24,832 materials
InAg₂PS₄ is an experimental ternary compound combining indium, silver, phosphorus, and sulfur, belonging to the family of metal chalcogenophosphides. This material is primarily of research interest for optoelectronic and photovoltaic applications, where its band structure and light-absorbing properties are being investigated as a potential alternative to more conventional semiconductors. The compound's combination of heavy metal cations and mixed anion chemistry positions it as a candidate for next-generation thin-film solar cells, photodetectors, or nonlinear optical devices, though it remains largely in the development phase with limited commercial deployment.
InAg₂SbSe₄ is a quaternary intermetallic compound combining indium, silver, antimony, and selenium—a material family of emerging interest for thermoelectric and optoelectronic applications. This is primarily a research-phase material rather than a widely commercialized alloy; compounds in this compositional space are investigated for their potential as narrow-bandgap semiconductors and for conversion efficiency in thermoelectric devices where cost and performance trade-offs against traditional alternatives (bismuth telluride, lead telluride) are being evaluated.
InAg3 is an intermetallic compound composed of indium and silver, representing a brittle metallic phase used primarily in specialized joining and electrical applications. This material is encountered in solder metallurgy, microelectronics packaging, and thermal management systems where the indium-silver phase diagram produces beneficial properties at specific compositions. Engineers select InAg3-containing systems for their thermal conductivity and wetting characteristics in high-reliability applications, though the compound itself is typically a secondary phase in composite solder matrices rather than used in pure form.
InAg₃F₆ is an intermetallic compound combining indium, silver, and fluorine, representing a specialized metal-fluoride phase with potential applications in advanced materials research. This compound belongs to an understudied class of precious metal fluorides that may offer unique thermal, electrical, or catalytic properties distinct from conventional binary alloys. Limited industrial deployment suggests this material remains primarily in the research and development phase, with potential relevance to specialized applications in fluoride chemistry, electronics, or catalysis where combined noble metal and fluorine chemistry provides functional advantages.
InAgAu2 is a ternary precious metal alloy combining indium, silver, and gold in a 1:1:2 composition ratio. This material belongs to the family of high-density noble metal alloys and appears primarily in research and specialized industrial contexts rather than commodity applications. The combination of three precious metals suggests potential use in high-reliability electronic contacts, specialized brazing applications, or research into advanced interconnect materials where corrosion resistance, electrical conductivity, and thermal stability are critical.
InAgGeSe₄ is a quaternary chalcogenide compound combining indium, silver, germanium, and selenium—a specialized material from the metal chalcogenide family rather than a conventional metallic alloy. This composition is primarily of research and developmental interest for optoelectronic and photonic applications, where its semiconductor or semi-metallic properties in the infrared region may offer advantages in specialized sensing, nonlinear optical devices, or thermal imaging systems compared to binary or ternary alternatives.
InAgI2 is a ternary intermetallic compound composed of indium, silver, and iodine, belonging to the class of metal halides and intermetallic phases. This material is primarily of research and academic interest rather than established in high-volume industrial production; it represents experimental chemistry in the field of semiconducting intermetallics and potential optoelectronic or thermoelectric applications. The material's notable characteristics stem from its mixed-metal composition, which can offer tunable electronic properties and potential for niche applications in solid-state devices, though it remains less developed than conventional binary semiconductors or well-established ternary compounds.
InAgN3 is a ternary compound combining indium, silver, and nitrogen, belonging to the family of metal nitrides and intermetallic compounds. This material is primarily of research interest rather than established industrial production, with potential applications in semiconductor technology, optoelectronics, and high-performance coatings where the combined properties of indium and silver nitrides could provide benefits such as improved electrical conductivity, thermal stability, or unique optical characteristics.
InAgP is a ternary compound in the indium-silver-phosphorus system, belonging to the class of intermetallic or compound metal phases. This material represents an experimental or specialized composition rather than a commercial alloy, and is primarily of research interest for investigating phase diagrams, crystal structures, and potential applications in semiconductor or optoelectronic device research. The addition of silver to indium phosphide systems may offer opportunities for modified electronic properties or specialized contact materials, though industrial adoption remains limited compared to binary InP or established III-V semiconductor compounds.
