GH 3625 Powder
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GH 3625 Powder
| Product | GH 3625 Powder |
| CAS No. | 3526-43-0 |
| Appearance | Gray Powder |
| Purity | ≥99%,  ≥99.9%,  ≥95%(Other purities are also available) |
| APS | 1-5 µM, 10-53 µM  (Can be customized),  Ask for other available size range. |
| Ingredient | Ni-Fe-Cr-Mo |
| Density | N/A |
| Molecular Weight | 213.28g/mol |
| Product Codes | NCZ-DCY-287/25 |
GH 3625 Description:
GH 3526 Powder is one of the numerous advanced ceramic materials manufactured by Nanochemazone. Nanochemazone produces too many standard grades when applicable, including Mil Spec (military grade); ACS, Reagent and Technical Grade; Food, Agricultural and Pharmaceutical Grade; Optical Grade, USP and EP/BP (European Pharmacopoeia/British Pharmacopoeia) and follows applicable ASTM testing standards. Typical and custom packaging is available. Additional technical, research and safety (MSDS) information are available. Please request a quote above for more information on lead time and pricing
GH 3625 Powder Related Information :
Storage Conditions:
Airtight sealed, avoid light and keep dry at room temperature.
Please contact us for customization and price inquiry
Email: contact@nanochemazone.com
Note: We supply different size ranges of Nano and micron as per the client’s requirements and also accept customization in various parameters.
GH3625 powder Inconel 625 powder
GH3625 powder Inconel 625 powder is a Mo-Nb reinforced nickel-based high-temperature alloy.
| Metal Powder | Size | Quantity | Price/kg | Size | Quantity | Price/kg |
| Inconel 625 | 0-20μm | 1KG | $59 | 20-63μm | 1KG | $98.30 |
| 10KG | $39 | 10KG | $69.10 | |||
| 100KG | $34 | 100KG | $64.50 |
Overview
GH3625 powder Inconel 625 powder is an alloy powder used for metal additive manufacturing processes like selective laser sintering (SLS) and direct metal laser sintering (DMLS). It is a nickel-based superalloy that offers high strength, corrosion resistance, and excellent high-temperature properties.
GH3625 is designed specifically for additive manufacturing to produce complex, dense parts with exceptional mechanical properties comparable to wrought materials. It enables the production of lightweight components with complex geometries for aerospace, automotive, medical, and industrial applications.
This guide provides a detailed overview of GH3625 powder covering its composition, properties, applications, specifications, pricing, advantages, and limitations. Comparisons are made to other common alloys like Inconel 718 and Satellite 21 to highlight the performance and suitability of GH3625 for different uses. An FAQ section addresses key questions about this material.
GH3625 powder Inconel 625 powder Composition
GH3625 has a complex chemical composition designed to provide a combination of high strength, resistance to thermal fatigue, oxidation, and corrosion resistance. Here is an overview of its composition:
| Element | Weight % |
| Nickel | Balance |
| Chromium | 15-17% |
| Cobalt | 10% |
| Molybdenum | 8-10% |
| Tantalum | 5-6% |
| Aluminum | 1.2-1.7% |
| Titanium | 0.5-1.2% |
| Boron | 0.01% |
Nickel forms the base of this superalloy providing ductility and toughness. Elements like chromium, cobalt, and molybdenum contribute to high temperature strength through solid solution strengthening.
Tantalum provides solid solution strengthening and forms carbide particles for precipitation hardening. Aluminum and titanium form the gamma prime phase Ni3(Al,Ti) to give excellent high temperature mechanical properties. Boron enhances grain boundary strength.
The balanced composition gives GH3625 powder excellent weldability compared to precipitation hardening stainless steels. It can be easily post-processed through hot isostatic pressing (HIP), heat treatment, and machining.
GH3625 powder Inconel 625 powder Properties
GH3625 powder has the following physical and mechanical properties that make it suitable for demanding applications:
GH3625 powder Inconel 625 powder Properties
| Property | Value |
| Density | 8.1-8.5 g/cc |
| Melting Point | 1260-1335°C |
| Thermal Conductivity | 11-12.5 W/mK |
| Coefficient of Thermal Expansion | 12.5-13.5 x 10<sup>-6</sup>/K |
| Modulus of Elasticity | 156-186 GPa |
| Poission’s Ratio | 0.29-0.33 |
| Tensile Strength | 1050-1280 MPa |
| Yield Strength (0.2% offset) | 860-1050 MPa |
| Elongation | 8-15% |
| Hardness | 32-38 HRC |
The high melting point, thermal conductivity, and low coefficient of thermal expansion enable good dimensional stability under high temperature service environments up to 1000°C for limited periods.
The alloy has excellent tensile and yield strength comparable to wrought materials along with good ductility and fracture toughness. It exhibits high hardness, resistance to wear, galling, and abrasion.
The properties allow GH3625 to outperform stainless steels, cobalt alloys, and even rival precipitation hardening nickel superalloys in high temperature strength. It also offers better weldability than Inconel 718.
GH3625 powder Inconel 625 powder Applications
The combination of high strength, hardness, toughness, and thermal stability makes GH3625 suitable for:
GH3625 powder Inconel 625 powder Applications
| Industry | Components |
| Aerospace | Turbine blades, combustor parts, nozzle guide vanes |
| Automotive | Turbocharger wheels, manifolds, valves |
| Oil and Gas | Wellhead parts, downhole tools, valves |
| Power Generation | Heat exchangers, burner components |
| Chemical Processing | Pump impellers, valves, reaction vessels |
| Medical | Dental implants, prosthetics, surgical instruments |
The ability to 3D print complex geometries allows consolidating multiple parts into single components and lightweight lattice structures. This enables faster printing of single-piece components versus assembling multiple sections.
GH3625 is used to print blades, impellers, plates, discs, tubes with conformal cooling channels, and other mission-critical components working under high pressures and temperatures.
