For components that must sustain very high temperatures, severe oxidation, or concentrated chemical attack, choose Inconel (nickel-chromium superalloys). For parts where weight reduction, high specific strength, and biocompatibility matter, choose titanium alloys (notably Ti-6Al-4V). Each metal family solves different engineering problems; selection must be made from component-level requirements: service temperature, environment, fatigue regime, manufacturability, and cost.
Why these two metals are compared
Inconel and titanium often appear on shortlist stages for high-performance engineering parts because both resist corrosion and provide strength beyond ordinary steels. They differ strongly in density, thermal limits, and alloy chemistry, resulting in tradeoffs between weight, heat resistance, and fabrication. Understanding those tradeoffs prevents costly material misselection.
High-level chemistry and families
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Inconel — family of nickel-based superalloys with significant chromium, molybdenum, niobium/tantalum and sometimes iron. Designed to form stable oxide layers and retain mechanical strength at elevated temperatures. Common grades: Inconel 625 (corrosion resistance), Inconel 718 (high strength at elevated temperature).
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Titanium alloys — primarily titanium with alloying elements like aluminum and vanadium. Ti-6Al-4V (Grade 5) is the workhorse: excellent specific strength, good corrosion resistance, and widely used in aerospace and biomedical fields.
Key material properties
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Density / weight: Titanium alloys are much lighter; Ti-6Al-4V density ≈ 4.43 g/cm³. Inconel densities commonly exceed 8.0 g/cm³ (nickel base), producing heavier components for the same volume. That yields strong motivation for titanium where mass matters.
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Strength at room temperature: Both deliver high tensile/yield strength, but titanium offers a superior strength-to-weight ratio. Inconel often shows higher absolute strength when heat treated (e.g., Inconel 718) and maintains strength at temperatures where titanium softens.
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High-temperature performance: Inconel retains mechanical integrity and oxidation resistance at temperatures far above those usable for titanium alloys; superalloys are chosen for turbine hot sections and exhaust. Titanium alloys typically recommended up to roughly 350°C service for Ti-6Al-4V; beyond that strength and creep resistance drop substantially.
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Corrosion resistance: Both resist many corrosive environments. Inconel shows exceptional resistance to oxidizing, reducing, and chloride environments, often outperforming titanium in certain chemical exposures. Titanium forms a tenacious oxide film granting outstanding resistance to seawater and many acids, yet some halogenated acids and hot chlorine can attack it. Choose by chemistry and environment.
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Fatigue & creep: Titanium has good fatigue properties for weight-sensitive designs; Inconel exhibits superior creep resistance at elevated temperatures and is favored where long-term load and heat cause time-dependent deformation.
Compact comparison table — practical numbers and effects
Characteristic | Typical Inconel (718/625) | Ti-6Al-4V (Grade 5) | Practical impact |
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Density | ~8.1–8.5 g/cm³ (nickel base) | ~4.43 g/cm³ | Titanium halves the mass of an Inconel part for equal volume. |
Tensile strength (annealed/aged) | 700–1,400 MPa (varies by grade/HT) | 850–1,200 MPa (heat treated) | Absolute strength similar in some heat-treated alloys; weight differs. |
Service temperature | Up to 700°C+ for short terms; some alloys perform beyond. | Recommended up to ~350°C for Ti-6Al-4V; properties degrade at higher temperature. | |
Oxidation/corrosion | Very high at elevated temperature; forms protective oxides. | Excellent in many media; native oxide gives seawater resistance; vulnerable to certain halogens. | |
Weldability | Good for many grades, but requires control (post-weld heat treat for 718). | Excellent with proper shielding; reactive metal requires inert gas and clean surface. | |
Machinability | Difficult; work-hardening and toughness require special tooling. | Challenging too (galling, springback) but easier than some superalloys. | |
Cost | High (superalloy processing, dense) | High (raw titanium costs, processing) | Both are premium; titanium may carry higher raw-material cost per kg but weight savings affect total system cost. |
Typical uses | Gas turbines, exhaust, chemical service, high-temp fasteners. | Airframe structure, surgical implants, racing parts, marine components. |
(Numbers are representative; always consult datasheets and supplier certifications for design.)
Detailed engineering considerations
Temperature and creep resistance
Inconel alloys were developed specifically for stable strength at elevated temperature and for resistance to oxidation and thermal fatigue. High nickel and chromium contents produce a stable oxide scale and slow microstructural degradation under heat and stress. For components that operate at steady or cyclic temperatures above 400–500°C, Inconel frequently outperforms titanium.