InAgP₂S₆ is a layered metal chalcogenide compound combining indium, silver, phosphorus, and sulfur—a material family that bridges metallic and semiconducting properties. This is a research-phase material not yet widely commercialized; compounds in this family are being investigated for applications requiring weak interlayer bonding, tunable electronic properties, or anisotropic mechanical behavior. The material's structural characteristics make it relevant to emerging technologies in nanoelectronics, optoelectronics, and heterostructure engineering where layer-by-layer assembly or exfoliation is desirable.
InAgP2Se6 is a ternary chalcogenide compound combining indium, silver, phosphorus, and selenium—a member of the layered metal chalcogenide family with potential for two-dimensional materials applications. This is a research-stage material studied for its layered crystal structure and exfoliable properties, making it a candidate for emerging applications in nanoelectronics, optoelectronics, and heterogeneous device fabrication where van der Waals materials are explored as alternatives to graphene and transition metal dichalcogenides.
InAgS2 is a ternary metal sulfide compound combining indium, silver, and sulfur, belonging to the family of chalcogenide semiconductors and mixed-metal sulfides. This material is primarily investigated in research contexts for optoelectronic and thermoelectric applications, where the combination of metallic and semiconducting character offers potential advantages in energy conversion and light-emitting device architectures. InAgS2 and related ternary sulfides are of interest to materials scientists exploring alternatives to conventional binary semiconductors, particularly for applications requiring tunable bandgaps or enhanced electrical-thermal coupling.
InAgSe2 is a ternary intermetallic compound combining indium, silver, and selenium, belonging to the chalcogenide alloy family. This material is primarily of research interest for optoelectronic and thermoelectric applications, where its layered crystal structure and semiconductor-like properties make it a candidate for infrared detectors, photovoltaic devices, and solid-state cooling systems. Engineers would consider InAgSe2 in advanced materials development where conventional single-element semiconductors are insufficient, though it remains largely in the experimental phase with limited commercial deployment compared to established III-V or II-VI semiconductor systems.
InAgSnS4 is a quaternary compound in the metal sulfide family, combining indium, silver, tin, and sulfur elements. This material is primarily of research and developmental interest rather than a mature commercial product, with potential applications in semiconductor, optoelectronic, and thermoelectric device research where mixed-metal sulfides offer tunable electronic properties. Engineers would consider this compound when exploring materials for photovoltaic absorbers, ionic conductors, or specialized solid-state devices where the unique combination of elements provides advantages over binary or ternary alternatives in band gap engineering or carrier mobility.
InAlN3 is a ternary III-nitride semiconductor compound containing indium, aluminum, and nitrogen, belonging to the wide-bandgap nitride family used in high-performance electronic and optoelectronic devices. This material is primarily of research and emerging industrial interest for next-generation high-electron-mobility transistors (HEMTs), deep ultraviolet (UV) emitters, and power electronics where its wide bandgap and high breakdown field enable operation at elevated temperatures and voltages. InAlN offers potential advantages over binary GaN and AlN in lattice matching and strain engineering, making it attractive for advanced heterostructure designs in RF power amplifiers, UV photonics, and high-frequency switching applications.
InAsPt5 is an intermetallic compound combining indium, arsenic, and platinum in a 1:1:5 stoichiometry. This is an experimental material primarily of research interest rather than an established commercial alloy; it belongs to the family of platinum-based intermetallics being investigated for high-temperature structural and functional applications. The platinum-rich composition and high density suggest potential use in demanding environments requiring thermal stability, corrosion resistance, and mechanical strength, though practical applications remain limited to specialized research and development contexts.
InAu is an intermetallic compound formed from indium and gold, belonging to the precious metal alloy family. It is primarily investigated in microelectronics and materials research for its potential in semiconductor bonding, contact metallurgy, and high-reliability interconnection systems where the combination of indium's softness and gold's stability offers advantages in thermal and electrical performance. This material remains largely in the research and development phase rather than widespread production use, with interest driven by demands for improved bump bonding in flip-chip assemblies and hybrid integrated circuits where conventional solders face thermal cycling challenges.
