Thermal Properties | Metric | English | Comments |
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CTE, linear | 12.8 µm/m-°C @Temperature 250 °C |
7.11 µin/in-°F @Temperature 482 °F |
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Mykroy/Mycalex MM 561 Molding Grade Glass-bonded Mica Composite Synthetic mica filler. Does not burn. Good radiation resistance (3 x 10^10 Rads-Cobalt). ROHS CompliantThis ceramoplastic material is a versatile and efficient insulating material designed to meet.. |
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CTE, linear | 12.8 µm/m-°C @Temperature 0.000 - 200 °C |
7.11 µin/in-°F @Temperature 32.0 - 392 °F |
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Kennametal Stellite Stellite® 12 PM with P/M Processing Applications: include vane plugs, fuel metering pins, spacer bushings, ball blanks (bearings), race blanks (bearings), diesel engine exhaust, fluid valve seats, saw cutter inserts, miscellaneous wea.. |
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CTE, linear | 12.8 µm/m-°C @Temperature 20.0 - 316 °C |
7.11 µin/in-°F @Temperature 68.0 - 601 °F |
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Haynes Hastelloy® S alloy, flat products, solution heat-treated at 538°C (1000°F), aged 4000 hours 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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CTE, linear | 12.8 µm/m-°C @Temperature 20.0 - 316 °C |
7.11 µin/in-°F @Temperature 68.0 - 601 °F |
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Haynes Hastelloy® S alloy, flat products, solution heat-treated at 538°C (1000°F), aged 8000 hours 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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CTE, linear | 12.8 µm/m-°C @Temperature 20.0 - 316 °C |
7.11 µin/in-°F @Temperature 68.0 - 601 °F |
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Haynes Hastelloy® S alloy, gas tungsten arc welded plate 12.7 mm (1/2 in.) thick, aged at 649°C (1200°F) for 8000 hours 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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CTE, linear | 12.8 µm/m-°C @Temperature 20.0 - 316 °C |
7.11 µin/in-°F @Temperature 68.0 - 601 °F |
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Haynes Hastelloy® S alloy, gas tungsten arc welded, aged 1300 hours 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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CTE, linear | 12.8 µm/m-°C @Temperature 20.0 - 316 °C |
7.11 µin/in-°F @Temperature 68.0 - 601 °F |
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Haynes Hastelloy® S alloy, plate 12.7 mm (1/2 in.) thick, solution heat-treated at 427°C (800°F), aged 1000 hours 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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CTE, linear | 12.8 µm/m-°C @Temperature 20.0 - 316 °C |
7.11 µin/in-°F @Temperature 68.0 - 601 °F |
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Haynes Hastelloy® S alloy, plate 12.7 mm (1/2 in.) thick, solution heat-treated at 871°C (1600°F), aged 16000 hours 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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CTE, linear | 12.8 µm/m-°C @Temperature 20.0 - 316 °C |
7.11 µin/in-°F @Temperature 68.0 - 601 °F |
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Haynes Hastelloy® S alloy, weld metal, aged 1000 hours 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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CTE, linear | 12.8 µm/m-°C @Temperature 20.0 - 316 °C |
7.11 µin/in-°F @Temperature 68.0 - 601 °F |
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Haynes Hastelloy® S alloy, weld metal, aged 4000 hours 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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CTE, linear | 12.8 µm/m-°C @Temperature 25.0 - 300 °C |
7.11 µin/in-°F @Temperature 77.0 - 572 °F |
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Haynes 282® Nickel Alloy Synergic Gas Metal Arc Welded (GMAW) Plate 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 la.. |
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CTE, linear | 12.8 µm/m-°C @Temperature 25.0 - 100 °C |
7.11 µin/in-°F @Temperature 77.0 - 212 °F |
