1. Introduction
Inconel® 625 is a nickel-chromium-molybdenum-niobium superalloy engineered for resilience in some of the most aggressive environments known to modern industry.
First introduced by Huntington Alloys (now Special Metals Corporation) in the 1960s, it was designed for high-strength marine and aerospace applications where corrosion and temperature extremes demanded more than stainless steel could offer.
Today, Inconel 625 is synonymous with superior corrosion resistance, structural stability, and weldability, making it an essential material in sectors like oil & gas, power generation, and chemical processing.
2. What Is Inconel 625?
Inconel 625 (UNS N06625; W.Nr. 2.4856) is a corrosion-resistant, high-performance nickel-based superalloy known for its excellent strength, fatigue resistance, and structural stability over a broad temperature range.
Chemically composed primarily of nickel, chromium, molybdenum, and niobium, it belongs to the class of solid-solution-strengthened alloys, meaning its mechanical strength is derived not from heat treatment (like precipitation-hardened alloys such as Inconel 718) but from the uniform dispersion of alloying elements within the crystal lattice.

This metallurgy provides consistent mechanical and corrosion-resistant properties from cryogenic temperatures (-270°C) to elevated service temperatures (up to 1,093°C or 2,000°F), making it uniquely valuable for applications in extreme environments.
Its metallurgical simplicity also contributes to exceptional weldability, thermal fatigue resistance, and stress-corrosion resistance—key factors in industries such as aerospace, marine, chemical processing, and nuclear power.
Inconel 625 is commonly used in both annealed and solution-treated conditions and meets various international standards, including ASTM B443 (plate/sheet) and ASTM B446 (bar/rod).
3. Inconel 625 Chemical Composition
Inconel 625’s performance stems from a precisely balanced blend of elements, each contributing to its corrosion resistance and mechanical strength.
Here is the chemical composition of Inconel 625 (UNS N06625 / W.Nr. 2.4856) as per common standards such as ASTM B446 and B443:
| Element | Weight % (Typical Range) | Function |
| Nickel (Ni) | 61.0 min (Balance) | Corrosion resistance, base matrix |
| Chromium (Cr) | 20.0 – 23.0 | Oxidation resistance, passivation |
| Molybdenum (Mo) | 8.0 – 10.0 | Strengthening, pitting resistance |
| Niobium (Nb) + Ta | 3.15 – 4.15 | Solid-solution strengthening |
| Iron (Fe) | ≤5.0 | Residual/strength contributor |
| Cobalt (Co) | ≤1.0 | Minor strengthening (optional) |
| Manganese (Mn) | ≤0.5 | Deoxidizer |
| Silicon (Si) | ≤0.5 | Improves fluidity in melting |
| Aluminum (Al) | ≤0.4 | Grain refinement, oxidation resistance |
| Titanium (Ti) | ≤0.4 | Grain strengthening (minor) |
| Carbon (C) | ≤0.10 | Increases hardness, limited for weldability |
| Phosphorus (P) | ≤0.015 | Impurity—should be minimized |
| Sulfur (S) | ≤0.015 | Impurity—causes hot cracking if excessive |
Note: Slight variations may occur depending on the specific form (bar, plate, wire) or product standard.
4. Inconel 625 Material Properties
Mechanical Properties (at Room Temperature unless otherwise noted)
| Property | Typical Value | Notes |
| Tensile Strength | ~827 MPa (120 ksi) | Solid solution strengthened |
| Yield Strength (0.2% offset) | ~414 MPa (60 ksi) | Can be increased via cold working |
| Elongation at Break | 30–35% | Excellent ductility |
| Hardness (Rockwell B) | ~92 HRB | Annealed condition |
| Fatigue Strength | ~276 MPa (40 ksi) | At 10⁷ cycles in air |
| Creep Resistance | Excellent | Up to ~980°C (1800°F) |
| Impact Toughness | High | Maintains toughness at cryogenic temperatures |
Physical Properties
| Property | Typical Value | Units / Notes |
| Density | 8.44 g/cm³ | (0.305 lb/in³) |
| Melting Range | 1290 – 1355 °C | (2354 – 2471 °F) |
| Thermal Conductivity | 9.8 W/m·K | At 21 °C (lower than stainless steel) |
| Specific Heat Capacity | 410 J/kg·K | At 20 °C |
| Electrical Resistivity | 1.31 μΩ·m | At 20 °C |
| Modulus of Elasticity | 207 GPa | (30 x 10⁶ psi) |
| Coefficient of Thermal Expansion | 13.0 ×10⁻⁶ /K | From 20°C to 100°C |
| Magnetic Permeability | ~1.0006 (Relative) | Essentially non-magnetic |
5. Corrosion Resistance of Inconel 625
Inconel 625’s corrosion resistance is unmatched in many aggressive environments, thanks to its alloying elements:

- High-Temperature Oxidation: Forms a dense Cr₂O₃ scale that resists oxidation up to 1,093°C. At 800°C, oxidation rate is <0.02 mm/year (vs. 316L: 0.15 mm/year).