GH3625 powder Inconel 625 powder Specifications
GH3625 powder for AM processes is available in different size distributions, shapes, and formulations from various powder manufacturers.
GH3625 Powder Types
| Specification | Details |
| Particle Size Distribution | 15-45 μm, 15-53 μm, 53-150 μm |
| Particle Shape | Spherical, satellite, polyhedral |
| Alloy Modifications | With B, C, Zr, Nb, Ta |
| Manufacturing Method | Gas atomization, plasma atomization |
Gas atomization and plasma atomization produce spherical powders optimal for SLS/DMLS processes. Satellite powders have higher tap density and improve powder flowability.
Smaller 15-45 μm powders provide high resolution and surface finish while larger 53-150 μm allow faster build speeds. Different alloying additions like boron, carbon, zirconium, niobium, and tantalum are used to tailor material properties.
GH3625 powder Inconel 625 powder Standards
| Standard | Description |
| ASTM F3056 | Standard specification for additive manufacturing nickel alloy |
| AMS7016 | Nickel alloy powder for high temperature service |
| ASME B46.1 | Surface texture requirements |
GH3625 powder is qualified based on composition limits, particle size distribution, morphology, flowability, apparent density, and microstructure per ASTM F3056. Additional testing as per application standards is required.
GH3625 powder Inconel 625 powder Pros and Cons
GH3625 has the following advantages that make it a popular choice:
GH3625 Pros
Excellent strength and hardness up to 1000°C
Good corrosion and oxidation resistance
Weldable for post-processing
Higher ductility than Inconel 718
Can be age hardened by heat treatment
Complex geometries enabled by AM
Faster and cheaper than castings
Reduces part count through consolidation
More expensive than stainless steels
Lower strength than Inconel 718 above 550°C
Susceptible to strain-age cracking
Requires hot isostatic pressing (HIP)
Difficult to machine – requires specialist tools
Limited supplier data on long term performance
Proper selection of AM process parameters and post-processing mitigates some of the limitations of GH3625 powder.
Comparison of GH3625 powder Inconel 625 powder with Inconel 718 and Satellite 21
GH3625 occupies a niche between Inconel 718 and Satellite 21 in terms of properties and cost:
Alloy Comparison
| Property | GH3625 | Inconel 718 | Satellite 21 |
| Cost | Medium | High | Low |
| Density | High | Medium | High |
| Strength | Medium | Very High | Medium |
| Hardness | High | Medium | Very High |
| Wear Resistance | Medium | Low | Very High |
| Corrosion Resistance | Medium | High | Medium |
| Oxidation Resistance | Medium | High | Medium |
| Thermal Stability | Up to 1000°C | Up to 700°C | Up to 900°C |
| Weldability | Good | Poor | Medium |
| Manufacturability | Medium | Difficult | Easy |
GH3625 matches or exceeds the performance of Satellite 21 cobalt alloys in wear and corrosion resistance but at lower cost. It approaches the strength of Inconel 718 up to 550°C and offers better weldability and manufacturability.
This makes it a cost-effective alternative for many applications requiring performance between these standard alloys. The ability to 3D print complex geometries also gives it an edge.
GH3625 powder Inconel 625 powder – FAQs
Q: What is GH3625 powder?
A: GH3625 is a nickel-based superalloy powder specifically designed for additive manufacturing processes like selective laser sintering (SLS) and direct metal laser sintering (DMLS). It provides an excellent combination of high temperature strength, hardness, wear and corrosion resistance.
Q: What is GH3625 powder used for?
A: GH3625 powder is used to 3D print critical components like turbine blades, manifolds, impellers, heat exchangers that require high mechanical properties, dimensional stability, and thermal resistance up to 1000°C. It finds applications across aerospace, automotive, energy, chemical processing, and medical industries.
Q: What metal 3D printing processes use GH3625 powder?
A: Selective laser sintering (SLS) and direct metal laser sintering (DMLS) are powder bed fusion 3D printing processes commonly used with GH3625 powder. Binder jetting is also suitable for GH3625.
Q: What are the material properties of GH3625?
A: GH3625 has excellent tensile strength 1050-1280 MPa, yield strength 860-1050 MPa, and hardness 32-38 HRC similar to wrought materials. It has good ductility of 8-15% elongation and high resistance to wear, galling, abrasion, and corrosion. Thermal properties allow use up to 1000°C.
Q: Does GH3625 powder require heat treatment?
A: Yes, GH3625 parts printed using SLS/DMLS require hot isostatic pressing (HIP) followed by heat treatment to achieve optimal mechanical properties, material consolidation, and microstructure. HIP helps close internal pores and voids.
Q: Is GH3625 weldable?
A: GH3625 is designed to have excellent weldability compared to precipitation hardening stainless steels and Inconel 718. This allows repairing and joining AM GH3625 parts through welding. Stress relieving may be required after welding to prevent cracking.
Q: Is GH3625 machinable?
A: GH3625 is difficult to machine compared to stainless steel and requires high-speed machining with specialist carbide tools. Tool wear is higher so optimal feeds, speeds, and tool paths are necessary.
Q: How much does GH3625 powder cost?
A: GH3625 typically costs between $90-250 per kg based on order size, particle size distribution, manufacturing method, and additional testing/qualification requirements. It is more expensive than stainless steel powders but lower cost than Inconel 718.
Description
Description
Note: For pricing & ordering information, please get in touch with us at sales@nanochemazone.com
Please contact us for quotes on Larger Quantities and customization. E-mail: contact@nanochemazone.com
Customization:
If you are planning to order large quantities for your industrial and academic needs, please note that customization of parameters (such as size, length, purity, functionalities, etc.) is available upon request.
NOTE:
Images, pictures, colors, particle sizes, purity, packing, descriptions, and specifications for the real and actual goods may differ. These are only used on the website for the purposes of reference, advertising, and portrayal. Please contact us via email at sales@nanochemazone.com or by phone at (+1 780 612 4177) if you have any questions.