InAu₃ is an intermetallic compound formed between indium and gold, belonging to the family of precious metal alloys. This material is primarily of research and specialized industrial interest, valued for applications requiring the combined properties of gold's corrosion resistance and chemical inertness with indium's semiconductor and thermal characteristics. InAu₃ appears in thin-film electronics, bonding applications, and experimental systems where the interaction between these two elements offers advantages over single-metal alternatives, though it remains less common than binary gold alloys in mainstream engineering.
InAuN3 is an intermetallic compound combining indium, gold, and nitrogen, representing an experimental material in the class of ternary metal nitrides. This compound exists primarily in research contexts exploring advanced material properties at the intersection of metallurgy and nitride chemistry. The material's potential applications would leverage properties common to gold-indium systems (high thermal and electrical conductivity, corrosion resistance) combined with the hardness and thermal stability that nitrogen incorporation typically imparts, though industrial deployment remains limited and further characterization is required.
InBiAu is a ternary metal alloy composed of indium, bismuth, and gold. This material belongs to the family of low-melting-point metallic systems and is primarily of research and specialized industrial interest rather than a commodity engineering material. The alloy is notably used in applications requiring low-temperature processing, soft soldering, thermal interface materials, and specialized joining applications where conventional solders are unsuitable; its composition positions it as an alternative to lead-based solders and cadmium-containing systems in temperature-sensitive or biocompatible applications.
InCo2N2 is an intermetallic nitride compound combining indium, cobalt, and nitrogen, representing an experimental material in the high-entropy and refractory compound family. While not yet widely commercialized, materials in this class are of interest for advanced applications requiring high hardness, thermal stability, and chemical resistance, particularly where conventional metal alloys or ceramics fall short. Research on indium-cobalt nitrides focuses on potential use in wear-resistant coatings, catalytic systems, and high-temperature structural applications.
InCo3N is a transition metal nitride compound combining indium and cobalt, belonging to the family of hard ceramic-metal hybrids that exhibit metallic conductivity alongside ceramic hardness and wear resistance. While primarily investigated in research settings, InCo3N and related ternary nitrides are explored for applications requiring high hardness, thermal stability, and chemical resistance—particularly in cutting tools, wear-resistant coatings, and high-temperature structural components where conventional alloys fall short. Its appeal lies in combining the toughness typical of metallic systems with the extreme hardness of ceramic nitrides, making it a candidate material for next-generation tool and protective coating applications.
InCo3SnS2 is an intermetallic compound combining indium, cobalt, tin, and sulfur elements, representing a complex multi-component metallic system with potential for advanced functional applications. This material falls within the realm of research-phase intermetallic compounds and chalcogenides, explored for its unique electronic and mechanical properties that differ from conventional binary or simple ternary alloys. Its dense, stiff structure makes it relevant for applications demanding high modulus and stability, particularly in thermoelectric devices, catalytic systems, or advanced energy storage where multi-element synergy provides performance advantages over traditional alternatives.
InCoN3 is a nickel-based superalloy from the inconel family, likely designed for high-temperature applications requiring exceptional strength and corrosion resistance. The material typically finds use in aerospace propulsion systems, power generation turbines, and chemical processing equipment where sustained elevated-temperature performance is critical. Engineers select InCoN3-class alloys when competing materials cannot meet the combination of creep resistance, oxidation resistance, and mechanical stability demanded in extreme thermal environments.
Inconel 625 made by bound metal deposition is the nickel-chromium-molybdenum-niobium alloy printed from metal-filled polymer filament, then debound and sintered into a metal part. The green part is printed oversize to allow for sintering shrinkage, and the sintered part keeps layer lines, a rougher surface than machined stock, and some porosity. Sagging during sintering limits long unsupported spans, so supports or setters are often needed, and properties can vary with build direction. Typical uses are corrosion-resistant fixtures, housings and fluid-handling parts, and low-volume components for marine, chemical and aerospace service.
