition requiring joints with strength & corrosion resistance comparable to those of the base metal.

Chemical Composition

• Carbon; 0.050max
• Phosphorous; 0.0080max
• Manganese; 0.10max
• Silicon; 0.10max
• Sulfur; 0.010max
• Chromium; 12.9
• Hydrogen; 0.0025max
• Molybdenum; 2.25
• Nitrogen; 0.010max
• Oxygen; 0.0050max
• Aluminium; 1.10
• Nickel; 8.0max
• Iron; 76

AMS-5546 Sheet/Strip is a columbium/tantalum stabilised austenitic chromium nickel stainless steel. This material is stabilised against formation by the addition of columbium & tantalum. Its applications are furnace heating elements, cabin heaters, aircraft exhaust & heavy wall welded equipment.

Chemical Composition

• Carbon; 0.08max
• Manganese; 2.00max
• Phosphorus; 0.045max
• Sulfur; 0.030max
• Silicon; 0.75max
• Chromium; 17.0-19.0
• Nickel; 9.0-13.0
• Columbium+Tantalum; 10xCmin to 1.00max
• Iron; Bal

Mechanical Properties

• 0.2% Yield Strength Offset; 30,000psi, 205Mpa
• Tensile Strength; 75,000psi, 515Mpa
• Elongation in 2" ; 40%

AMS 5604 Sheet/ Plate/ Strip
AMS 5604, is a martensitic, precipitation hardening stainless steel that provides an outstanding combination of high strength & hardness along with excellent corrosion resistance. It is a versatile material widely used in the paper & pulp, aerospace, chemical, petrochemical, food processing industries.

AMS 5604 Chemical Composition
Carbon; 0.07max
Silicon; 1.00max
Manganese; 1.00max
Phosphorus; 0.040max
Sulfur; 0.030max
Chromium; 15.0-17.5
Nickel; 3.0-5.0
Cb+Ta; 5XC/0.45
Copper; 3.0-5.0

AMS 5604 Mechanical Properties
Tensile Strength; 190ksi
0.2% Yield Strength; 170ksi
Rockwell C Hardness; 40-47

AMS 5549, is a chromium nickel molybdenum stainless steel. It is a heat treatable austenitic alloy. It is used for industrial cutters, blades, discs, rotors, shafts, knives etc.

Chemical Composition

• Carbon; 0.10-0.15
• Phosphorus; 0.040max
• Manganese; 0.5-1.25
• Chromium; 15.0-16.0
• Silicon; 0.50max
• Sulfur; 0.030max
• Molybdenum; 2.5-3.5
• Nickel; 4.0-5.0
• Iron; 73.53-77.33

AMS-5529 Sheet/ Strip
AMS-5529 Sheet/ Strip, is a semi austenitic stainless steel which is austenitic in the annealed condition. It provides high strength & hardness, excellent fatigue properties, good corrosion resistance & minimum distortion upon heat treatment. 

Chemical Composition

• Carbon; 0.090max
• Manganese; 1.00max
• Silicon; 1.00max
• Chromium; 16.0-18.0
• Nickel; 6.50-7.75
• Aluminium; 0.75-1.50
• Phosphorus; 0.040max
• Sulfur; 0.030max
• Iron; Bal

Mechanical Properties

• Tensile Strength(max); 150ksi, 1035Mpa
• 0.2% Offset Yield Strength(max); 65ksi, 450Mpa

AMS-5864, is a martensitic precipitation hardening stainless steel that has excellent strength, high hardness, good corrosion resistance & superior toughness. It offers a high level of useful mechanical properties under severe environmental conditions.

Chemical Composition

• Carbon; 0.05max
• Phosphorus; 0.010max
• Silicon; 0.10max
• Nickel; 7.5-8.5
• Aluminium; 0.90-1.35
• Iron; Bal
• Manganese; 0.10max
• Sulfur; 0.008max
• Chromium; 12.25-13.25
• Molybdenum; 2.0-2.5
• Nitrogen; 0.01max

Mechanical Properties

• Tensile Strength; 220ksi
• 0.2% Yield Strength; 205ksi
• Elongation; 10%
• Reduction of Area; 45%
• Rockwell C Hardness; 45

AMS-5520 Sheet/ Plate/ Strip
AMS-5520, is a precipitation hardening stainless steel used for applications requiring high strength & moderate corrosion resistance.

Chemical Composition

• Carbon; 0.09max
• Manganese; 1.00max
• Silicon; 1.00max
• Phosphorus; 0.040max
• Sulfur; 0.030max
• Chromium; 14.0-16.0
• Nickel; 6.50-7.75
• Molybdenum; 2.0-3.0
• Aluminium; 0.75-1.50

Mechanical Properties

• Tensile Strength, max; 190ksi
• Yield Strength, max; 170ksi
• Elongation; 4%
• Hardness; 40HRC

AMS 5515 is non hardenable by heat treatment & in non magnetic in the annealed condition. It becomes slightly magnetic witgh cold working.  