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GH3536 Alloy Powder
GH3536 Alloy Powder
| Product | GH3536 Alloy Powder |
| CAS No. | N/A |
| Appearance | Â Gray to Metallic Silver Powder |
| Purity | ≥99%,  ≥99.9%,  ≥95%(Other purities are also available) |
| APS | 1-5 µM, 10-53 µM  (Can be customized),  Ask for other available size range. |
| Ingredient | Ni-Cr-Mo-Co-W |
| Density | 8.3g/cm3 |
| Molecular Weight | N/A |
| Product Codes | NCZ-DCY-286/25 |
GH3536 Alloy Description:
GH3536 Alloy Powder is one of the numerous advanced ceramic materials manufactured by Nanochemazone. Nanochemazone produces too many standard grades when applicable, including Mil Spec (military grade); ACS, Reagent and Technical Grade; Food, Agricultural and Pharmaceutical Grade; Optical Grade, USP and EP/BP (European Pharmacopoeia/British Pharmacopoeia) and follows applicable ASTM testing standards. Typical and custom packaging is available. Additional technical, research and safety (MSDS) information are available. Please request a quote above for more information on lead time and pricingGH3536 Alloy Powder Related Information :
Storage Conditions: Airtight sealed, avoid light and keep dry at room temperature. Please contact us for customization and price inquiry Email: contact@nanochemazone.com Note: We supply different size ranges of Nano and micron as per the client’s requirements and also accept customization in various parameters. GH3536 Alloy Powder GH3536 alloy powder is a nickel-based superalloy powder used for additive manufacturing applications requiring high strength and corrosion resistance at elevated temperatures. As an advanced powder metallurgy product, GH3536 allows complex geometries to be fabricated using laser or electron beam-based metal 3D printing processes. GH3536 alloy powder was designed specifically for additive manufacturing, using composition optimization and powder atomization techniques to achieve superior properties compared to conventional nickel superalloys. The key features of GH3536 alloy powder include: High strength at temperatures up to 760°C (1400°F) Oxidation and corrosion resistance in harsh environments Excellent thermal fatigue life and crack growth resistance Good printability and low porosity in printed parts Can be age hardened to optimize strength and ductility The combination of properties make GH3536 suitable for aerospace, power generation, oil & gas, and chemical processing components exposed to extreme temperatures and stresses. Both new part fabrication and repair of worn components can benefit from using this advanced powder. GH3536 Alloy Powder Composition GH3536 has a complex composition designed to provide an optimal balance of properties. The nominal composition is shown below:| Element | Weight % |
| Nickel (Ni) | Balance |
| Chromium (Cr) | 13.5 – 16.0 |
| Cobalt (Co) | 12.0 – 15.0 |
| Tungsten (W) | 5.0 – 7.0 |
| Tantalum (Ta) | 3.0 – 5.0 |
| Aluminum (Al) | 2.8 – 3.8 |
| Titanium (Ti) | 0.5 – 1.5 |
| Niobium (Nb) | 0.5 – 1.5 |
| Hafnium (Hf) | 0.2 – 0.8 |
| Carbon (C) | 0.05 – 0.15 |
| Boron (B) | 0.01 – 0.03 |
| Zirconium (Zr) | 0.01 – 0.05 |
| Property | As-printed | Aged |
| Tensile Strength | 1050 – 1250 MPa (152 – 181 ksi) | 1275 – 1400 MPa (185 – 203 ksi) |
| Yield Strength (0.2% offset) | 900 – 1100 MPa (131 – 160 ksi) | 1150 – 1300 MPa (167 – 189 ksi) |
| Elongation | 25 – 35% | 16 – 22% |
| Hardness | 32 – 38 HRC | 36 – 43 HRC |
| Property | Typical Value |
| Density | 8.3 g/cm3 |
| Melting Point | 1310°C (2390°F) |
| Property | Temperature |
| Coefficient of Thermal Expansion | 12.8 x 10-6/°C at 20-100°C |
| Thermal Conductivity | 11.4 W/m-K at 20°C |
| Specific Heat | 0.43 J/g-°C at 20°C |
| Powder Size Distribution | |
| D10 | 10 μm |
| D50 | 25 μm |
| D90 | 45 μm |
| Powder Classes | Nominal Flow Rate | Apparent Density |
| Class I | 25 s | 2.5 g/cm3 |
| Class II | 28 s | 2.8 g/cm3 |
| Class III | 32 s | 3.2 g/cm3 |
GH4169 Powder
GH4169 Powder
| Product | GH4169 Powder |
| CAS No. | 7440-02-0 |
| Appearance | Gray Dull Silver Powder |
| Purity | ≥99%,  ≥99.9%,  ≥95%(Other purities are also available) |
| APS | 1-5 µM, 10-53 µM  (Can be customized),  Ask for other available size range. |
| Ingredient | NiCr22Mo9Nb |
| Density | 8.19g/cm3 |
| Molecular Weight | N/A |
| Product Codes | NCZ-DCY-289/25 |
GH4169 Description:
GH4169 Powder is one of the numerous advanced ceramic materials manufactured by Nanochemazone. Nanochemazone produces too many standard grades when applicable, including Mil Spec (military grade); ACS, Reagent and Technical Grade; Food, Agricultural and Pharmaceutical Grade; Optical Grade, USP and EP/BP (European Pharmacopoeia/British Pharmacopoeia) and follows applicable ASTM testing standards. Typical and custom packaging is available. Additional technical, research and safety (MSDS) information are available. Please request a quote above for more information on lead time and pricingGH4169 Powder Related Information :
Storage Conditions: Airtight sealed, avoid light and keep dry at room temperature. Please contact us for customization and price inquiry Email: contact@nanochemazone.com Note: We supply different size ranges of Nano and micron as per the client’s requirements and also accept customization in various parameters. GH4169 Powder for Additive Manufacturing GH4169 powder is a precipitation hardening stainless steel powder designed to provide high strength, hardness and corrosion resistance after heat treatment. It contains 17% chromium along with nickel, aluminum, titanium, and niobium additions for enhanced mechanical and corrosion properties. GH4169 powder is a precipitation hardening stainless steel powder designed to provide high strength, hardness and corrosion resistance after heat treatment. It contains 17% chromium along with nickel, aluminum, titanium, and niobium additions for enhanced mechanical and corrosion properties.| Size Range | 15-45um/15-53um/20-63 um | 45-105um |