Desktop Metal Nickel Alloy IN625 (Studio System 2) is the maker's grade of Inconel 625 printed by bound metal deposition, here in the sintered condition. Alloy powder held in a polymer and wax binder is extruded layer by layer, then debound and furnace-sintered, shrinking substantially, so parts are printed oversized to reach final dimensions. Sintering gives an equiaxed grain structure without the melt-pool texture of laser processes, but leaves some residual porosity, visible layer lines and a rough surface, so functional faces are usually machined. Parts serve as low-volume corrosion- and heat-resistant brackets, fittings, fixtures and prototypes for chemical, marine and energy equipment. Every value on this page is read from Desktop Metal's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Markforged Inconel 625 is the maker's grade of the nickel-chromium-molybdenum alloy printed by bound metal deposition, extruded as a metal-powder-filled polymer filament. The green part is debound and furnace-sintered, shrinking as it densifies, so it is printed oversize. It ends with a sintered grain structure and some closed residual porosity, without the melt-pool structure and residual stress of laser-fused parts. Surfaces show layer lines, and critical features are usually machined. Parts are used for corrosion- and heat-resistant fixtures, tooling, manifolds and low-volume replacement parts in chemical processing, marine and energy equipment. Every value on this page is read from Markforged's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Markforged Inconel 625 is the maker's grade of the nickel-chromium-molybdenum-niobium alloy printed by bound metal deposition, here as a part in the sintered condition. The part is extruded oversized from polymer-bound powder filament, debound to remove the binder and furnace-sintered, shrinking as the powder densifies into a near-dense metal with a sintered grain structure rather than a melt-pool structure. Some residual porosity remains, and layer lines leave a rough surface, so critical faces and holes are usually machined. Printed parts are used for corrosion- and heat-resistant fixtures, tooling, brackets and low-volume functional components in chemical, marine and industrial equipment. Every value on this page is read from Markforged's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Inconel 625 printed by laser powder bed fusion is the nickel-chromium-molybdenum-niobium alloy built layer by layer from fine gas-atomized powder. Rapid solidification gives a fine cellular-dendritic structure with columnar grains along the build direction, so properties can differ between vertical and horizontal builds. Parts have high residual stress and a rough as-built surface, need supports for overhangs, and are usually stress relieved on the plate, then often heat treated, hot isostatically pressed or machined. Printed parts serve as corrosion- and heat-resistant aerospace ducting, combustor components, heat exchangers and chemical-process hardware with complex internal passages.
3D Systems LaserForm Ni625 (A) is a grade of Inconel 625, a nickel-chromium-molybdenum-niobium alloy, made by laser powder bed fusion. As printed, it has a fine cellular solidification structure with columnar grains along the build direction, so its properties differ between build directions. Parts carry residual stress and need supports, so they are usually stress relieved on the build plate, often hot isostatically pressed or solution annealed, and machined where the rough surface matters. Typical parts are corrosion- and heat-resistant heat exchangers, manifolds, combustion hardware and chemical processing components with internal channels. Every value on this page is read from 3D Systems' own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
3D Systems LaserForm Ni625 (A) is that maker's grade of Inconel 625 made by laser powder bed fusion, here in the annealed condition. As printed, the alloy has a fine cellular structure with niobium and molybdenum segregated at cell boundaries, columnar grains along the build direction and high residual stress. Annealing relieves that stress and homogenizes the structure, lowering strength, raising ductility and reducing anisotropy compared with the as-built state, while supports still need removing and functional surfaces machining. It is used for corrosion- and heat-resistant parts with complex internal passages, such as manifolds, heat exchangers and combustion hardware. Every value on this page is read from 3D Systems' own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
3D Systems LaserForm Ni625 (A) is a grade of Inconel 625 printed by laser powder bed fusion, here in the as-built condition without heat treatment. Rapid solidification gives a fine cellular-dendritic structure with niobium and molybdenum segregated to the cell boundaries, inside columnar grains elongated along the build direction, so properties vary with build orientation. Parts carry high residual stress, need supports and have rough surfaces, so printing is usually followed by stress relief, support removal and often machining. Typical uses are heat- and corrosion-resistant parts with internal channels, such as heat exchangers, manifolds and combustion hardware. Every value on this page is read from 3D Systems' own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
3D Systems LaserForm Ni625 (A) is Inconel 625 printed by laser powder bed fusion from that maker's powder grade and then stress-relieved. As printed, it has a fine cellular-dendritic structure with columnar grains along the build direction, giving some anisotropy, and high residual stress. Stress relief, usually done on the build plate, lowers that stress and distortion on removal while largely keeping the as-built grain structure. Overhangs need supports, and the rough surface is often machined where sealing or fatigue matters. Typical parts are complex corrosion- and heat-resistant components such as heat exchangers, manifolds, ducting and exhaust parts. Every value on this page is read from 3D Systems' own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Inconel 625 in the as-built condition is the nickel-chromium-molybdenum-niobium alloy exactly as it leaves the L-PBF machine, before stress relief, hot isostatic pressing or solution treatment. Rapid solidification gives fine cellular-dendritic grains, often elongated along the build direction, with niobium and molybdenum segregated between cells, so properties can vary with orientation. High residual stress can distort parts once they are cut from the plate, and surfaces are rough with supports to remove. The state is mainly a starting point for heat treatment and machining of parts for corrosion- and heat-exposed service, such as ducting and heat exchangers.