Chemical Composition

• Carbon; 0.08-0.15
• Manganese; 2.00max
• Silicon; 1.00max
• Chromium; 17.0-19.0
• Nickel; 7.0-10.0
• Molybdenum; 0.75max
• Phosphorus; 0.040max
• Sulfur; 0.030max
• Iron; Bal

Mechanical Properties

• Tensile Strength, min; 75ksi, 515Mpa
• 0.2% Offset Yield Strength, min; 30ksi, 205Mpa
• Elongation; 40%min

AMS 5637 Bar/Wire
AMS 5637, is used for defense, aerospace, oil & gas, wind turbine, pipeline, shipbuilding, medical instrument, satellite & rocket building.

Chemical Composition

• Chromium; 17.0-19.0
• Nickel; 8.0-10.0
• Manganese; 2.00max
• Silicon; 1.00max
• Carbon; 0.15max
• Sulfur; 0.030max
• Phosphorus; 0.045max

Mechanical Properties

• Tensile Strength; 620Mpa, 89900psi
• 0.2% Yield Strength; 275Mpa, 39900psi
• Elongation(in 50mm); 55%
• Hardness, Rockwell B; 85

AMS 5825 Bar/Wire
AMS 5825, is the most widely used steel of the precipitation hardening grade steel. It has high toughness, strength & corrosion resistance. It is used for applications such as aircraft & gas turbines, chemical process components, paper mills, nuclear reactor & oil field.

Chemical Composition

• Carbon; 0.05max
• Manganese; 0.25-0.75
• Silicon; 0.75max
• Sulfur; 0.025max
• Phosphorus; 0.025max
• Chromium; 16.0-16.75
• Nickel; 4.50-5.00
• Columbium; 0.15-0.30
• Copper; 0.15-0.30
• Molybdenum; 0.75max
• Iron; Bal

AMS 5622, is one of the most widely used precipitation hardening grades. It provides good corrosion resistance, high hardness, strength & toughness.

AMS 5622 Tube Chemical Composition

• Carbon; 0.07max
• Silicon; 1.00max
• Manganese; 1.00max
• Phosphorus; 0.040max
• Sulfur; 0.030max
• Chromium; 15.0-17.50
• Molybdenum; 0.50max
• Nickel; 3.0-5.0
• Columbium; 0.45max
• Copper; 3.0-5.0
• Iron; Bal

AMS 5622 Tube Mechanical Properties

• 0.2% Proof Stress; 1172Mpa(min)
• Tensile Strength; 1310Mpa(min)
• Elongation; 6-10%

AMS-5595, is a high manganese nitrogen strengthened steel. It properties include high strength in the annealed condition. It has excellent resistance to corrosion at high temperatures. It is used in a numerous applications including chemical processing, aircraft engine & pollution control equipment.

Chemical Composition

• Carbon; 0.040max
• Phosphorus; 0.060max
• Silicon; 1.00max
• Nickel; 5.5-7.5
• Manganese; 8.0-10.0
• Sulfur; 0.030max
• Chromium; 19.0-21.5
• Nitrogen; 0.15-0.40
• Molybdenum; 0.75max
• Copper; 0.75max
• Iron; Bal

Mechanical Properties

• 0.2% Yield Strength; 62ksi, 428Mpa
• Ultimate Tensile Strength; 95ksi, 655Mpa
• Elongation in 2"; 46%

Aesteiron Steels LLP, is one of the leading manufacturers, suppliers and exporters of Hastelloy B-3 Plate.

UNS Number N010675

Hastelloy B3 Application

• Maintains excellent ductility during transient exposures to intermediate temperatures
• Excellent resistance to pitting, corrosion and stress-corrosion cracking
• Excellent resistance to knife-line and heat-affected zone attack
• Excellent resistance to acetic, formic and phosphoric acids and other non-oxidizing media
• Resistance to hydrochloric acid at all concentrations and temperatures
• Thermal stability superior to alloy B-2

Hastelloy B3 Chemical Composition


Specification


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Aesteiron Steels LLP, is one of the leading manufacturers, suppliers and exporters of Hastelloy C-22 Plates.

UNS Number N06022

Hastelloy C-22 Application

• Resistant to pitting, crevice corrosion and stress corrosion cracking
• Outstanding resistance to both reducing and oxidizing media
• Excellent resistance to oxidizing aqueous media
• Exceptional resistance to a wide variety of chemical process environments including strong oxidizers such as ferric acids, acetic anhydride, and seawater and brine solutions
• Resists the formation of grain-boundary precipitates in the weld heat-affected zone
• Excellent weldability

Hastelloy C-22 Chemical Composition

Hastelloy C-22 Mechanical Properties

Specifications


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