| Form | Spherical | Spherical |
| Flow Ability | ≤25s | |
| Apparent Density | ≥4.0 g/c㎡ | |
| Oxygen Content | ≤200 ppm | |
| Nitrogen Content | ≤150ppm | |
| Properties | Details |
| Composition | Fe-17Cr-4Ni-1.5Ti-0.7Al-0.25Nb alloy |
| Density | 7.9 g/cc |
| Particle shape | Irregular, angular |
| Size range | 10-150 microns |
| Apparent density | Up to 50% of true density |
| Flowability | Moderate |
| Strength | Very high after aging treatment |
| Corrosion resistance | Excellent, including marine environments |
| Element | Weight % |
| Iron (Fe) | Balance |
| Chromium (Cr) | 16-18% |
| Nickel (Ni) | 3.5-5.5% |
| Titanium (Ti) | 1.2-1.8% |
| Aluminum (Al) | 0.3-1.2% |
| Niobium (Nb) | 0.15-0.45% |
| Carbon (C) | 0.04% max |
| Silicon (Si), Manganese (Mn) | 1% max each |
| Property | Values |
| Density | 7.9 g/cc |
| Melting point | 1400-1450°C |
| Electrical resistivity | 0.80 μΩ-m |
| Thermal conductivity | 12 W/mK |
| Thermal expansion | 12 x 10^-6 /K |
| Maximum service temperature | 650°C |
| Property | Condition | Values |
| Hardness | Solution annealed | 90 HRB |
| Hardness | Peak aged | 40-45 HRC |
| Tensile strength | Annealed | 550-750 MPa |
| Tensile strength | Peak aged | 1300-1600 MPa |
| Yield strength | Peak aged | 1100-1400 MPa |
| Elongation | Peak aged | 8-13% |
| Industry | Example Uses |
| Aerospace | Airframe and engine components, fasteners |
| Marine | Shafts, fixtures, solenoids, valves |
| Nuclear | Fuel element cladding, internal structures |
| Oil and gas | Structural parts for wellheads, offshore platforms |
| Chemical | Process equipment like vessels and pipes |
| Standard | Description |
| AMS 5922 | Precipitation hardening stainless steel powder for aerospace parts |
| ASTM A580 | Standard for precipitation hardening stainless steel wire |
| ASTM A638 | Standard for precipitation hardening iron-based superalloys |
| AMS 5898 | Bars, forgings, rings of precipitation hardening stainless steels |
| Particle Size | Characteristics |
| 10-22 microns | Ultrafine grade for high density |
| 22-75 microns | Most commonly used size range |
| 75-150 microns | Coarser sizes for improved flowability |
| Apparent density | Details |
| Up to 50% of true density | For irregular powder morphology |
| 4.5-5.5 g/cc | Higher for spherical powders |
| Method | Details |
| Gas atomization | High pressure inert gas breaks up molten metal stream into fine droplets |
| Water atomization | High pressure water jet breaks metal into fine particles |
| Vacuum induction melting | High purity input materials melted under vacuum |
| Multiple remelting | Improves chemical homogeneity |
| Sieving | Classifies powder into different particle size ranges |
| Recommendation | Reason |
| Ensure proper ventilation | Prevent exposure to fine metallic particles |
| Avoid ignition sources | Powder can combust in oxygen atmosphere |
| Follow safe protocols | Reduce health and fire hazards |
| Use non-sparking tools | Prevent possibility of ignition |
| Store sealed containers | Prevent contamination or oxidation |
| Test | Details |
| Chemical analysis | ICP and XRF verify composition |
| Particle size analysis | Determines particle size distribution |
| Apparent density | Measured as per ASTM B212 standard |
| Powder morphology | SEM imaging of particle shape |
| Flow rate testing | Gravity flow rate through specified funnel |
| Loss on ignition | Determines moisture content |
| Parameter | GH4169 | 17-4PH | 15-5PH |
| Density | 7.9 g/cc | 7.7 g/cc | 7.8 g/cc |
| Hardness | 40-45 HRC | 38-45 HRC | 36-42 HRC |
| Tensile strength | 1300-1600 MPa | 1200-1450 MPa | 1050-1400 MPa |
| Corrosion resistance | Excellent | Very good | Good |
| Cost | High | Moderate | Low |
GH4169 Powder
GH4169 Powder
| Product | GH4169 Powder |
| CAS No. | 7440-02-0 |
| Appearance | Gray Dull Silver Powder |
| Purity | ≥99%,  ≥99.9%,  ≥95%(Other purities are also available) |
| APS | 1-5 µM, 10-53 µM  (Can be customized),  Ask for other available size range. |
| Ingredient | NiCr22Mo9Nb |
| Density | 8.19g/cm3 |
| Molecular Weight | N/A |
| Product Codes | NCZ-DCY-290/25 |
GH4169 Description:
GH4169 Powder is one of the numerous advanced ceramic materials manufactured by Nanochemazone. Nanochemazone produces too many standard grades when applicable, including Mil Spec (military grade); ACS, Reagent and Technical Grade; Food, Agricultural and Pharmaceutical Grade; Optical Grade, USP and EP/BP (European Pharmacopoeia/British Pharmacopoeia) and follows applicable ASTM testing standards. Typical and custom packaging is available. Additional technical, research and safety (MSDS) information are available. Please request a quote above for more information on lead time and pricingGH4169 Powder Related Information :
Storage Conditions: Airtight sealed, avoid light and keep dry at room temperature. Please contact us for customization and price inquiry Email: contact@nanochemazone.com Note: We supply different size ranges of Nano and micron as per the client’s requirements and also accept customization in various parameters. GH4169 powder for metal 3d Printing GH4169 is a Nb-Mo reinforced nickel-based high-temperature alloy. Its normal working environment is 253-650C. It has good mechanical properties below 650C. Under special circumstances, GH4169 can be used at 800°C for a short period of time.| Metal Powder | Size | Quantity | Price/kg | Size | Quantity | Price/kg |
