K465 Alloy Powder
$0.00
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 pricing
K465 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.
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 |
Nickel forms the base of the alloy and provides a face-centered cubic matrix for high temperature strength. Elements like chromium, cobalt, and molybdenum contribute to solid solution strengthening and enable precipitation hardening.
Aluminum and titanium are added to form gamma prime precipitates Ni3(Al,Ti) to provide hardness and creep resistance up to 700°C. Tantalum provides solid solution strengthening and forms carbides for grain structure control. Boron facilitates precipitation of complex carbides.
The balanced composition of K465 nickel superalloy powder results in a combination of strength, ductility, corrosion resistance, and weldability required for high performance additive manufactured components. The optimized levels of alloying elements can be tailored based on final part requirements.
K465 Alloy Powder Properties
K465 superalloy powder processed via laser powder bed fusion or electron beam melting exhibits the following properties in as-built and heat treated states:
Mechanical Properties
| 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 |
High strength levels comparable to cast and wrought Ni-based superalloys
Ductility retained after heat treatment allows some forming/forging
Precipitation hardening by gamma prime phase after solution treatment
Physical Properties
| 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 |
Retains over half its strength at maximum service temperature
Resists oxidation and hot corrosion in gas turbine environments
Excellent creep rupture strength under load at high temperature
Other Notable Properties
Weldable using conventional fusion welding methods
Good surface finish and dimensional accuracy in AM builds
Customizable with different heat treatments
High thermal fatigue and crack growth resistance
The balanced set of mechanical, physical, and thermal properties make K465 suitable for extreme environments faced in aerospace engines, power generation systems, and chemical processing equipment. The properties can be fine-tuned based on application requirements.
K465 Alloy Powder Applications
The major applications of additive manufactured K465 superalloy parts include:
Aerospace:
Combustor liners, augmentors, flame holders in jet engines
Structural brackets, frames, housings, fittings
Hot section components like turbine blades and vanes
Rocket propulsion systems and spacecraft engines
Power Generation:
Heat exchangers, piping, valves, manifolds in boilers and heat recovery systems
Gas turbine hot gas path components like nozzles, shrouds
Solar power receivers and collectors
Automotive:
Turbocharger wheels and housings
Exhaust system manifolds and components
Chemical Processing:
Reformer tubes, reaction vessels, heat exchanger components
Piping, valves, pumps for corrosive chemicals
Tooling like mandrels, fixtures for composite parts
Benefits:
Withstands sustained use at over 700°C lower density than competing alloys
Oxidation and corrosion resistance in hot gas environments
Reduces component weight compared to cast nickel alloys
Enables complex optimized geometries not possible with casting
Consolidates multiple parts into one printed component
Saves material waste relative to subtractive methods
Shorter lead times compared to traditional processing
K465 is frequently used as substitute for heavier, costlier superalloys in aerospace engines and land-based power systems. The alloy powder can be tailored to meet requirements in extreme temperature, pressure, and corrosive service conditions.
K465 Alloy Powder Specifications
K465 alloy powder for AM processes is supplied by various manufacturers to the following nominal specifications:
| 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 |
Powder particle size distribution optimized for AM processes
High powder flowability ensures uniform layer spreading
Low oxygen content minimizes risk of defects in builds
Spherical morphology provides good packing and powder bed density
Additional Requirements:
Powder should be handled in an inert atmosphere to prevent contamination
Moisture content must be kept below 0.1 wt% for good powder flow
Temporary storage life up to 1 year in sealed containers with argon
Open containers to be used within 1 week to avoid degradation
Meeting powder specifications in terms of size, shape, chemistry, and handling is critical to achieving high density AM parts with expected mechanical properties.