- Chloride Resistance: Pitting Resistance Equivalent Number (PREN = Cr + 3.3Mo + 16N) of ~45—far exceeding 316L (PREN ~31) and even Inconel 718 (PREN ~30).
In seawater (35,000 ppm Cl⁻), corrosion rate is <0.01 mm/year with no pitting even after 10,000 hours. - Acid Resistance:
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- Sulfuric acid (5% at 60°C): Corrosion rate <0.05 mm/year (vs. 316L: 1.2 mm/year).
- Hydrochloric acid (10% at 25°C): <0.1 mm/year (Hastelloy C-276: <0.05 mm/year, a close rival).
- Nitric acid (20% at 50°C): <0.03 mm/year, suitable for chemical processing.
- Sulfide Resistance: Withstands sour gas (H₂S-rich) environments per NACE MR0175, with no sulfide stress cracking (SSC) at 60% of yield strength.
6. Manufacturing and Processing of Inconel 625
Inconel 625, a high-performance nickel-based superalloy, offers outstanding weldability and corrosion resistance, but its high alloy content—especially molybdenum and niobium—makes it challenging to machine and form.
However, with proper techniques and tooling, Inconel 625 can be efficiently processed into complex, high-integrity components for demanding industries such as aerospace, marine, and chemical processing.

Welding
- Preferred Process: Gas Tungsten Arc Welding (GTAW/TIG), using ERNiCrMo-3 filler metal for metallurgical compatibility.
- Heat Input Management: Welding is typically performed at 100–150 A to limit grain growth in the heat-affected zone (HAZ), which preserves mechanical properties and microstructural integrity.
- Post-Weld Treatment: Unlike precipitation-strengthened alloys (e.g., Inconel 718), Inconel 625 does not require post-weld heat treatment, thanks to its solid-solution strengthening mechanism.
- Weld Integrity: Welds retain up to 90% of the base metal’s strength and demonstrate excellent corrosion resistance without sensitization—an issue commonly seen in austenitic stainless steels.
Machining
- Challenge: Inconel 625 work-hardens rapidly—surface hardness can increase by up to 50% during cutting—leading to severe tool wear.
- Solutions:
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- Use carbide tools with TiAlN (Titanium Aluminum Nitride) coatings.
- Maintain low cutting speeds (5–10 m/min) and high feed rates to reduce heat concentration.
- Apply high-pressure coolant systems (≥70 bar) to assist in chip removal and thermal control.
- Economic Impact: Machining costs are 4–5 times higher than for 316L stainless steel due to slower speeds, increased tool wear, and the need for specialized cutting equipment.
Forming and Forging
- Cold Forming:
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- Inconel 625’s high ductility (elongation ~40%) enables operations like bending, rolling, and deep drawing.
- Due to springback (15–20% higher than 316L), forming dies must compensate with over-bending or tighter tolerances.
- Hot Forming:
-
- Performed at 980–1,090°C (1,800–2,000°F) to reduce yield strength and increase plasticity.
- Rapid air cooling is preferred post-forming to retain the alloy’s microstructure and avoid sensitization.
Additive Manufacturing (AM)
- Process Compatibility: Inconel 625 is ideal for Laser Powder Bed Fusion (LPBF) and Electron Beam Melting (EBM) due to its weldability, thermal fatigue resistance, and homogenous microstructure.
