Inconel 718 Powder
$0.00
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 pricing
Inconel 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 |
Overview of Inconel 718 Powder
Inconel 718 is a precipitation hard enable nickel-based superalloy powder widely used for additive manufacturing across aerospace, oil & gas, power generation and automotive industries. This article provides a detailed guide to Inconel 718 powder.
Key aspects covered include composition, properties, AM print parameters, applications, specifications, suppliers, handling, inspection methods, comparisons to alternatives, pros and cons, and FAQs. Tables are used to present information in an easy-to-reference format.
Composition of Inconel 718 Powder
The composition of Inconel 718 is:
| 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 |
Trace amounts of cobalt, boron, copper and magnesium are also added to enhance properties.
Key properties of Inconel 718 include:
| 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 |
Typical parameters for printing Inconel 718 powder include:
| 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 |
The parameters depend on factors like build geometry, temperature management and post-processing needs.
Applications of 3D Printed Inconel 718 Parts
Inconel 718 parts made by AM are used in:
| 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 |
Benefits over wrought parts include complex geometries and reduced buy-to-fly ratios.
Specifications of Inconel 718 Powder for AM
Inconel 718 powder must meet the following specifications for 3D printing:
| 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 |
Handling and Storage of Inconel 718 Powder
As a reactive material, Inconel 718 powder requires controlled handling:
Store sealed containers in a cool, dry inert atmosphere
Prevent exposure to moisture, air, temperature extremes
Use properly grounded equipment during transfer
Avoid dust accumulation and ignition sources
Local exhaust ventilation recommended
Follow applicable safety guidelines
Correct storage/handling prevents composition changes or hazards.
Inspection and Testing of Inconel 718 Powder
Inconel 718 powder batches are validated using:
| 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 |
Testing per ASTM standards ensures batch-to-batch quality consistency.
Comparing Inconel 718 to Alternative Superalloy Powders
Inconel 718 compares with other alloys as:
| 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 |
For balanced properties at lower cost, Inconel 718 supersedes other Ni superalloys for many applications.
Pros and Cons of Inconel 718 Powder for AM
| 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 |
Inconel 718 enables high performance AM at a reasonable cost.
Frequently Asked Questions about Inconel 718 Powder
Q: What particle size range works best for printing Inconel 718 alloy?
A: A range of 15-45 microns provides the optimum combination of flowability, high resolution, and high density parts.
Q: What post processing is typically required for Inconel 718 AM parts?
A: Hot isostatic pressing, heat treatment, and machining are commonly needed to eliminate voids, optimize properties, and achieve tolerances.
Q: Is Inconel 718 easier to 3D print than other Ni superalloys?
A: Yes, its excellent weldability and lower cracking susceptibility make Inconel 718 one of the easier Ni-based superalloys to process by AM.
Q: What industries use Inconel 718 alloy for metal 3D printing?
A: Aerospace, oil & gas, power generation, automotive, and medical sectors are major applications benefiting from additively manufactured Inconel 718.
Q: Does Inconel 718 require supports when 3D printing?
A: Minimal supports are recommended on overhangs and bridged sections to prevent deformation and allow easy removal after printing.
Q: What defects can occur when printing Inconel 718 powder?
A: Potential defects are cracking, porosity, distortion, incomplete fusion, and surface roughness. Most can be prevented with optimized parameters.
Q: What hardness can be expected with Inconel 718 AM components?
A: Hardness after printing is typically 30-35 HRC. Post-processes like aging can increase it to 40-50 HRC for higher wear resistance.
Q: What accuracy can be obtained with Inconel 718 printed parts?
A: Comparable dimensional tolerances and surface finishes to CNC machined components can be achieved after post-processing.
Q: Is hot isostatic pressing mandatory for Inconel 718 3D printed parts?
A: HIP eliminates internal voids and improves fatigue life. It may not be required for non-critical applications.
Q: What alloy powder has properties closest to Inconel 718 for AM?
A: Inconel 625 has comparable corrosion resistance and weldability to 718 but lower strength. Inconel 939 trades weldability for higher strength.
