Mechanical Properties | Metric | English | Comments |
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Tensile Strength, Ultimate | 750 MPa @Thickness 12.7 mm, Temperature 149 °C |
109000 psi @Thickness 0.500 in, Temperature 300 °F |
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Haynes Hastelloy® Hybrid-BC1® Nickel Alloy Shielded Metal Arc Welded (SMAW) Plate HASTELLOY® HYBRID-BC1® alloy possesses much higher resistance to hydrochloric and sulfuric acids than the nickel-chromium-molybdenum (C-type) alloys, and can tolerate the presence of oxidizing.. |
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Tensile Strength, Ultimate | 751 MPa @Thickness 9.50 - 25.4 mm, Temperature 427 °C |
109000 psi @Thickness 0.374 - 1.00 in, Temperature 801 °F |
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Haynes Hastelloy® S alloy, flat products Nickel-based, high temperature alloy. Excellent thermal stability, low thermal expansion, excellent oxidation resistance to 1093°C, good high temperature and thermal fatigue strength. Application.. |
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Tensile Strength, Ultimate | 752 MPa @Thickness 25.4 mm |
109000 psi @Thickness 1.00 in |
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Haynes Hastelloy® C-2000® alloy, flat products Nickel-chromium-molybdenum (Ni-Cr-Mo) C-type alloys have a long history of use in the Chemical Process Industries and are known for their versatility. Not only do they resist all acids (especially h.. |
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Tensile Strength, Ultimate | 752 MPa @Thickness 1.60 mm |
109000 psi @Thickness 0.0630 in |
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Haynes Hastelloy® C-2000® alloy, flat products Nickel-chromium-molybdenum (Ni-Cr-Mo) C-type alloys have a long history of use in the Chemical Process Industries and are known for their versatility. Not only do they resist all acids (especially h.. |
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Tensile Strength, Ultimate | 752 MPa @Thickness 46.1 mm, Temperature 20.0 °C |
109000 psi @Thickness 1.81 in, Temperature 68.0 °F |
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Haynes Hastelloy® C-22® alloy, transverse, GMAW short arc weldment, plate HASTELLOY® C-22® alloy is a nickel-chromium-molybdenum-tungsten alloy with excellent overall corrosion resistance compared to other Ni-Cr-Mo alloys, including HASTELLOY C-276 and C-4 alloys an.. |
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Tensile Strength, Ultimate | 754 MPa @Temperature 200 °C |
109000 psi @Temperature 392 °F |
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Haynes Hastelloy® C-22HS™ Nickel Alloy Sheet, Cold-rolled, Solution Annealed Outstanding Corrosion Resistance, High Strength HASTELLOY® C-22HSTM alloy is corrosion-resistant, nickel-chromium-molybdenum alloy which can be heat treated to obtain a strength approximately dou.. |
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Tensile Strength, Ultimate | 754 MPa @Thickness 3.20 mm, Temperature 260 °C |
109000 psi @Thickness 0.126 in, Temperature 500 °F |
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Haynes Hastelloy® Hybrid-BC1® Nickel Alloy Sheet, Cold Rolled and Solution Annealed HASTELLOY® HYBRID-BC1® alloy possesses much higher resistance to hydrochloric and sulfuric acids than the nickel-chromium-molybdenum (C-type) alloys, and can tolerate the presence of oxidizing.. |
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Tensile Strength, Ultimate | 750 MPa @Temperature 260 °C |
109000 psi @Temperature 500 °F |
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Crucible Steel XM-19 Stainless Steel Crucible XM-19 Stainless is a nitrogen strengthened, low carbon, austenitic, stainless steel that provides good corrosion resistance in combination with high strength. The alloy has better corrosio.. |
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Tensile Strength, Ultimate | 752 MPa @Thickness 12.7 mm, Temperature 20.0 °C |
109000 psi @Thickness 0.500 in, Temperature 68.0 °F |
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Haynes Hastelloy® C-22® alloy, transverse, GTAW short arc weldment, plate HASTELLOY® C-22® alloy is a nickel-chromium-molybdenum-tungsten alloy with excellent overall corrosion resistance compared to other Ni-Cr-Mo alloys, including HASTELLOY C-276 and C-4 alloys and al.. |
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Tensile Strength, Ultimate | 749 MPa @Thickness 19.1 mm, Temperature 149 °C |
109000 psi @Thickness 0.752 in, Temperature 300 °F |
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Haynes Hastelloy® Hybrid-BC1® Nickel Alloy Plate, Hot Rolled and Solution Annealed HASTELLOY® HYBRID-BC1® alloy possesses much higher resistance to hydrochloric and sulfuric acids than the nickel-chromium-molybdenum (C-type) alloys, and can tolerate the presence of oxidizing spe.. |
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Tensile Strength, Ultimate | 750 MPa @Temperature 800 °C |
109000 psi @Temperature 1470 °F |
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Haynes 282® Nickel Alloy Plate, Solution Annealed and Age-Hardened Excellent High Temperature Strength HAYNES® 282® alloy is a wrought, gamma-prime strengthened superalloy developed for high temperature structural applications, especially those in aero and land-b.. |