SLM 3D Metal Printer Inconel 625 Product - Build Parameters:
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- Laser Power: 150–200 W
- Scan Speed: 800–1,000 mm/s
- Performance: AM-fabricated components can reach 95% of the strength of wrought products, making them suitable for mission-critical applications (e.g., aerospace fuel nozzles, marine heat exchangers).
- Post-Processing:
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- Hot Isostatic Pressing (HIP): Conducted at 1,100°C / 100 MPa to close internal porosity and ensure near-full density (~99.9%).
- Solution annealing and surface finishing may follow to optimize mechanical and corrosion properties.
7. Applications of Inconel 625
Inconel 625 is prized for its exceptional resistance to corrosion, oxidation, fatigue, and high-temperature creep—making it indispensable in extreme environments where conventional materials fail.

Aerospace and Aviation
- Exhaust ducts
- Turbine shrouds and seals
- Thrust-reverser systems
- Fuel and hydraulic lines
Inconel 625 offers excellent oxidation resistance up to 1,093°C (2,000°F), and its ability to resist thermal fatigue makes it ideal for jet engine components and high-altitude structural systems.
Oil and Gas Industry
- Downhole tubing and tools
- Flexible risers and manifolds
- Offshore platform piping
- Bellows and expansion joints
Inconel 625 is extensively used in subsea and sour gas environments due to its exceptional resistance to pitting, crevice corrosion, and stress-corrosion cracking—even in high-chloride, high-pressure conditions.
Chemical and Petrochemical Processing
- Heat exchangers and columns
- Reactors and scrubbers
- Piping and pressure vessels
- Flare stacks and incinerator parts
The alloy’s resistance to a broad range of acids (e.g., nitric, phosphoric, sulfuric) and aggressive chemicals enables safe long-term operation in corrosive process streams at both ambient and elevated temperatures.
- Seawater piping systems
- Pump housings and impellers
- Submarine hull fasteners and cable sheathing
Thanks to its excellent seawater resistance, Inconel 625 is used in saltwater-exposed applications such as naval vessel fittings, offshore structures, and undersea cables.
Power Generation
- Steam line bellows
- Turbine and boiler components
Inconel 625 resists intergranular corrosion and irradiation embrittlement, making it suitable for high-temperature nuclear reactor parts and heat exchangers in power plants.
Environmental Engineering
- Waste gas treatment units
- Flue gas desulfurization systems (FGD)
- Incineration components
It provides superior life in systems handling acidic gases and hot flue exhaust, especially where chlorine or sulfur compounds are present.
Additive Manufacturing and Custom Fabrication
- Turbine nozzles and combustion liners
- Biomedical implants and surgical tools (non-implant grades)
- Customized heat shields and ducts
The alloy’s weldability and resistance to cracking under rapid thermal cycles make it ideal for complex, high-performance components produced via LPBF and DMLS (Direct Metal Laser Sintering).
8. Advantages and Limitations
Advantages of Inconel 625
Exceptional Corrosion Resistance
Inconel 625 offers outstanding resistance to a wide range of corrosive environments, including seawater, acidic media (e.g., nitric, phosphoric, and sulfuric acids), and chlorides.
This makes it ideal for marine, offshore, and chemical processing applications.
High Strength Without Heat Treatment
Unlike precipitation-hardened alloys like Inconel 718, Inconel 625 is strengthened by solid solution mechanisms, meaning it maintains excellent mechanical strength without requiring complex aging or hardening processes.
Excellent Weldability
Inconel 625 exhibits superior weldability compared to many other superalloys and stainless steels.
It resists post-weld cracking, and welded joints retain high strength and corrosion resistance, making it suitable for pressure vessels, piping, and structural components.
High Temperature Performance
It retains mechanical properties at elevated temperatures up to approximately 1,093°C (2,000°F), making it suitable for aerospace, heat exchangers, and furnace components.
Fatigue and Creep Resistance
Good resistance to fatigue, creep, and rupture under cyclic thermal and mechanical loading makes Inconel 625 a reliable material for demanding, high-stress environments.
Cryogenic Capability
Inconel 625 maintains ductility and toughness at cryogenic temperatures (as low as −196 °C), making it suitable for LNG systems and other low-temperature applications.
Limitations of Inconel 625
- High Cost: Raw material ($60–80/kg) is 10–15× that of 316L; machining adds 40–50% to fabrication costs.