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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| Purity | ≥99%,  ≥99.9%,  ≥95%(Other purities are also available) |
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| Density | 8.3 g/cc |
| Particle shape | Predominantly spherical |
| Size range | 10-45 microns |
| Apparent density | Up to 60% of true density |
| Flowability | Good |
| Strength | Very high after aging treatment |
| Corrosion resistance | Excellent including pitting and crevice corrosion |
| Element | Weight % |
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| Chromium | 28-32% |
| Molybdenum | 3-5% |
| Aluminum | 1-3% |
| Carbon | 0.1% max |
| Manganese | 1% max |
| Silicon | 0.5% max |
| Sulfur | 0.015% max |
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| Density | 8.3 g/cc |
| Melting point | 1370-1420°C |
| Thermal conductivity | 12 W/mK |
| Electrical resistivity | 70 μΩ-cm |
| Coefficient of thermal expansion | 12.5 x 10^-6 /K |
| Property | Condition | Values |
| Hardness | Solution annealed | 37 HRC |
| Hardness | Peak aged | 52-58 HRC |
| Tensile strength | Annealed | 1100 MPa |
| Tensile strength | Aged | 1600-2000 MPa |
| Yield strength | Aged | 1400-1800 MPa |
| Elongation | Aged | 8-12% |
| Industry | Uses |
| Aerospace | Turbine blades, bolts, fasteners |
| Oil and gas | Wellhead valves, downhole tools |
| Chemical processing | Extruder screws, valve parts |
| Power generation | Boiler components, steam and gas turbines |
| Standard | Description |
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| AMS 5408 | Wire, rods, bars of precipitation hardening nickel alloys |
| AMS 5698 | Investment castings of PH nickel alloys |
| AMS 5772 | Nickel alloy forgings |
| AMS 5634 | Nickel alloy extruded shapes |
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| 22-45 microns | Size range for most powder bed AM systems |
| 45-75 microns | Larger sizes used in laser cladding or thermal spraying |
| Apparent Density | Details |
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| 4.8 – 5.5 g/cc | Improves with greater packing density |
| Method | Details |
| Gas atomization | High pressure inert gas breaks up molten metal stream into fine droplets |
| Vacuum induction melting | High purity input materials melted under vacuum |
| Multiple remelting | Improves chemical homogeneity |
| Sieving | Classifies powder into different particle size fractions |
| Recommendation | Reason |
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| Use appropriate PPE | Prevent accidental inhalation or ingestion |
| Follow safe protocols | Reduce health and fire hazards |
| Store sealed containers | Prevent contamination or oxidation |
| Test | Details |
| Chemical analysis | OES or XRF spectroscopy used to verify composition |
| Particle size distribution | Laser diffraction analysis |
| Apparent density | Measured as per ASTM B212 standard |
| Powder morphology | SEM imaging of particle shape |
| Flow rate analysis | Gravity flow rate through specified nozzle |
| Moisture measurement | Loss on drying analysis |
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| Density | 8.3 g/cc | 8.2 g/cc |
| Strength | Higher | Lower |
| Corrosion resistance | Excellent | Outstanding |
| Cost | Moderate | Very high |
| Uses | Oil and gas, chemical processing | Aerospace, nuclear |
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| 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. |
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| Molecular Weight | N/A |
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| 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 |
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 |
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| 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 | – | – | – |
IN738LC Powder
IN738LC Powder
| Product | INC738LC Powder |
| CAS No. | N/A |
| Appearance | Gray or 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-16Cr-8.5Co-2.4Al-3.4Ti-1.75Mo-1.75w-0.9Nb-0.6Zr-0.1C |
| Density | 8.19g/cm3 |
| Molecular Weight | N/A |
| Product Codes | NCZ-DCY-278/25 |