| Inconel 718 | 0-20μm | 1KG | 60.9 | 53-105μm | 1KG | 59 |
| 10KG | 39.8 | 10KG | 38 | |||
| 100KG | 34.5 | 100KG | 33 |
| Size range | Size distribution | Hall flow rate | Bulk density | Tap density | ||
| D10(μm) | D50(μm) | D90(μm) | ||||
| 15-53μm | 17-22 | 32-38 | 52-58 | ≤18s/50g | ≥4.20g/cm³ | ≥4.80g/cm³ |
| 815°C high temperature durability performance | |||
| Constant stress (δ/Mpa) | Duration(t/h) | Elongation after break(δ5/%) | |
| 690 | 80 | 5 | |
| Test temperature | Tensile strength (σb/Mpa) | Yield strength (σp0.2/Mpa) | Elongation (δ5/%) |
| 25℃ | 1270 | 1030 | 12 |
| 650℃ | 1000 | 860 | 12 |
| Element | C | Cr | Ni | Co | Nb | Mo |
| wt％ | 0.02-0.06 | 17.00-21.00 | 50.00-55.00 | ≤1.00 | 4.75-5.50 | 2.80-3.30 |
| Element | Al | Ti | Fe | B | Mg | Mn |
| wt％ | 0.20-0.80 | 0.65-1.15 | Bal | ≤0.006 | ≤0.010 | ≤0.35 |
| Element | Si | P | S | Cu | O | N |
| wt％ | ≤0.35 | ≤0.015 | ≤0.015 | ≤0.30 | ≤0.020 | ≤0.015 |
GH5188 Powder
GH5188 Powder
| Product | GH5188 Powder |
| CAS No. | N/A |
| Appearance | Metallic Gray or Dark Gray Powder |
| Purity | ≥99%,  ≥99.9%,  ≥95%(Other purities are also available) |
| APS | 1-5 µM, 10-53 µM  (Can be customized),  Ask for other available size range. |
| Ingredient | CoCrNiW |
| Density | 9.10g/cm3 |
| Molecular Weight | N/A |
| Product Codes | NCZ-DCY-291/25 |
GH5188 Description:
GH5188 Powder is one of the numerous advanced ceramic materials manufactured by Nanochemazone. Nanochemazone produces too many standard grades when applicable, including Mil Spec (military grade); ACS, Reagent and Technical Grade; Food, Agricultural and Pharmaceutical Grade; Optical Grade, USP and EP/BP (European Pharmacopoeia/British Pharmacopoeia) and follows applicable ASTM testing standards. Typical and custom packaging is available. Additional technical, research and safety (MSDS) information are available. Please request a quote above for more information on lead time and pricingGH5188 Powder Related Information :
Storage Conditions: Airtight sealed, avoid light and keep dry at room temperature. Please contact us for customization and price inquiry Email: contact@nanochemazone.com Note: We supply different size ranges of Nano and micron as per the client’s requirements and also accept customization in various parameters. GH5188 Powder GH5188 is a W-strengthened diamond-based high-temperature alloy. GH5188 has good mechanical properties and excellent high temperature oxidation resistance. It is suitable for aviation parts that require tensile strength below 980°C and oxidation resistance below 1100°C. GH5188 is a W-strengthened diamond-based high-temperature alloy. GH5188 has good mechanical properties and excellent high temperature oxidation resistance. It is suitable for aviation parts that require tensile strength below 980°C and oxidation resistance below 1100°C. Physical Properties| Size range | Size distribution | Hall flow rate | Bulk density | Tap density | ||
| D10(μm) | D50(μm) | D90(μm) | ||||
| 15-53μm | 17-22 | 32-38 | 52-58 | ≤18s/50g | ≥4.80g/cm³ | ≥5.40g/cm³ |
| Test temperature | Tensile strength (σb/Mpa) | Yield strength (σp0.2/Mpa) | Elongation (δ5/%) |
| 25℃ | 900 | 400 | ≥45 |
| 650℃ | 650 | 280 | ≥50 |
| 900℃ | 300 | 240 | ≥50 |
| 950℃ | 200 | 170 | ≥50 |
| 1000℃ | 160 | 130 | ≥50 |
| Element | C | Cr | Ni | Co | W | Fe |
| wt％ | 0.05-0.15 | 20.00-24.00 | 20.00-24.00 | Bal | 13.00-16.00 | ≤3.00 |
| Element | B | La | Mn | Si | P | S |
| wt％ | ≤0.015 | 0.03-0.12 | ≤1.25 | 0.20-0.50 | ≤0.02 | ≤0.015 |
| Element | Cu | O | N | – | – | – |
| wt％ | ≤0.07 | ≤0.025 | ≤0.015 | – | – | – |
Hastelloy X Powder
Hastelloy X Powder
| Product | Hastelloy X Powder |
| CAS No. | N/A |
| Appearance | Silvery-Gray  Powder |
| Purity | ≥99%,  ≥99.9%,  ≥95%(Other purities are also available) |
| APS | 1-5 µM, 10-53 µM  (Can be customized),  Ask for other available size range. |
| Ingredient | NiCrMoFe |
| Density | 8.22g/cm3 |
| Molecular Weight | N/A |
| Product Codes | NCZ-DCY-276/25 |
Hastelloy X Description:
Hastelloy X Powder is one of the numerous advanced ceramic materials manufactured by Nanochemazone. Nanochemazone produces too many standard grades when applicable, including Mil Spec (military grade); ACS, Reagent and Technical Grade; Food, Agricultural and Pharmaceutical Grade; Optical Grade, USP and EP/BP (European Pharmacopoeia/British Pharmacopoeia) and follows applicable ASTM testing standards. Typical and custom packaging is available. Additional technical, research and safety (MSDS) information are available. Please request a quote above for more information on lead time and pricingHastelloy X Powder Related Information :
