Polymer Property : Density = 8.19 g/cc Product List

Physical Properties

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Physical Properties	Metric	English	Comments
Density	8.19 g/cc	0.296 lb/inÂ³
IBC Advanced Alloys 46C Beryllium Nickel Casting Alloy Beryllium nickel casting alloys are characterized by their steel-like high strength, toughness, and hardness properties. However, unlike the steel alloys, the beryllium nickel alloy system offers th..
Density	8.19 g/cc	0.296 lb/inÂ³
Indium Corp. IndalloyÂ® 204 In-Pb Solder Alloy Indalloy's #7, #10, #150, #204, #205 and #206 comprise a group of lead-indium solders designed to cover the temperature range of 165Â°C-275Â°C. All have the minimum gold-leaching characteristics..
Density	8.19 g/cc	0.296 lb/inÂ³	P/M (98%)
Kennametal Stellite DeloroÂ® N-6 PM with P/M Processing Adhesive wear test data: P/M 0.1, cast 0.1; Abrasive wear test data: P/M 17, cast 35. Typical applications include vane plugs, fuel metering pins, spacer bushings, ball bearing blanks, race bearing ..
Density	8.19 g/cc	0.296 lb/inÂ³
Special Metals DURANICKELÂ® 301 (UNS N03301) Annealed and Aged Rod and Bar Tensile strength (ultimate and yield), compressive strength, hardness, and elongation values reported here are typical for Annealed and Aged Rod and Bar specifically. Other property values are typic..
Density	8.19 g/cc	0.296 lb/inÂ³
Special Metals DURANICKELÂ® 301 (UNS N03301) Annealed and Aged Wire Tensile strength (ultimate) and elongation values reported here are typical for Annealed and Aged Wire specifically. Other property values are typical of aged DURANICKELÂ® alloy 301 or the alloy i..
Density	8.19 g/cc	0.296 lb/inÂ³
Special Metals DURANICKELÂ® 301 (UNS N03301) Annealed Rod and Bar Tensile strength (ultimate and yield), compressive strength, hardness, and elongation values reported here are typical for Annealed Rod and Bar specifically. Other property values are typical of ann..
Density	8.19 g/cc	0.296 lb/inÂ³
Special Metals DURANICKELÂ® 301 (UNS N03301) Cold-Drawn and Aged Rod and Bar Tensile strength (ultimate and yield), compressive strength, hardness, and elongation values reported here are typical for Cold-Drawn and Aged Rod and Bar specifically. Other property values are typ..
Density	8.19 g/cc	0.296 lb/inÂ³
Special Metals DURANICKELÂ® 301 (UNS N03301) Half-Hard and Aged Strip Tensile strength (ultimate), hardness, and elongation values reported here are typical for Half-Hard and Aged Strip specifically. Other property values are typical of aged DURANICKELÂ® alloy 301 o..
Density	8.19 g/cc	0.296 lb/inÂ³
Special Metals DURANICKELÂ® 301 (UNS N03301) Half-Hard Strip Tensile strength (ultimate), hardness, and elongation values reported here are typical for Half-Hard Strip specifically. Other property values are typical of annealed DURANICKELÂ® alloy 301 or the..
Density	8.19 g/cc	0.296 lb/inÂ³
Special Metals DURANICKELÂ® 301 (UNS N03301) Hot-Finished and Aged Rod and Bar Tensile strength (ultimate and yield), hardness, and elongation values reported here are typical for Hot-Finished and Aged Rod and Bar specifically. Other property values are typical of aged DURANIC..
Density	8.19 g/cc	0.296 lb/inÂ³
Special Metals DURANICKELÂ® 301 (UNS N03301) Hot-Finished Rod and Bar Tensile strength (ultimate and yield), hardness, and elongation values reported here are typical for Hot-Finished Rod and Bar specifically. Other property values are typical of annealed DURANICKELÂ..
Density	8.19 g/cc	0.296 lb/inÂ³
Special Metals DURANICKELÂ® 301 (UNS N03301) Spring Strip, Aged Tensile strength (ultimate), hardness, and elongation values reported here are typical for Spring Strip, Aged specifically. Other property values are typical of aged DURANICKELÂ® alloy 301 or the ..
Density	8.19 g/cc	0.296 lb/inÂ³
Special Metals DURANICKELÂ® 301 (UNS N03301) Spring Wire Tensile strength (ultimate) and elongation values reported here are typical for Spring Wire specifically. Other property values are typical of annealed DURANICKELÂ® alloy 301 or the alloy in gener..
Density	8.19 g/cc	0.296 lb/inÂ³
Special Metals DURANICKELÂ® 301 (UNS N03301) Spring Wire, Aged Tensile strength (ultimate) and elongation values reported here are typical for Spring Wire, Aged specifically. Other property values are typical of aged DURANICKELÂ® alloy 301 or the alloy in gen..