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Haynes 625 alloy, 20% cold reduction, 1010°C anneal for 5 minutes Cb and Ta content 3.7% combined. Excellent strength up to 816°C, good oxidation resistance and aqueous corrosion, excellent forming and welding characteristics. Applications include a variety of .. |
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CTE, linear | 12.8 µm/m-°C @Temperature 25.0 - 100 °C |
7.11 µin/in-°F @Temperature 77.0 - 212 °F |
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Haynes 625 alloy, plate after 8000 hours at 760°C (1400°F) Cb and Ta content 3.7% combined. Excellent strength up to 816°C, good oxidation resistance and aqueous corrosion, excellent forming and welding characteristics. Applications include a variety of .. |
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CTE, linear | 12.8 µm/m-°C @Temperature 25.0 - 100 °C |
7.11 µin/in-°F @Temperature 77.0 - 212 °F |
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Haynes 625 alloy, plate, as annealed at 1025°C, rapid cooled Cb and Ta content 3.7% combined. Excellent strength up to 816°C, good oxidation resistance and aqueous corrosion, excellent forming and welding characteristics. Applications include a variety of .. |
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CTE, linear | 12.8 µm/m-°C @Temperature 21.0 - 427 °C |
7.11 µin/in-°F @Temperature 69.8 - 801 °F |
0.20%C |
Latrobe CBS-600™ VIM-VAR Carburizing Bearing and Gear Steel CBS-600 VIM-VAR is a carburizing bearing and gear steel designed for service temperatures up to 600°F. Double vacuum melting is employed to provide optimum tensile properties as well as describe.. |
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CTE, linear | 12.8 µm/m-°C @Temperature 23.9 - 316 °C |
7.11 µin/in-°F @Temperature 75.0 - 600 °F |
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HP Alloys Alloy C-276, 10% Cold Worked 10% Cold Worked applies to tensile and/or hardness; other properties are typical of this alloy.Data provided by High Performance Alloys, Inc., Allvac, Inco Alloys International, and Haynes Internati.. |
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CTE, linear | 12.8 µm/m-°C @Temperature 21.0 - 100 °C |
7.11 µin/in-°F @Temperature 69.8 - 212 °F |
Mean |
Special Metals INCONEL® 625LCF® Nickel Superalloy (UNS N06626) Annealed + 30% Cold Work Tensile strength (ultimate and yield), elongation, and reduction of area values are for annealed then cold worked samples. This produces ASTM grain size 10.0. Other property values are typical of .. |
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CTE, linear | 12.8 µm/m-°C @Temperature 21.0 - 100 °C |
7.11 µin/in-°F @Temperature 69.8 - 212 °F |
Mean |
Special Metals INCONEL® 625LCF® Nickel Superalloy (UNS N06626) Annealed + 5% Cold Work Tensile strength (ultimate and yield), elongation, and reduction of area values are for annealed then cold worked samples. This produces ASTM grain size 9.0. Other property values are typical of t.. |
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CTE, linear | 12.8 µm/m-°C @Temperature 21.0 - 100 °C |
7.11 µin/in-°F @Temperature 69.8 - 212 °F |
Mean |
Special Metals INCONEL® 625LCF® Nickel Superalloy (UNS N06626) Annealed 1950°F (1070°C) Tensile strength (ultimate and yield), elongation, and hardness values are for samples annealed 1950°F (1070°C)/5 minutes/AC. This produces ASTM grain size 9.5. Other property values are ty.. |
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CTE, linear | 12.8 µm/m-°C @Temperature 21.0 - 100 °C |
7.11 µin/in-°F @Temperature 69.8 - 212 °F |
Mean |
Special Metals INCONEL® 625LCF® Nickel Superalloy (UNS N06626) Annealed 2150°F (1180°C) Tensile strength (ultimate and yield), elongation, and hardness values are for samples annealed 2150°F (1180°C)/5 minutes/AC. This produces ASTM grain size 5.5. Other property values are ty.. |
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CTE, linear | 12.8 µm/m-°C @Temperature 0.000 - 100 °C |
7.11 µin/in-°F @Temperature 32.0 - 212 °F |
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Carpenter BioDur™ CCM Plus™ Medical Implant Alloy, Annealed 1093°C 1 hr Data provided by Carpenter Technology Corporation.Annealing followed by water quench and low stress grinding prior to tensile testing.Medical Implant Alloy. Non-magnetic Co-Cr-Mo alloy exhibiting h.. |