Colibrium Additive Nickel 625 is the maker's Inconel 625 grade for laser powder bed fusion, here as-built, without post-print heat treatment. Rapid melt-pool solidification gives a fine cellular-dendritic structure, columnar grains along the build direction and niobium and molybdenum segregation at cell boundaries, making properties orientation-dependent. Parts carry high residual stress, are anchored to the plate by supports and have rough down-facing surfaces, so stress relief, plate removal and often hot isostatic pressing or solution annealing and machining follow. Printed parts serve as heat- and corrosion-resistant components with internal channels, such as heat exchangers and combustion hardware. Every value on this page is read from Colibrium Additive's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Colibrium Additive Nickel 625 is the maker's laser powder bed fusion grade of the nickel-chromium-molybdenum-niobium alloy Inconel 625, here in the stress-relieved condition. Printing gives a fine cellular-dendritic structure with columnar grains along the build direction, interdendritic segregation of molybdenum and niobium, and high residual stress. Stress relief, usually done before parts are cut from the build plate, reduces distortion but largely keeps the as-built structure and its anisotropy between build directions. Supports must still be removed and rough surfaces machined or finished. Typical parts are heat- and corrosion-resistant components with internal passages, such as heat exchangers and manifolds. Every value on this page is read from Colibrium Additive's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
EOS NickelAlloy IN625 is a maker's grade of Inconel 625, a nickel-chromium-molybdenum-niobium alloy, processed by laser powder bed fusion. As built it is near fully dense, with a fine cellular-dendritic structure and columnar grains along the build direction that make properties differ between orientations. Rapid solidification leaves residual stress and niobium segregation, so parts are stress-relieved before removal from the plate and often solution annealed or hot isostatically pressed. Overhangs need supports, and the rough surface is usually machined or polished. Parts serve as corrosion- and heat-resistant components with complex geometry, such as aerospace ducting, heat exchangers and chemical-processing hardware. Every value on this page is read from EOS's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
EOS NickelAlloy IN625 is one maker's grade of the nickel-chromium-molybdenum-niobium alloy Inconel 625 printed by laser powder bed fusion, here in the as-built condition. As built, it has a fine cellular-dendritic structure with columnar grains along the build direction and niobium and molybdenum segregated at cell boundaries. This makes it stronger but less ductile than annealed wrought alloy and gives it properties that differ between build directions. Parts carry high residual stress and a rough surface, need supports on overhangs, and are usually stress relieved before removal from the plate. They are used for corrosion- and heat-resistant manifolds, heat exchangers, ducting and combustion hardware. Every value on this page is read from EOS's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
EOS NickelAlloy IN625 is a maker's powder grade of the nickel-chromium-molybdenum-niobium alloy Inconel 625, printed by laser powder bed fusion and then heat-treated. As built, it has a fine cellular structure with niobium and molybdenum segregated to cell boundaries, columnar grains along the build direction and high residual stress. Heat treatment relieves that stress before parts are cut from the plate and can homogenize the structure, reducing anisotropy, though supports must still be removed and the rough surface usually machined. Typical parts are heat exchangers, combustion and exhaust hardware, ducting and fluid-handling components for aerospace, energy and chemical processing. Every value on this page is read from EOS's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Nikon SLM Solutions IN625 is that maker's grade of the nickel-chromium-molybdenum-niobium alloy Inconel 625 for laser powder bed fusion. As printed, it has a fine cellular-dendritic structure with columnar grains along the build direction, so its properties differ between build orientations. Residual stress calls for stress relief before parts are cut from the plate. This is often followed by solution annealing or hot isostatic pressing, and by machining of the rough surface. Printed parts serve as heat exchangers, combustor and exhaust hardware, and chemical-processing or marine components with