- Lower High-Temp Strength Than 718: At 650°C, Inconel 718 has 20–30% higher tensile strength, limiting 625’s use in ultra-high-stress turbine components.
- Work Hardening: Machining requires specialized tools and slower speeds, increasing production time.
9. Inconel 625 vs Other Alloys
| Feature | Inconel 625 | Inconel 718 | Hastelloy C-276 | 316L Stainless Steel |
| Composition | Ni-Cr-Mo-Nb; solid-solution strengthened | Ni-Cr-Fe-Nb-Ti; precipitation hardened | Ni-Mo-Cr-Fe; high Mo content | Fe-Cr-Ni-Mo; austenitic stainless |
| Primary Strength Mechanism | Solid solution strengthening (Mo, Nb) | Precipitation hardening (γ’ and γ” phases) | Solid solution + carbide precipitates | Work hardening and solid solution |
| Temperature Range | -270°C to ~1093°C (high temperature stability) | Up to ~700°C | ~982°C | Up to ~870°C |
| Corrosion Resistance | Excellent resistance to pitting, crevice, and stress corrosion in chloride and oxidizing environments | Good corrosion resistance, less resistant in chloride environments | Exceptional resistance to oxidizing and reducing acids | Moderate corrosion resistance, susceptible to chloride pitting |
| Mechanical Strength | High strength, retains ductility at elevated temps | Higher strength at room and moderate temps | Good strength, less than Inconel 718 | Lower strength compared to superalloys |
Weldability |
Excellent; minimal post-weld heat treatment needed | Good but requires precise post-weld heat treatment | Good, but sensitive to welding defects | Excellent and easy to weld |
| Work Hardening | Rapid work hardening during machining | Moderate | Moderate | Lower work hardening |
| Cost | High due to alloying and machining difficulty | High, slightly more expensive due to complex heat treatment | Very high, due to Mo and other expensive elements | Lower cost compared to superalloys |
| Applications | Aerospace, marine, chemical, nuclear, power plants | Aerospace, gas turbines, nuclear reactors | Chemical processing, pollution control, aerospace | General industrial, food processing, medical |
10. Internationally Equivalent grades for Inconel 625
| Standard System | Equivalent Grade/Designation | Notes |
| UNS (USA) | N06625 | Standard UNS number |
| EN (Europe) | 2.4856 | European material number |
| JIS (Japan) | NCF625 | Japanese Industrial Standard |
| GB (China) | N06625 | Same as UNS number |
| DIN (Germany) | XNiCrMoNb25-20-5 | German material designation |
| ASTM | B443, B444 | Common ASTM specifications for bars and tubes |
11. Conclusion
Inconel 625 remains one of the most versatile and reliable superalloys in engineering, offering unmatched corrosion resistance and high-temperature performance with excellent fabricability.
Though costly, its lifecycle benefits, especially in critical environments, often justify its selection over cheaper alternatives.
FAQs
Is Inconel 625 a stainless steel?
No, Inconel 625 is a nickel-based superalloy, not a stainless steel. It offers superior high-temperature and corrosion resistance compared to stainless steels.
What is the maximum continuous operating temperature for Inconel 625?
It performs reliably up to 1,093°C (2,000°F) for continuous service, with short-term exposure to 1,200°C (2,192°F) possible in non-critical applications.
Is Inconel 625 magnetic?
No. Its fully austenitic (FCC) microstructure remains non-magnetic in all conditions, unlike ferritic or martensitic alloys.
Can Inconel 625 be used in seawater long-term?
Yes. Its corrosion rate in seawater is <0.01 mm/year, with a service life exceeding 25 years in subsea applications (e.g., offshore oil manifolds).
How does Inconel 625 compare to Inconel 718?
625 offers superior corrosion resistance and broader temperature range, while 718 provides higher strength at 600–650°C. 625 is better for chemical processing; 718 for high-stress aerospace components.
Why is Inconel 625 preferred for welding?
Its solid-solution strengthening avoids brittle precipitates in the HAZ, and welded joints retain 90% of base metal strength without post-weld heat treatment—unlike many superalloys.
Alloy 625
Inconel composition
“Inconel” refers to a family of nickel-chromium-based superalloys. Common elements include Ni, Cr, Mo, Fe, Nb, Ti, and Al. Composition varies by grade (e.g., 600, 625, 718).