Storage Conditions: Airtight sealed, avoid light and keep dry at room temperature. Please contact us for customization and price inquiry Email: contact@nanochemazone.com Note: We supply different size ranges of Nano and micron as per the client’s requirements and also accept customization in various parameters. Best Hastelloy X Powder丨High temperature alloy Powder for 3D Printing Hastelloy X Powder holds a special place. It’s a nickel-based superalloy that has an extraordinary blend of properties, thanks to its composition which includes chromium, iron, and molybdenum. The high nickel content offers exceptional resistance to oxidation and corrosion. Overview of Hastelloy X Powder Hastelloy X is a nickel-based superalloy powder known for its excellent high temperature strength, oxidation resistance, and fabricability. It has applications in the aerospace, industrial, and energy industries where parts are exposed to extreme environments. This article provides a comprehensive guide to Hastelloy X powder. It covers the composition, properties, applications, specifications, suppliers, handling, inspection, comparisons, pros and cons, and frequently asked questions about this versatile alloy powder. Quantitative data is presented in easy-to-read tables for quick reference. Composition of Hastelloy X Powder Hastelloy X has a complex composition optimized for high temperature performance. The main alloying elements are nickel, chromium, iron, and molybdenum.| Element | Weight % | Role |
| Nickel | Balance | Matrix element, provides corrosion resistance |
| Chromium | 21.5 – 23.5 | Oxidation resistance, formation of protective Cr2O3 |
| Iron | 17 – 20 | Solid solution strengthening |
| Molybdenum | 8 – 10 | Solid solution strengthening, creep resistance |
| Cobalt | 1 max | Enhances hot workability |
| Manganese | 1 max | Deoxidizer |
| Silicon | 0.5 max | Deoxidizer |
| Carbon | 0.15 max | Carbide former |
| Property | Description |
| High temperature strength | Excellent creep rupture strength up to 1150°C |
| Oxidation resistance | Resists oxidation in air up to 1200°C |
| Thermal fatigue resistance | Resists cracking during thermal cycling |
| Fabricability | Easy to form and weld compared to other superalloys |
| Corrosion resistance | Resists many oxidizing and reducing environments |
| Industry | Applications |
| Aerospace | Jet engine combustion liners, afterburners, exhaust parts |
| Industrial | Reformer tubes, heat treatment equipment |
| Energy | Nuclear & fossil fuel power generation, chemical processing |
| Automotive | Exhaust system components, turbocharger parts |
| Parameter | Specification |
| Alloy grades | Hastelloy X, B3, BC3, BN |
| Particle size | 15-45 microns, 45-105 microns |
| Particle shape | Spherical, irregular morphology |
| Apparent density | 2.5-4.5 g/cc |
| Tap density | 4-6 g/cc |
| Purity | >99.9% |
| Oxygen content | <1000 ppm |
| Moisture content | <0.2% |
| Test Method | Parameters Checked |
| Sieve analysis | Particle size distribution |
| Apparent density | Powder flowability |
| Tap density | Packed density |
| Scanning electron microscopy | Particle morphology |
| Energy dispersive X-ray | Chemistry, alloy composition |
| X-ray diffraction | Phases present |
| Inductively coupled plasma | Trace element analysis |
| Alloy | Oxidation Resistance | Fabricability | Cost |
| Hastelloy X | Excellent | Good | High |
| Inconel 625 | Good | Excellent | Medium |
| Haynes 230 | Excellent | Poor | Very High |
| Inconel 718 | Medium | Fair | Medium |
| Pros | Cons |
| Excellent high temperature strength | Expensive compared to stainless steels |
| Outstanding oxidation resistance | Lower fabricability than Inconel 625 |
| Thermal fatigue resistance | Susceptible to embrittlement at lower temperatures |
| Ease of welding and machining | Requires controlled handling and processing |
| Resists many corrosive environments | Limited data available compared to popular alloys |
IN939 Powder
IN939 Powder
| Product | IN939 Powder |
| CAS No. | N/A |
| Appearance | Gray Powder |
| Purity | ≥99%,  ≥99.9%,  ≥95%(Other purities are also available) |
| APS | 1-5 µM, 10-53 µM  (Can be customized),  Ask for other available size range. |
| Ingredient | C6H6N6O6 |
| Density | 8.15g/cm3 |
| Molecular Weight | N/A |
| Product Codes | NCZ-DCY-280/25 |
IN939 Description:
IN939 Powder is one of the numerous advanced ceramic materials manufactured by Nanochemazone. Nanochemazone produces too many standard grades when applicable, including Mil Spec (military grade); ACS, Reagent and Technical Grade; Food, Agricultural and Pharmaceutical Grade; Optical Grade, USP and EP/BP (European Pharmacopoeia/British Pharmacopoeia) and follows applicable ASTM testing standards. Typical and custom packaging is available. Additional technical, research and safety (MSDS) information are available. Please request a quote above for more information on lead time and pricingIN939 Powder Related Information :
Storage Conditions: Airtight sealed, avoid light and keep dry at room temperature. Please contact us for customization and price inquiry Email: contact@nanochemazone.com Note: We supply different size ranges of Nano and micron as per the client’s requirements and also accept customization in various parameters. Best IN939 Powder for 3D Printing in 2024 IN939 powder is a nickel-based superalloy that exhibits exceptional mechanical properties and high resistance to corrosion and oxidation. It is primarily composed of nickel, chromium, cobalt, molybdenum, and tantalum. This composition gives IN939 powder its remarkable strength, heat resistance, and stability at elevated temperatures. Overview of IN939 Powder for 3D Printing IN939 is a high-performance nickel-based superalloy powder designed for additive manufacturing of critical components needing exceptional mechanical properties at high temperatures. This article provides a comprehensive guide to IN939 powder for 3D printing applications across aerospace, automotive, energy and industrial sectors. Key aspects covered include IN939 composition, properties, print parameters, applications, specifications, suppliers, handling, inspection, comparisons to alternatives, advantages and limitations, and frequently asked questions. Quantitative data is presented in easy-to-reference tables. Composition of IN939 Powder IN939 has a complex precipitation hardening alloy composition:| Element | Weight % | Purpose |