IN738LC Description:
INC738LC 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 pricingIN738LC 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 IN738LC powder for 3D printing in 2024| Alloy | Nominal Composition (wt%) |
| IN738LC | Ni – 16Cr – 8.5Co – 3.4Al – 3.4Ti – 1.7Mo – 2.6W – 1.7Ta – 0.9Nb – 0.05C – 0.03Zr – 0.001B |
| Property | Value |
| Density | 8.19 g/cm³ |
| Melting Range | 1260-1335°C |
| Yield Strength (at 650°C) | >758 MPa |
| Tensile Strength (at 650°C) | >1035 MPa |
| Elongation (at 650°C) | >12% |
| Grain Size | Fine-grained |
| Gamma Prime Phase | High volume fraction |
| Application | Industry | Examples |
| Turbine Components | Aerospace, Energy | Blades, Vanes, Nozzles |
| Automotive Components | Automotive | Turbochargers, Exhaust Manifolds |
| Tooling and Molds | Manufacturing | Injection Molds, Die Casting Molds |
| Heat Exchangers | Energy, Chemical | High-Temperature Recuperators |
| Medical Implants | Healthcare | Orthopedic Implants, Dental Restorations |
| Powder Specifications |
| Particle Size Distribution: 15-53 μm |
| Flowability: Excellent |
| Sphericity: High |
| Apparent Density: 4.2-4.6 g/cm³ |
| Standards: AMS 5832, AMS 5385 |
| Typical Grades |
| IN738LC – Standard Grade |
| IN738LC-LG – Low Gauge Grade |
| IN738LC-HG – High Gauge Grade |
| Pros | Cons |
| Excellent high-temperature strength and creep resistance | Higher material cost compared to some other alloys |
| Superior oxidation and corrosion resistance | Potential for cracking and distortion during printing |
| Ability to produce complex geometries | Strict process control required for optimal properties |
| Lightweight and high strength-to-weight ratio | Limited availability of qualified suppliers |
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 |
K465 Alloy Powder
K465 Alloy Powder
| Product | K465 Alloy Powder |
| CAS No. | 7440-02-0 |
| 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 | NiCrMoCo |
| Density | 8.1-8.3g/cm3 |
| Molecular Weight | N/A |
| Product Codes | NCZ-DCY-293/25 |
K465 Alloy Description:
K465 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 pricingK465 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. K465 Alloy Powder K465 alloy powder is a nickel-based superalloy that offers high strength and corrosion resistance at elevated temperatures. It is widely used in aerospace, power generation, and chemical processing industries. K465 Alloy Powder: Composition, Properties, Applications, and Specifications K465 has become a popular choice for aerospace, power generation, and chemical processing industries where components are subjected to high temperatures or aggressive environments. It allows complex geometries to be 3D printed for optimal performance. This article provides detailed information on the composition, properties, applications, specifications, availability, processing, and comparisons of K465 superalloy powder for additive manufacturing. K465 Alloy Powder Composition The nominal composition of K465 nickel-based superalloy powder is given below:| Element | Weight % |
| Nickel (Ni) | Balance |
| Chromium (Cr) | 15 – 17% |
| Cobalt (Co) | 9 – 10% |
| Molybdenum (Mo) | 3% |
| Tantalum (Ta) | 4.5 – 5.5% |
| Aluminum (Al) | 5 – 6% |
| Titanium (Ti) | 0.5 – 1% |
| Boron (B) | 0.01% max |
| Carbon (C) | 0.03% max |
| Zirconium (Zr) | 0.01% max |
| Niobium (Nb) | 1% max |
| Property | As-Built Condition | After Heat Treatment |
| Tensile Strength | 1050 – 1250 MPa | 1150 – 1350 MPa |
| Yield Strength | 750 – 950 MPa | 1000 – 1200 MPa |
| Elongation | 10 – 25% | 8 – 15% |
| Hardness | 35 – 45 HRC | 42 – 48 HRC |
| Property | Value |
| Density | 8.1 – 8.3 g/cc |
| Melting Point | 1260 – 1350°C |
| Thermal Conductivity | 11 – 16 W/m-K |
| Thermal Expansion Coefficient | 12 – 16 x 10<sup>-6</sup> /K |
| Property | Value |
| Service Temperature | Up to 700°C |
| Oxidation Resistance | Good up to 850°C |
| Phase Stability | Retains strength up to 70% of melting point |
| Creep Rupture Strength | 140 MPa at 700°C for 1000 hours |
| Parameter | Specification |
| Particle size distribution | 15 – 53 microns |
| Oxygen content | 0.05% max |