K465 Alloy Powder Availability
K465 superalloy powder can be sourced from major suppliers like:
| Manufacturer | Product Name |
| Praxair | TA1 |
| Carpenter Additive | Car Tech K465 |
| Sandvik Osprey | K465-TCP |
| Erasteel | Satellite AM K465 |
The alloy powder is sold in various sizes ranging from 1 kg containers for R&D purposes up to 1000 kg containers for production volumes. Prices range from $90-150 per kg based on quantity and manufacturer.
Lead times for procurement typically range from 2-8 weeks after order confirmation. Customized particle size distributions and special handling may require a longer lead time.
K465 powder inventory should be monitored closely and reordered well in advance of running out. Shortages can cause costly AM machine downtime. Consider spacing out orders over time to maintain stock.
K465 Alloy Powder Processing
Parameter Ranges for AM Processes:
| 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 |
DMLS = Direct metal laser sintering
EBM = Electron beam melting
A wider range of parameters allows flexibility to optimize for surface finish, build time, or mechanical properties
Preheating reduces residual stresses; higher for EBM due to higher temperatures
Slower scan speeds improve density but prolong build time
Fine hatch spacing reduces porosity but requires more scan passes
Post-Processing:
Removal of parts from build plate using EDM wire cutting
Removal of residual powder via glass bead blasting
Stress relief heat treatment at 870°C for 1 hour
HIP treatment at 1160°C under 100 MPa pressure for 4 hours
Age hardening heat treatment at 760°C for 10 hours
Benefits of Post-Processing:
HIP closes internal voids and minimizes porosity
Heat treatments relieve residual stress and achieve optimal hardness
Yields close to 100% dense parts with mechanical properties equivalent to cast and wrought
Additional hot isostatic pressing (HIP) and heat treatments can further enhance properties
Parameter selection, support structures, build orientation, post-processing steps are all optimizable based on AM technology used and properties required.
How K465 Compares with Other Superalloy Powders
K465 vs Inconel 718
| 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 |
K465 chosen for higher temperature capability where cost increase is justified
Inconel 718 more economical for lower temperature applications
K465 vs Haynes 282
| Alloy | K465 | Haynes 282 |
| Processability | Better | More difficult |
| Thermal conductivity | Higher | Lower |
| Service temperature | Similar | Similar |
| Cost | Similar | Similar |
K465 easier to laser print and post-process without cracking
Haynes 282 more prone to solidification cracks during builds
K465 vs CM 247 LC
| Alloy | K465 | CM 247 LC |
| Density | Lower | Higher |
| Strength | Similar | Similar |
| Ductility | Higher | Lower |
| Cost | Lower | Higher |
K465 has better combinaton of strength and ductility
Lower cost alloy alternative to CM 247 LC
K465 vs Inconel 625
| Alloy | K465 | Inconel 625 |
| Service Temperature | Higher | Up to 700°C |
| Corrosion Resistance | Moderate | Excellent |
| Cost | Higher | Lower |
| Availability | More limited | Readily available |
Inconel 625 chosen where corrosion resistance trumps high temperature capability
K465 preferred for jet engine parts seeing extreme temperatures
Understanding where K465 excels or falls short compared to alternatives aids material selection for AM components. The alloy can be tailored to shift the balance between cost, availability, processability, and properties.
K465 Alloy Powder – Frequently Asked Questions
Q: What pre-processing steps are required for K465 powder?
A: K465 powder needs to be dried for 1-4 hours at 100-150°C to remove moisture absorbed during shipping and storage. Sieving between 20-63 microns will eliminate large particles that can cause recoater issues.
Q: Does K465 require hot isostatic pressing (HIP) post-processing?
A: HIP is recommended but not mandatory for K465. It helps close internal voids and achieve maximum density and mechanical properties. HIP at 1160°C under 100 MPa for 4 hours is typical.
Q: What heat treatments can be used to tailor K465 properties?
A: Solution treatment at 1150°C plus single or double aging between 700-850°C is used to optimize strength and ductility. Rapid cooling after solution treatment enhances properties.
Q: Is K465 superalloy weldable for repair purposes?