| Nickel | Balance | Principal matrix element |
| Chromium | 15 – 18 | Oxidation resistance |
| Aluminum | 3.8 – 4.8 | Precipitation hardening |
| Titanium | 0.9 – 1.4 | Precipitation hardening |
| Cobalt | 12 – 15 | Solid solution strengthening |
| Tantalum | 3.8 – 4.8 | Carbide former |
| Carbon | 0.05 – 0.15 | Carbide former |
| Boron | 0.006 – 0.012 | Grain boundary strengthener |
| Property | Description |
| High strength | Excellent tensile and creep rupture strength up to 1050°C |
| Thermal stability | Strength maintained up to 1000°C |
| Creep resistance | High stress-rupture life at high temperatures |
| Oxidation resistance | Forms protective Cr2O3 oxide scale |
| Thermal fatigue resistance | Resists cracking during thermal cycling |
| Phase stability | Microstructure stable after prolonged exposures |
| Corrosion resistance | Resistant to hot corrosion, oxidation, sulfidation |
| Parameter | Typical value | Purpose |
| Layer thickness | 20-50 μm | Resolution vs build speed |
| Laser power | 250-500 W | Sufficient melting without evaporation |
| Scan speed | 800-1200 mm/s | Density vs production rate |
| Hatch spacing | 100-200 μm | Mechanical properties |
| Support structure | Minimal | Easy removal |
| Hot isostatic pressing | 1160°C, 100 MPa, 3h | Eliminate porosity |
| Industry | Components |
| Aerospace | Turbine blades, vanes, combustors |
| Power generation | Hot gas path parts, heat exchangers |
| Automotive | Turbocharger wheels, valves |
| Chemical processing | Pumps, valves, reaction vessels |
| Parameter | Specification |
| Particle size | 15-45 μm typical |
| Particle shape | Spherical morphology |
| Apparent density | > 4 g/cc |
| Tap density | > 6 g/cc |
| Hall flow rate | > 23 sec for 50 g |
| Purity | >99.9% |
| Oxygen content | <100 ppm |
| Method | Parameters Tested |
| Sieve analysis | Particle size distribution |
| SEM imaging | Particle morphology |
| EDX | Chemistry and composition |
| XRD | Phases present |
| Pycnometry | Density |
| Hall flow rate | Powder flowability |
| Alloy | High Temperature Strength | Cost | Printability | Ductility |
| IN939 | Excellent | High | Excellent | Low |
| IN738 | Good | Medium | Excellent | Medium |
| IN718 | Fair | Low | Good | Excellent |
| Hastelloy X | Excellent | High | Fair | Medium |
| Pros | Cons |
| Exceptional high temperature strength | Expensive compared to IN718 |
| Excellent oxidation and creep resistance | Significant parameter optimization needed |
| Complex geometries feasible | Limited room temperature ductility |
| Faster processing than cast/wrought | Controlled storage and handling environment |
| Comparable properties to cast alloy | Difficult to machine after printing |
Inconel 718 Powder
Inconel 718 Powder
| Product | Inconel 718 Powder |
| CAS No. | 7440-02-0 |
| Appearance | Gray Metallic  Powder |
| Purity | ≥99%,  ≥99.9%,  ≥95%(Other purities are also available) |
| APS | 1-5 µM, 10-53 µM  (Can be customized),  Ask for other available size range. |
| Ingredient | Ne-Fe-Cr |
| Density | 8.19g/cm3 |
| Molecular Weight | N/A |
| Product Codes | NCZ-DCY-277/25 |
Inconel 718 Description:
Inconel 718 Powder is one of the numerous advanced ceramic materials manufactured by Nanochemazone. Nanochemazone produces too many standard grades when applicable, including Mil Spec (military grade); ACS, Reagent and Technical Grade; Food, Agricultural and Pharmaceutical Grade; Optical Grade, USP and EP/BP (European Pharmacopoeia/British Pharmacopoeia) and follows applicable ASTM testing standards. Typical and custom packaging is available. Additional technical, research and safety (MSDS) information are available. Please request a quote above for more information on lead time and pricingInconel 718 Powder Related Information :
Storage Conditions: Airtight sealed, avoid light and keep dry at room temperature. Please contact us for customization and price inquiry Email: contact@nanochemazone.com Note: We supply different size ranges of Nano and micron as per the client’s requirements and also accept customization in various parameters. Best in718 powder inconel 718 powder for metal 3D printing inconel 718 powder Overview Inconel 718 powder is a high-performance alloy powder used in additive manufacturing (AM) processes, such as laser powder bed fusion (LPBF) and electron beam powder bed fusion (EBPBF). It is renowned for its exceptional strength, corrosion resistance, and high-temperature capabilities. Inconel 718 powder is widely employed in demanding industries like aerospace, energy, and medical. inconel 718 powder Composition and Characteristics Inconel 718 powder is an alloy primarily composed of nickel (Ni), chromium (Cr), iron (Fe), and niobium (Nb). Its specific composition varies slightly depending on the manufacturer and application requirements. The table below highlights the typical composition and characteristics of Inconel 718 powder:| Property | Value |
| Nickel (Ni) | 50-55% |
| Chromium (Cr) | 17-21% |
| Iron (Fe) | 17-21% |
| Niobium (Nb) | 4.75-5.5% |
| Molybdenum (Mo) | 2.8-3.3% |
| Titanium (Ti) | 0.65-1.15% |
| Aluminum (Al) | 0.2-0.8% |
| Carbon (C) | 0.08% max |
| Silicon (Si) | 0.35% max |
| Manganese (Mn) | 0.35% max |
