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Special Alloys/Corrosion-Resistant Alloy/

ALLOY 188 (UNS R30188) – High-Temperature Cobalt-Nickel Superalloy for Extreme Heat & Corrosion Environments

HAYNES® 188 alloy (UNS R30188) is a cobalt-nickel-chromium-tungsten superalloy that delivers an exceptional combination of high-temperature strength, long-term oxidation resistance up to 2000°F (1095°C), and outstanding resistance to sulfate-deposit hot corrosion. This versatile material is also highly resistant to molten chloride salts and gaseous sulfidation, making it a reliable choice for the most demanding chemical processing, power generation, and aerospace applications. Alloy 188 is readily fabricated and formed using conventional techniques and has been successfully used for both wrought and cast components. Equivalent Designations PWA 1042 Werkstoff 2.4683 / EN 2.4683 AMS 5801 / AMS 5608 Alloy 188 pipes Applicable Specifications (HAYNES® 188 / UNS R30188) Product FormSpecificationSheet, Plate & StripAMS 5608Billet, Rod & BarAMS 5772ForgingsAMS 5772Coated Electrodes–Bare Welding Rods…

  • Product Details

HAYNES® 188 alloy (UNS R30188) is a cobalt-nickel-chromium-tungsten superalloy that delivers an exceptional combination of high-temperature strength, long-term oxidation resistance up to 2000°F (1095°C), and outstanding resistance to sulfate-deposit hot corrosion. This versatile material is also highly resistant to molten chloride salts and gaseous sulfidation, making it a reliable choice for the most demanding chemical processing, power generation, and aerospace applications. Alloy 188 is readily fabricated and formed using conventional techniques and has been successfully used for both wrought and cast components.

Equivalent Designations

  • PWA 1042
  • Werkstoff 2.4683 / EN 2.4683
  • AMS 5801 / AMS 5608
Alloy 188 pipes
Alloy 188 pipes

Applicable Specifications (HAYNES® 188 / UNS R30188)

Product FormSpecification
Sheet, Plate & StripAMS 5608
Billet, Rod & BarAMS 5772
ForgingsAMS 5772
Coated Electrodes
Bare Welding Rods & Wire
Seamless Pipe & Tube
Welded Pipe & Tube
Fittings

UNS R30188 Chemical Composition

ElementWeight %
Cobalt39 (Balance)
Nickel22
Chromium22
Tungsten14
Iron3 max.
Manganese1.25 max.
Silicon0.35
Carbon0.1
Lanthanum0.03
Boron0.015 max.

ALLOY 188 Physical Properties (at 22 °C / 72 °F)

PropertyMetricEnglish
Density8.98 g/cm³0.324 lbs/in³
Modulus of Elasticity232 GPa33.7 Mpsi
Electrical Resistivity101.0 μohm·m39.6 μohm·in
Thermal Conductivity10.4 W/m·°K72 BTU·in/hr·ft²·°F
Coefficient of Thermal Expansion12.1 μm/(m·°C)6.7 μin/(in·°F)

Typical Mechanical Properties – Room Temperature Cold-Worked

Cold Worked %Yield StrengthUltimate Tensile StrengthElongation %
0938 MPa (136 ksi)1324 MPa (192 ksi)34
201110 MPa (161 ksi)1544 MPa (224 ksi)5.6
371641 MPa (238 ksi)2013 MPa (292 ksi)4.1
501813 MPa (263 ksi)2165 MPa (314 ksi)3.3
Values typical; 25.4 cm (10 in) gauge length.

Elevated-Temperature Tensile Properties – Hot-Rolled & Solution-Annealed Plate

Test Temp (°F/°C)YS (ksi/MPa)UTS (ksi/MPa)Elong. %
RT / RT70.1 / 483143.8 / 99150.6
1000 / 53845.7 / 315120.6 / 83260.3
1200 / 64945.1 / 311121.6 / 83862.8
1400 / 76043.6 / 30184.1 / 58085.6
1600 / 87137.1 / 25649.5 / 34197.9
1800 / 98219.2 / 13227.2 / 188102.6
2000 / 10939.6 / 6613.9 / 9687.1

Elevated-Temperature Tensile Properties – Cold-Rolled & Solution-Annealed Sheet

Test Temp (°F/°C)YS (ksi/MPa)UTS (ksi/MPa)Elong. %
RT / RT70.1 / 483142.4 / 98250.9
1000 / 53844.8 / 309117.4 / 80958.8
1200 / 64944.8 / 309119.1 / 82158.6
1400 / 76043.8 / 30281.6 / 56381.8
1600 / 87137.8 / 26147.0 / 324103.9
1800 / 98218.2 / 12525.4 / 17581.0
2000 / 10938.5 / 5912.4 / 8549.7

Thermal Stability

Like solid-solution-strengthened superalloys (e.g., Alloy 625 or HASTELLOY® X), HAYNES® 188 alloy can precipitate a CO₂W Laves phase after prolonged high-temperature exposure, which may reduce tensile ductility and impact strength. However, Alloy 188 demonstrates significantly better thermal stability than the older HAYNES® 25 alloy. For applications where maximum thermal stability is critical, 230® alloy is recommended.

Figure. Retained tensile ductility vs. exposure temperature (8000 h).
Figure. Retained tensile ductility vs. exposure temperature (8000 h).

Room-Temperature Properties of Plate After Thermal Exposure

Exposure Temperature0.2% Yield StrengthUltimate Tensile StrengthElongationImpact Strength
°F°ChksiMPaksiMPa%ft.- lbs.J
1200650065.0450140.096556.0143194
800079.7550151.6104529.12331
1400760065.0450140.096556.0143194
800074.0510147.9102010.834
16008700*70.1485146.0100550.4143194
100070.7490157.5108528.71013
8000*64.5445147.4101522.2912

Welding & Forming

Alloy 188 offers good formability and welding characteristics. It can be forged or hot-worked after soaking at 2150°F (1175°C). Its excellent ductility also permits cold forming, but the alloy work-hardens rapidly—frequent intermediate annealing may be necessary for complex shapes. All hot- or cold-worked parts should be annealed and rapidly cooled to restore optimal properties. Welding processes include TIG, MIG, electron beam, and resistance welding, with good restraint-welding performance.

Heat Treatment

Wrought HAYNES® 188 alloy is supplied in the solution heat-treated condition. Standard solution treatment: 2125–2175°F (1163–1191°C) followed by rapid cooling or water quenching. Annealing below solution temperature can cause carbide precipitation that may alter properties.


Contact Us – Your Global Supplier of Alloy 188 Pipe Fittings & Flanges

We warmly welcome global customers to inquire about HAYNES® 188 alloy (UNS R30188) and our full range of specialty alloy pipe fittings, flanges, forged parts, and custom machining solutions. From material verification and full technical consultation to one-stop procurement, we support your chemical processing, power plant, environmental, and hydrometallurgy projects with reliable quality and on-time delivery.


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