intricate internal channels. Every value on this page is read from Nikon SLM Solutions' own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Nikon SLM Solutions IN625 is that maker's grade of Inconel 625, a nickel-chromium-molybdenum-niobium alloy, for laser powder bed fusion, here annealed. As printed it has a fine cellular structure with niobium and molybdenum segregated to cell boundaries, grains elongated along the build direction and high residual stress, so parts need supports and stress relief before removal from the plate. Annealing relieves that stress and dissolves much of the segregation, lowering strength but raising ductility and reducing anisotropy. Parts serve as heat exchangers, combustor and exhaust hardware, manifolds and corrosion-resistant chemical and marine components with internal channels. Every value on this page is read from Nikon SLM Solutions' own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Nikon SLM Solutions IN625 is that maker's grade of Inconel 625 for laser powder bed fusion, here in the as-built condition without heat treatment. Rapid solidification gives a fine cellular-dendritic structure, with niobium and molybdenum segregated to cell boundaries and columnar grains along the build direction. As a result, strength is high, ductility is below annealed wrought material and properties depend on build direction. Parts carry high residual stress and a rough surface, need supports on overhangs and are usually stress relieved, often also solution annealed or hot isostatically pressed. Typical uses are heat exchangers, combustor and exhaust parts, manifolds and chemical-process hardware with internal passages. Every value on this page is read from Nikon SLM Solutions' own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Renishaw In625-0402 is that maker's grade of Inconel 625, a nickel-chromium-molybdenum-niobium alloy, for laser powder bed fusion. Rapid solidification gives a fine cellular structure with niobium and molybdenum segregated to the cell walls, and columnar grains along the build direction make properties differ between orientations. Parts carry high residual stress, so they are stress relieved before removal from the plate and often solution annealed or hot isostatically pressed, then machined where the rough surface matters. Printed parts serve as corrosion- and heat-resistant components with complex internal passages, such as heat exchangers, manifolds and combustion hardware. Every value on this page is read from Renishaw's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Renishaw In625-0402 printed by laser powder bed fusion is the maker's grade of the nickel-based alloy Inconel 625 in the as-built state, without heat treatment. Rapid solidification gives a fine cellular-dendritic microstructure with niobium and molybdenum segregated at cell boundaries and columnar grains along the build direction, so properties are anisotropic. Parts carry high residual stress, need supports and have a rough surface. Stress relief, often hot isostatic pressing or solution annealing, and machining usually follow. It is used for corrosion- and heat-resistant parts such as aerospace exhaust and combustion hardware, heat exchangers and chemical-processing components. Every value on this page is read from Renishaw's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Renishaw In625-0402 is Renishaw's grade of the nickel-chromium-molybdenum-niobium alloy Inconel 625 for laser powder bed fusion, here in the heat-treated condition. As printed, it has a fine cellular structure with niobium and molybdenum segregated at cell boundaries, columnar grains along the build direction and high residual stress, giving direction-dependent properties. Heat treatment relieves that stress before parts are removed from the plate and can homogenize and recrystallize the structure, reducing anisotropy; supports still have to be removed and functional surfaces machined. It is used for corrosion- and heat-resistant parts such as heat exchangers, manifolds and combustor and exhaust components. Every value on this page is read from Renishaw's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Velo3D Inconel 625 is Velo3D's grade of the nickel-chromium-molybdenum-niobium alloy Inconel 625 made by laser powder bed fusion. As printed, it has a fine cellular structure with niobium and molybdenum segregated to the cell walls and columnar grains running along the build direction, so its properties vary with build orientation. Residual stress is high, so parts are stress relieved on the build plate and are often hot isostatically pressed or solution annealed, then machined or finished where the rough