| Sulfur (S) | 0.015% max |
| Phosphorus (P) | 0.015% max |
| Industry | Applications |
| Aerospace | Turbine blades, engine components, structural parts |
| Energy | Gas turbine components, heat exchangers, pressure vessels |
| Medical | Surgical instruments, implants, dental prosthetics |
| Automotive | High-performance engine components, exhaust systems |
| Defense | Armor, weapons, aerospace components |
| Parameter | Details |
| Specifications | ASTM B163, AMS 5848, ISO 2076 |
| Sizes | 15-150 microns (typical) |
| Grades | Inconel 718, Inconel 718Plus |
| Pros | Cons |
| High strength and hardness | Expensive compared to other alloys |
| Excellent corrosion resistance | Difficult to machine |
| High-temperature capabilities | Requires specialized welding techniques |
| Good weldability and formability | Can be susceptible to stress corrosion cracking |
Inconel 718 Powder
Inconel 718 Powder
| Product | Inconel 718 Powder |
| CAS No. | N/A |
| Appearance | Gray Metallic Powder |
| Purity | ≥99%,  ≥99.9%,  ≥95%(Other purities are also available) |
| APS | 1-5 µM, 10-53 µM  (Can be customized),  Ask for other available size range. |
| Ingredient | Ne-Fe-Cr |
| Density | 8.192g/cm3 |
| Molecular Weight | N/A |
| Product Codes | NCZ-DCY-281/25 |
Inconel 718 Description:
Inconel 718 Powder is one of the numerous advanced ceramic materials manufactured by Nanochemazone. Nanochemazone produces too many standard grades when applicable, including Mil Spec (military grade); ACS, Reagent and Technical Grade; Food, Agricultural and Pharmaceutical Grade; Optical Grade, USP and EP/BP (European Pharmacopoeia/British Pharmacopoeia) and follows applicable ASTM testing standards. Typical and custom packaging is available. Additional technical, research and safety (MSDS) information are available. Please request a quote above for more information on lead time and pricingInconel 718 Powder Related Information :
Storage Conditions:. Airtight sealed, avoid light and keep dry at room temperature. Please contact us for customization and price inquiry Email: contact@nanochemazone.com Note: We supply different size ranges of Nano and micron as per the client’s requirements and also accept customization in various parameters. Best inconel 718 powder for 3D printing Inconel 718 powder (IN718) is a well-known nickel-based superalloy powder that is extensively used in high-value-added engineering applications such as jet engines in aerospace and steam generators in nuclear power plants, as well as in the defense and marine sectors.| Metal Powder | Size | Quantity | Price/kg | Size | Quantity | Price/kg |
| Inconel 718 | 0-20μm | 1KG | 60.9 | 53-105μm | 1KG | 59 |
| 10KG | 39.8 | 10KG | 38 | |||
| 100KG | 34.5 | 100KG | 33 |
| Element | Weight % | Purpose |
| Nickel | 50 – 55 | Principal matrix element |
| Chromium | 17 – 21 | Oxidation resistance |
| Iron | Balance | Solid solution strengthener |
| Niobium | 4.75 – 5.5 | Precipitation hardening |
| Molybdenum | 2.8 – 3.3 | Solid solution strengthening |
| Titanium | 0.65 – 1.15 | Carbide former |
| Aluminum | 0.2 – 0.8 | Precipitation hardening |
| Carbon | 0.08 max | Carbide former |
| Property | Description |
| High strength | Tensile strength 1050 – 1350 MPa |
| Phase stability | Retains strength after prolonged use up to 700°C |
| Corrosion resistance | Resistant to aqueous corrosion and oxidation |
| Weldability | Readily weldable with matching filler |
| Fabricability | Easy to form and machine |
| Creep resistance | High stress rupture strength at high temperatures |
| Parameter | Typical value | Purpose |
| Layer height | 20 – 50 μm | Balance speed and resolution |
| Laser power | 195 – 350 W | Sufficient melting without evaporation |
| Scan speed | 700 – 1300 mm/s | Density versus build rate |
| Hatch spacing | 80 – 160 μm | Mechanical properties |
| Support structure | Minimal | Easy removal |
| Hot isostatic pressing | 1120°C, 100 MPa, 3h | Eliminate internal voids |
| Industry | Components |
| Aerospace | Turbine blades, disks, hot section parts |
| Oil & gas | Downhole tools, valves, pumps |
| Power generation | Combustion cans, transition ducts |
| Automotive | Turbocharger wheels, exhaust valves |
| Medical | Orthopedic implants, surgical tools |
| Parameter | Specification |
| Particle size range | 10 – 45 μm |
| Particle shape | Spherical morphology |
| Apparent density | > 4 g/cc |
| Tap density | > 6 g/cc |
| Hall flow rate | > 23 sec for 50 g |
| Purity | >99.9% |
| Oxygen content | <100 ppm |
| Method | Parameters Tested |
| Sieve analysis | Particle size distribution |
| SEM imaging | Particle morphology |
| EDX | Chemistry and composition |
| XRD | Phases present |
| Pycnometry | Density |
| Hall flow rate | Powder flowability |
| Alloy | Cost | Printability | Weldability | Strength |
| Inconel 718 | Low | Good | Excellent | Medium |
| Inconel 625 | Medium | Excellent | Excellent | Low |
| Inconel 939 | Very High | Fair | Limited | Excellent |
| Haynes 282 | High | Good | Limited | Excellent |
| Pros | Cons |
| Proven material credentials in AM | Lower high temperature strength than some alloys |
| Excellent weldability and machinability | Susceptible to solidification cracking during printing |
| Readily printed into complex shapes | Requires controlled atmosphere handling |
| Cost advantage over exotic superalloys | Significant post-processing often required |
| Available from range of suppliers | Relatively low hardness after printing |
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