| Nitrogen content | 0.05% max |
| Morphology | Spheroidal |
| Apparent density | 4.0 – 4.5 g/cc |
| Tap density | 4.5 – 5.0 g/cc |
| Flow rate | 15 – 25 s/50g |
| Manufacturer | Product Name |
| Praxair | TA1 |
| Carpenter Additive | Car Tech K465 |
| Sandvik Osprey | K465-TCP |
| Erasteel | Satellite AM K465 |
| Process | Preheating Temp | Layer Thickness | Laser Power | Scan Speed | Hatch Spacing |
| DMLS | 150 – 180°C | 20 – 60 μm | 195 – 250 W | 600 – 1200 mm/s | 0.08 – 0.12 mm |
| EBM | 1000 – 1100°C | 50 – 200 μm | 5 – 25 mA | 50 – 200 mm/s | 0.1 – 0.2 mm |
| Alloy | K465 | Inconel 718 |
| Density | Higher | Lower |
| Tensile Strength | Similar | Similar |
| Service Temperature | 100°C higher | Up to 650°C |
| Cost | 2X more expensive | More economical |
| Alloy | K465 | Haynes 282 |
| Processability | Better | More difficult |
| Thermal conductivity | Higher | Lower |
| Service temperature | Similar | Similar |
| Cost | Similar | Similar |
| Alloy | K465 | CM 247 LC |
| Density | Lower | Higher |
| Strength | Similar | Similar |
| Ductility | Higher | Lower |
| Cost | Lower | Higher |
| Alloy | K465 | Inconel 625 |
| Service Temperature | Higher | Up to 700°C |
| Corrosion Resistance | Moderate | Excellent |
| Cost | Higher | Lower |
| Availability | More limited | Readily available |
Nickel-based K403 Powder
Nickel-based K403 Powder
| Product | Nickel-based K403 Powder |
| CAS No. | 7440-02-0 |
| 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-Cr-Co-Al-Mo-W-Ti-C-B |
| Density | 8.2g/cm3 |
| Molecular Weight | N/A |
| Product Codes | NCZ-DCY-294/25 |
Nickel-based K403 Description:
Nickel-based K403 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 pricingNickel-based K403 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. Nickel-based K403 Powder K403 powder is a nickel-chromium-iron-molybdenum alloy powder. It offers excellent resistance to oxidation, corrosion and thermal fatigue cracking. K403 has good phase stability at high temperatures. K403 powder is designed for protective coatings, thermal spray, welding, brazing, and other high temperature applications. Overview of Nickel-based K403 Powder K403 powder is a nickel-chromium-iron-molybdenum alloy powder. It offers excellent resistance to oxidation, corrosion and thermal fatigue cracking. K403 has good phase stability at high temperatures. Key features of K403 powder include: Outstanding high temperature strength and creep resistance Resists oxidation and hot corrosion up to 1150°C Retains properties under cyclic heating conditions Compatible coefficient of expansion with common alloys Available in various size ranges and morphologies K403 powder is designed for protective coatings, thermal spray, welding, brazing, and other high temperature applications. This article provides a detailed look at the composition, properties, applications, specifications, pricing, safety, and other essential information about nickel-based K403 powder. Composition of Nickel-based K403 Powder The typical composition of nickel-based K403 powder is:| Element | Composition |
| Nickel (Ni) | Balance |
| Chromium (Cr) | 21-23% |
| Iron (Fe) | 17-20% |
| Molybdenum (Mo) | 8-10% |
| Tungsten (W) | 1-2% |
| Manganese (Mn) | ≤0.5% |
| Silicon (Si) | ≤0.5% |
| Carbon (C) | ≤0.1% |
| Property | Details |
| Density | 8.2 g/cm3 |
| Melting Point | 1350-1400°C |
| Thermal Conductivity | 11 W/m.K |
| Electrical Resistivity | 94 microhm-cm |
| Young’s Modulus | 207 GPa |
| Poisson’s Ratio | 0.29-0.30 |
| Tensile Strength | ≥ 550 MPa up to 1050°C |
| Elongation | 15-25% |
| Hardness | 30-35 HRC |
| Oxidation Resistance | Excellent isothermal up to 1150°C |
| Parameter | K403 Powder | IN738 Powder |
| Composition | Ni-Cr-Fe-Mo | Ni-Cr-Co-Al-Ti |
| Oxidation Resistance | Excellent up to 1150°C | Very Good up to 1100°C |
| Cost | Higher | Lower |
| Phase Stability | Very Good | Poor |
| Mechanical Strength | High up to 1050°C | Good up to 750°C |
| Fabrication | Medium | Easy |
| Applications | Thermal spray, welding | Turbine components, AM parts |
| Availability | Moderate | Readily available |

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