Density	8.19 g/cc	0.296 lb/inÂ³
Special Metals INCONELÂ® 690 Nickel Superalloy, Cold Drawn Tube, 3.50 inch (88.9 mm) o.d. and 0.219 inch (5.49 mm) Thickness Composition adjustments for nuclear applications: 28-31 Cr; 0.04 max C; 0.10 max Co.Tensile strength (ultimate and yield) and elongation values reported here are typical for Cold Drawn Tube, 3.50 in..
Density	8.19 g/cc	0.296 lb/inÂ³
Special Metals INCONELÂ® 690 Nickel Superalloy, Hot Rolled Flat, 0.5 x 2.0 inch (13 x 51 mm) Composition adjustments for nuclear applications: 28-31 Cr; 0.04 max C; 0.10 max Co.Tensile strength (ultimate and yield) and elongation values reported here are typical for Hot Rolled Flat, 0.5 x 2..
Density	8.19 g/cc	0.296 lb/inÂ³
Special Metals INCONELÂ® 690 Nickel Superalloy, Hot Rolled Flat, 2.0 inch (51 mm) Diameter Composition adjustments for nuclear applications: 28-31 Cr; 0.04 max C; 0.10 max Co.Tensile strength (ultimate and yield) and elongation values reported here are typical for Hot Rolled Flat, 2.0 inc..
Density	8.19 g/cc	0.296 lb/inÂ³
Special Metals INCONELÂ® 718SPFâ„¢ Nickel Superalloy, Annealed Typical annealing - continuous process anneal, 1700Â°F (927Â°C) at 15 ft (4.57 m) per minute. This produces ASTM No. 12 grain size. Heat capacity, melting range, moduli, and Poisson's ratio re..
Density	8.19 g/cc	0.296 lb/inÂ³
Special Metals INCONELÂ® Alloy 718 Developed in the early 1960's, IN718 is still considered the material of choice for the majority of aircraft engine components with service temperatures below 1200Â°F (650Â°C). Inconel 718 is a..
Density	8.19 g/cc	0.296 lb/inÂ³
Special Metals NIMONICÂ® Alloy 80A A nickel-chromium alloy similar to NIMONIC alloy 75 but made precipitation hardenable by additions of aluminum and titanium. The alloy has good corrosion and oxidation resistance and high tensile a..
Density	8.19 g/cc	0.296 lb/inÂ³
Special Metals UDIMETÂ® alloy D-979 Fe-Ni Alloy UDIMETÂ® alloy D-979 (UNS N09979) is an iron-nickel alloy designed for turbine disc applications at temperatures up to 1200-1400Â°F (649-760Â°C). Hardened by a complex precipitation of interm..
Density	8.19 g/cc	0.296 lb/in³
Williams Advanced Alloys WS174 Solder All Williams alloys are available in a variety of shapes and forms, including ribbon, preforms, rod, ring, wire, and custom shapes.Information provided by Williams Advanced Alloys
Density	8.19 g/cc	0.296 lb/in³
California Fine Wire Manganin 290 Copper, Manganese, and Nickel Resistance Wire All values may vary dependent on specific design and usageCapabilities: WireRibbonSquareInsulatedPlatedInformation provided by California Fine Wire.
Density	8.19 g/cc	0.296 lb/in³
ATI Allegheny Ludlum Altemp® 718 Nickel-Base Superalloy, Solution Treated Sheet and Strip, 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..
Density	8.19 g/cc	0.296 lb/in³
ATI Allvac® 718 Nickel Superalloy, Heat Treatment: 982°C (1800°F) + Age Data provided by Allvac.Applications: Jet engine rings, discs, shafts, compressor blades, seals, spacers. Fasteners, nuclear, oil & gas components.
Density	8.19 g/cc	0.296 lb/in³
ATI Allvac® 718-OP® UNS N07718 Nickel Superalloy Uses: Turbines and engines, fasteners, sub-surface safety valves, hot extrusion tooling, nuclear reactors.Property values are for samples in the metallurgical condition: 1800°F age.Information prov..
Density	8.19 g/cc	0.296 lb/in³
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..
Density	8.19 g/cc	0.296 lb/in³	P/M (98%)
Kennametal Stellite Deloro® N-6 PM cast Adhesive wear test data: P/M 0.1, cast 0.1; Abrasive wear test data: P/M 17, cast 35. Typical applications include vane plugs, fuel metering pins, spacer bushings, ball bearing blanks, race bearing ..
Density	8.19 g/cc	0.296 lb/in³
ATI Allvac® WASPALOY® Nickel Superalloy, Heat Treatment: 1010°C (1850°F) + Age Data provided by Allvac.Applications: Turbine compressor blades and discs, shafts, spacers, fasteners, miscellaneous jet engine hardware; space shuttle turbo pump seals.Waspaloy is a registered trad..
Density	8.19 g/cc	0.296 lb/in³
Latrobe LSS™ H21 Hot Work Tool Steel (ASTM H21) TLS H21 hot work tool steel is a low-carbon, tungsten hot work steel that exhibits excellent resistance to softening at elevated temperature. This grade is intended for elevated-temperature service ..