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CTE, linear | 12.8 µm/m-°C @Temperature 0.000 - 100 °C |
7.11 µin/in-°F @Temperature 32.0 - 212 °F |
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Carpenter BioDur™ CCM Plus™ Medical Implant Alloy, Annealed 1093°C 2 hr Data provided by Carpenter Technology Corporation.Annealing followed by water quench and low stress grinding prior to tensile testing.Medical Implant Alloy. Non-magnetic Co-Cr-Mo alloy exhibiting h.. |
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CTE, linear | 12.8 µm/m-°C @Temperature 0.000 - 100 °C |
7.11 µin/in-°F @Temperature 32.0 - 212 °F |
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Carpenter BioDur™ CCM Plus™ Medical Implant Alloy, Annealed 1121°C 1 hr Data provided by Carpenter Technology Corporation.Annealing followed by water quench and low stress grinding prior to tensile testing.Medical Implant Alloy. Non-magnetic Co-Cr-Mo alloy exhibiting h.. |
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CTE, linear | 12.8 µm/m-°C @Temperature 21.0 - 93.0 °C |
7.11 µin/in-°F @Temperature 69.8 - 199 °F |
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Carpenter MP35N* Ni-Co-Cr-Mo Alloy, 35% Cold Reduction Data provided by Carpenter Technology Corporation.Carpenter MP35N alloy is a nonmagnetic, nickel-cobalt-chromium-molybdenum alloy possessing a unique combination of ultrahigh tensile strength, good .. |
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CTE, linear | 12.8 µm/m-°C @Temperature 21.0 - 93.0 °C |
7.11 µin/in-°F @Temperature 69.8 - 199 °F |
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Carpenter MP35N* Ni-Co-Cr-Mo Alloy, 45% Cold Reduction Data provided by Carpenter Technology Corporation.Carpenter MP35N alloy is a nonmagnetic, nickel-cobalt-chromium-molybdenum alloy possessing a unique combination of ultrahigh tensile strength, good .. |
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CTE, linear | 12.8 µm/m-°C @Temperature 21.0 - 93.0 °C |
7.11 µin/in-°F @Temperature 69.8 - 199 °F |
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Carpenter MP35N* Ni-Co-Cr-Mo Alloy, Cold Drawn 33%, Aged 565°C/4hr/AC Data provided by Carpenter Technology Corporation.Carpenter MP35N alloy is a nonmagnetic, nickel-cobalt-chromium-molybdenum alloy possessing a unique combination of ultrahigh tensile strength, good .. |
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CTE, linear | 12.8 µm/m-°C @Temperature 20.0 - 600 °C |
7.11 µin/in-°F @Temperature 68.0 - 1110 °F |
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ATI Allegheny Ludlum Martensitic Stainless Steel Type 425 Mod, Hardened + 427°C Temper Allegheny Ludlum Type 425 Mod is a hardenable straight-chromium stainless steel which combines superior wear resistance of high carbon alloys with the excellent corrosion resistance of chromium stai.. |
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CTE, linear | 12.8 µm/m-°C @Temperature 20.0 - 93.0 °C |
7.11 µin/in-°F @Temperature 68.0 - 199 °F |
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ATI Allegheny Ludlum Altemp® 718 Nickel-Base Superalloy, Solution Treated Plate, UNS N07718 Allegheny Ludlum Altemp 718 alloy is an austenitic nickel-base superalloy which is used in applications requiring high strength to approximately 760 degrees Celsius and oxidation resistance to appro.. |
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CTE, linear | 12.8 µm/m-°C @Temperature 20.0 - 316 °C |
7.11 µin/in-°F @Temperature 68.0 - 601 °F |
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Haynes Hastelloy® S alloy, plate 12.7 mm (1/2 in.) thick, solution heat-treated at 871°C (1600°F), aged 1000 hours Nickel-based, high temperature alloy. Excellent thermal stability, low thermal expansion, excellent oxidation resistance to 1093°C, good high temperature and thermal fatigue strength. Applications .. |
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CTE, linear | 12.8 µm/m-°C @Temperature 20.0 - 316 °C |
7.11 µin/in-°F @Temperature 68.0 - 601 °F |
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Haynes Hastelloy® S alloy, gas tungsten arc welded plate 12.7 mm (1/2 in.) thick, aged 4000 hours Nickel-based, high temperature alloy. Excellent thermal stability, low thermal expansion, excellent oxidation resistance to 1093°C, good high temperature and thermal fatigue strength. Applications .. |