surface matters. Typical parts are heat exchangers, rocket engine and combustor components, and manifolds with internal channels for hot, corrosive service. Every value on this page is read from Velo3D's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Velo3D Inconel 625 as-built is the maker's grade of the nickel-chromium-molybdenum-niobium alloy UNS N06625 printed by laser powder bed fusion, with no heat treatment after printing. Rapid solidification gives a fine cellular-dendritic structure with columnar grains along the build direction and niobium and molybdenum segregated to cell boundaries, which makes its properties anisotropic. Parts carry residual stress and a rough surface. They are normally stress relieved before removal from the build plate, often followed by annealing or hot isostatic pressing. Uses include heat exchangers, manifolds and combustion hardware for chemical, marine and aerospace service. Every value on this page is read from Velo3D's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Velo3D Inconel 625 in the HIP condition is that maker's grade of the nickel-chromium-molybdenum-niobium alloy, printed by laser powder bed fusion and then hot isostatically pressed. As printed, it has a fine cellular structure with columnar grains along the build direction, niobium and molybdenum segregated to cell boundaries, and residual stress that needs relief before removal from the plate. HIP closes internal porosity and recrystallizes and homogenizes the structure, which reduces anisotropy, but it leaves the rough as-built surface. Parts serve as corrosion- and heat-resistant aerospace ducting, heat exchangers, combustion hardware and chemical-process fittings. Every value on this page is read from Velo3D's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Velo3D Inconel 625, solution-treated, is that maker's laser powder bed fusion grade of the nickel-chromium-molybdenum-niobium alloy, heat treated after printing. As printed, it has a fine cellular-dendritic structure with niobium and molybdenum segregated to cell boundaries, columnar grains along the build direction and high residual stress. Parts are therefore stress relieved before removal from the build plate. Solution treatment dissolves the segregation and largely recrystallizes the grains, trading some as-built strength for ductility and more uniform properties across build directions. Typical parts are heat exchangers, manifolds and hot-section hardware needing corrosion and oxidation resistance at temperature. Every value on this page is read from Velo3D's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Inconel 718 made by metal binder jetting is the nickel-chromium-iron superalloy formed by binding alloy powder layer by layer, then debinding and sintering the fragile green part. Sintering causes substantial, fairly uniform shrinkage that the design must allow for, and some residual porosity usually remains. With no melt pool, there is little thermal residual stress, less anisotropy than in laser-melted material, and generally no supports, though surfaces are rough. Parts usually need solution treatment and aging, sometimes hot isostatic pressing, and machining of critical features. Typical uses are batches of complex components for high-temperature service, such as turbomachinery and fluid-handling parts.
Desktop Metal Nickel Alloy IN718 (Shop System) in the HIP condition is Inconel 718 printed by metal binder jetting (BJT), sintered and then hot isostatically pressed. Green parts are debound and sintered with substantial shrinkage, giving an equiaxed grain structure without the melt-track texture or residual stress of laser fusion. HIP closes the internal porosity left after sintering, improving ductility and fatigue resistance, though surface-connected pores are not closed. An age-hardening treatment usually follows, and critical surfaces are machined. It is used for complex nickel alloy parts made in batches for high-temperature or corrosive service, such as impellers, nozzles and turbine hardware. Every value on this page is read from Desktop Metal's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Inconel 718 is a nickel-iron-based superalloy strengthened by γ'' (Ni₃Nb) precipitates, used extensively in jet engines, gas turbines, and high-temperature aerospace applications requiring strength retention to ~650°C. The F condition is the as-fabricated state (annealed after final fabrication without precipitation hardening), providing lower strength but superior ductility and machinability compared to aged conditions, making it suitable for applications requiring post-delivery aging or intermediate machining operations.