A: Yes, K465 can be welded using ER NiCrMo-10 filler metal. Solution treatment at 1175°C and aging at 845°C is required after welding to restore properties.
Q: What manufacturing defects can occur with K465 builds?
A: Lack of fusion porosity, cracking between layers, delamination, and distortion are potential defects requiring parameter optimization. Lower preheat and faster scan speeds increase risk.
Q: What finishing methods can be used on additively manufactured K465 parts?
A: Machining, shot peening, chemical etching, and electropolishing allow surface roughness improvement. This facilitates NDE inspection and improves fatigue life.
Q: Does K465 alloy powder require special storage precautions?
A: K465 powder rapidly absorbs moisture, so storage in sealed argon purged containers is required. Use within 1 week of opening container to prevent degradation.
Q: What safety precautions are needed when handling K465 powder?
A: K465 powder is not flammable but may cause skin/eye irritation. Use protective gloves, clothing, face shields. Avoid inhalation and install proper ventilation.
Category: High Temperature Alloy Powder
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.
Reviews (0)
Only logged in customers who have purchased this product may leave a review.
Shipping & Delivery
Related products
Alloy Series Powder
$0.00
Alloy Series Powder
| Product | Alloy Series Powder |
| CAS No. | 12069-94-2 |
| Appearance | Silver-White 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 | NiCrCoMoFeAl |
| Density | 2.6-2.8g/cm3 |
| Molecular Weight | N/A |
| Product Codes | NCZ-DCY-290/25 |
Alloy Series Description:
Alloy Series 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 pricingAlloy Series 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. High temperature alloy series High-temperature alloy series powders are designed to handle extreme high-temperature environments, providing excellent performance and heat-resistant properties. Let’s explore this range of products and understand their potential for high temperature applications.| Product | Specification | Apparent Density | Flow Ability | Oxygen Content | Tensile Strength | Yield Strength | Elongation |
| GH3625 | 15-53µm 45-105µm 75-150µm | ≥4.40g/cm³ | ≤20s/50g | ≤300ppm | 1000±50Mpa | 600±50Mpa | 35±5% |
| GH4169 | ≥4.20g/cm³ | ≤20s/50g | ≤300ppm | 1250±30Mpa | 1000±30Mpa | 18±3% | |
| GH3230 | ≥4.40g/cm³ | ≤20s/50g | ≤300ppm | 930±30Mpa | 930±30Mpa | 25±5% | |
| GH3536 | ≥4.40g/cm³ | ≤20s/50g | ≤300ppm | 850±30Mpa | 550±20Mpa | 42±5% |
GH 3625 Powder
$0.00
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-283/25 |
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 pricingGH 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. GH 3625 Powder GH3625 powder is an age-hardenable nickel-iron base alloy containing 25% chromium along with additions of molybdenum and aluminum. It provides an exceptional combination of high strength, hardness, corrosion resistance, and oxidation resistance at elevated temperatures. Overview of GH3625 Powder GH 3625 powder is an age-hardenable nickel-iron base alloy containing 25% chromium along with additions of molybdenum and aluminum. It provides an exceptional combination of high strength, hardness, corrosion resistance, and oxidation resistance at elevated temperatures. Key properties and advantages of GH3625 powder include: GH3625 Powder Properties and Characteristics| Properties | Details |
| Composition | Ni-25Cr-4.5Mo-3.5Al alloy |
| Density | 8.2 g/cc |
| Particle shape | Predominantly spherical |
| Size range | 15-45 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 % |
| Nickel | Balance |
| Chromium | 24-27% |
| Molybdenum | 4-5% |
| Aluminum | 3-4% |
| Carbon | 0.1% max |
| Manganese | 1% max |
| Silicon | 0.5% max |
| Sulfur | 0.015% max |
| Property | Values |
| Density | 8.2 g/cc |
| Melting point | 1390-1440°C |
| Thermal conductivity | 11 W/mK |
| Electrical resistivity | 52 μΩ-cm |