Inconel 718 printed by laser powder bed fusion is the nickel-chromium-iron superalloy built from fine gas-atomized powder, melted layer by layer under inert gas. Rapid solidification gives a fine cellular-dendritic structure with columnar grains along the build direction, so as-built properties differ between build orientations, and niobium segregates to cell boundaries. Parts carry high residual stress and a rough surface, so they need stress relief on the plate, support removal, solution and aging treatment, often hot isostatic pressing, and machining of critical surfaces. Typical uses are turbine and combustor components, heat exchangers, manifolds and ducts.
LaserForm Ni718 (A) is the 3D Systems grade of Inconel 718 for laser powder bed fusion, a precipitation-hardening nickel superalloy printed from powder into dense parts. As printed, it has a fine cellular-dendritic structure with columnar grains along the build direction, niobium segregation and high residual stress, so parts need supports and stress relief before removal from the build plate. Hot isostatic pressing, solution treatment and ageing then close porosity, precipitate the strengthening phases and reduce anisotropy. Printed parts serve in gas turbine and rocket engine hardware such as combustor parts, fuel nozzles, brackets and heat exchangers. Every value on this page is read from 3D Systems' own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
3D Systems LaserForm Ni718 (A) is that maker's grade of Inconel 718 nickel superalloy processed by laser powder bed fusion, in the as-built condition. Rapid solidification gives a fine cellular-dendritic structure in columnar grains along the build direction, with niobium segregated between cells and little age-hardening precipitation, so properties are anisotropic. Parts carry high residual stress and a rough surface, and are usually stress relieved on the plate, then hot isostatically pressed or solution treated and aged before service. They are used for gas turbine and rocket engine hardware such as combustor parts, fuel nozzles, brackets and heat exchangers. Every value on this page is read from 3D Systems' own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
3D Systems LaserForm Ni718 (A) is a heat-treated grade of the nickel superalloy Inconel 718 made by laser powder bed fusion. As built, the alloy has a fine cellular-dendritic structure with niobium segregation, columnar grains along the build direction and high residual stress, so parts need supports and stress relief. Heat treatment relieves that stress and ages the alloy to precipitate its strengthening phases, though grain texture and some anisotropy between build directions can remain. Parts serve in gas turbine and rocket engine hardware, brackets and heat exchangers that need complex geometry and strength at elevated temperature. Every value on this page is read from 3D Systems' own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Inconel 718 printed by laser powder bed fusion in the as-built condition is the nickel-chromium-iron superalloy as it leaves the machine, before any stress relief, hot isostatic pressing or aging. Rapid melting and solidification give cellular-dendritic grains growing in columns along the build direction, with niobium and molybdenum segregated between dendrites, so properties differ between build and in-plane directions. High residual stress remains and can distort parts when they are removed from the build plate, and the surface is rough with support marks. It is used for prototypes, test coupons and parts that will be heat treated and finished afterward, such as turbine and combustor components.
Colibrium Additive Nickel 718 is a laser powder bed fusion grade of the precipitation-hardenable nickel superalloy Inconel 718, here in the aged condition. As printed, it has a fine cellular-dendritic structure with columnar grains along the build direction, niobium segregation, directional anisotropy and high residual stress, so parts need supports and stress relief before removal from the plate. Aging precipitates the gamma double prime and gamma prime phases that strengthen the alloy, often after solution treatment or hot isostatic pressing. Printed parts serve as turbine and rocket engine components, combustor hardware, manifolds and brackets loaded at elevated temperature. Every value on this page is read from Colibrium Additive's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.
Colibrium Additive Nickel 718 is that maker's grade of Inconel 718 made by laser powder bed fusion, here in the as-built condition without post-build heat treatment. Rapid solidification gives a fine cellular-dendritic structure with columnar grains along the build direction, interdendritic niobium segregation with Laves phase, and little of the strengthening gamma double prime precipitation. Parts carry high residual stress, differ in properties between build directions and have a rough surface, so they are normally stress relieved, hot isostatically pressed, and solution treated and aged. Printed parts are used for gas turbine and rocket engine hardware such as combustor and fuel system components, brackets and heat exchangers. Every value on this page is read from Colibrium Additive's own material data sheet — quoted, cited and dated — and is the maker's statement about printed material, not a measurement by MatWorld; none has yet been reviewed by a person.