| Coefficient of thermal expansion | 13.0 x 10^-6 /K |
| Property | Condition | Values |
| Hardness | Solution annealed | 35 HRC |
| Hardness | Peak aged | 50-56 HRC |
| Tensile strength | Annealed | 1000 MPa |
| Tensile strength | Aged | 1500-1800 MPa |
| Yield strength | Aged | 1200-1600 MPa |
| Elongation | Aged | 10-15% |
| 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 |
| AMS 5815 | Nickel alloy powder compositions |
| AMS 5408 | Wire, rods, and 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 |
| Particle Size | Characteristics |
| 15-25 microns | Ultrafine powder used in laser AM processes |
| 25-45 microns | Size range for most powder bed AM systems |
| 45-75 microns | Larger sizes used in laser cladding |
| Apparent Density | Details |
| Up to 60% of true density | For spherical powder morphology |
| 4.5 – 5.2 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 |
| Ensure proper ventilation | Avoid exposure to fine metallic particles |
| 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 |
| Parameter | GH3625 | Inconel 718 |
| Density | 8.2 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 |
GH3230 Powder
$0.00
GH3230 Powder
| Product | GH3230 Powder |
| CAS No. | 3230-94-2 |
| Appearance | Metallic 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-Mo-W-Fe |
| Density | 7.8g/cm3 |
| Molecular Weight | N/A |
| Product Codes | NCZ-DCY-285/25 |
GH3230 Description:
GH3230 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 pricingGH3230 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. GH3230 is a W-Mo reinforced nickel-based high-temperature alloy, which is usually used in an environment of 700-1000°C. GH3230 alloy has high high-temperature strength and good fatigue properties. And due to its excellent organizational stability, it has good anti-oxidation and anti-hot corrosion properties. GH3230 Powder is a W-Mo reinforced nickel-based high-temperature alloy, which is usually used in an environment of 700-1000°C. GH3230 alloy has high high-temperature strength and good fatigue properties. And due to its excellent organizational stability, it has good anti-oxidation and anti-hot corrosion properties, and is widely used in aerospace engine combustion chambers, ground gas turbine combustion chambers, and some high-temperature and corrosion-resistant components in the chemical industry. 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 | ≥4.60g/cm³ | ≥5.20g/cm³ |
| Test temperature | Tensile strength (σb/Mpa) | Yield strength (σp0.2/Mpa) | Elongation (δ5/%) |
| 25℃ | 840 | 450 | 35 |
| 815℃ | 250 | 200 | 35 |
| 1000℃ | 160 | 130 | 30 |
| Element | C | Cr | Ni | Co | W | Mo |
| wt% | 0.05-0.15 | 20.00-24.00 | Bal | ≤5.00 | 13.00-15.00 | 3.15-4.15 |
| Element | Al | Ti | Fe | La | B | Mn |
| wt% | 2.20-0.50 | ≤0.10 | ≤3.00 | 0.005-0.05 | ≤0.015 | 0.30-1.00 |
| Element | Si | P | S | Cu | O | N |
| wt% | 0.25-0.75 | ≤0.01 | ≤0.010 | ≤0.50 | ≤0.025 | ≤0.015 |
GH5188 Powder
$0.00
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
$0.00
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 |
Inconel 625 Powder
$0.00
Inconel 625 Powder
| Product | Inconel 625 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 | NiCr22Mo9Nb |
| Density | 8.4g/cm3 |
| Molecular Weight | N/A |
| Product Codes | NCZ-DCY-292/25 |
Inconel 625 Description:
Inconel 625 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 625 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 |
| 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% |
| 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 |
| 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 |
| 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 |
| 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 |
| 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 |
Inconel 718 Powder
$0.00
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 |
Nickel-based K403 Powder
$0.00
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 |

Reviews
There are no reviews yet.