Titanium allloys deliver very good strength at lower temperatures but suffer increasing creep and loss of stiffness when pushed toward 400°C or beyond. Design standards typically limit Ti-6Al-4V continuous service to near 350°C.
Strength-to-weight and structural efficiency
Because titanium’s density nearly equals half of Inconel’s, titanium yields exceptional structural efficiency where mass reduction improves system performance (aircraft, high-performance motorsport, selective robotics). When the limiting factor is inertia, center of gravity, or payload, titanium often becomes the economic choice despite higher per-kg raw material cost.
Inconel vs Titanium — Price Comparison Table (2025)
Material (typical grade) | Common form | Typical 2025 price (USD / kg) | Typical 2025 price (USD / lb) | Notes & source |
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Inconel 718 (industrial range) | Bar / plate / forgings | $25 – $35 / kg (industrial) | $11.34 – $15.88 / lb | Industrial-grade, China factory-direct listings show ~$25–$35/kg (varies by qty & form). |
Inconel 718 (aerospace / premium) | Aerospace spec plate / certified bar | $44 – $60 / kg | $19.96 – $27.22 / lb | Higher-spec, aerospace-certified lots command the upper range. |
Inconel 625 (sheet — North America Q1 2025 index) | Sheet (DEL Florida) | ~$56.24 / kg | ~$25.51 / lb | Market index example: Alloy 625 sheet price index reported at USD 56,240/MT (~$56.24/kg) for Q1 2025. Regional delivery & sheet thickness affect price. |
Inconel (powder for AM / PM) | Gas-atomized powder (In718 / In625) | $100 – $420 / kg (example: small-pack pricing) | $45.35 – $190.40 / lb | Powder is far higher-cost; example vendor lists ~$111/kg for 10 kg packs; premium spherical powder can exceed $400/kg. Price depends on particle spec & lot size. |
Titanium — Ti-6Al-4V (common aerospace alloy) | Bar / plate / sheet (wrought) | $22 – $66 / kg (equivalent to ~$10–$30 / lb) | $10 – $30 / lb | Market seller ranges for Ti-6Al-4V commonly reported $10–$30/lb (≈ $22–$66/kg), with variation by region, form, and quantity. |
Commercially Pure Titanium (CP-Ti, Grades 1–4) | Plate / sheet / tube | $13 – $22 / kg (approx) | $6 – $10 / lb | CP grades cheaper than aerospace alloys; used for chemical / architecture applications. |
Titanium (powder for AM / Ti-6Al-4V) | Powder (15–45 μm examples) | €94.56 / kg (vendor example) ≈ € / kg shown | (vendor quoted in EUR/kg) | Example European price lists show ~€95/kg for small-batch powder; powder pricing varies by supplier, spec and batch size — expect premium over wrought. |
Notes:
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Currency shown in USD per kg / USD per lb unless explicitly indicated. Conversion used: 1 kg = 2.20462 lb (prices rounded to 2 decimals for clarity).
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Form matters: sheet/plate/bar (wrought) is significantly cheaper than atomized powder. Aerospace-certified material, small quantities, or special lots increase price.
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Regional differences (China factory-direct vs Europe vs USA delivered) change landed cost significantly—always request ex-works, FOB and DDP quotes to compare fairly.
Quick procurement takeaways (2025)
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If weight-sensitive designs favor titanium (Ti-6Al-4V) — but check whether the alloy form and certification you need is available at a competitive price for your qty.
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If service temperature / oxidation / creep favors Inconel, expect higher raw-material cost per kg and higher machining/tooling costs; total system cost must include fabrication and inspection.
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Powder (additive manufacturing): Inconel and titanium powders command large premiums vs wrought stock — specify powder spec and supplier for accurate quotes.
Corrosion behavior and environment matching
Corrosion resistance must be matched to the specific chemistry and temperature. Inconel alloys like 625 resist chloride pitting, reducing acids, and high-temperature oxidation. Titanium excels in seawater and many oxidizing acids; it also has strong biocompatibility, making it common for implants. A materials compatibility check with service fluids at operating temperatures is mandatory.
Fatigue performance and surface treatments
Fatigue life depends on surface finish, residual stresses, geometry, and environment. Titanium fatigue behavior benefits strongly from compressive surface treatments (shot peening, laser peening). Inconel components operating at high temperature must be designed for low-cycle thermal fatigue and may need coatings or internal cooling for long life.
Fabrication, welding and joining
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Inconel: Some grades weld readily with proper filler and heat treatment; others require attention to avoid hot cracking or strain-age phenomena (notably in precipitation-strengthened alloys). Post-weld heat treatment often required for optimal properties.
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Titanium: Welding requires strict cleanliness and high-quality inert shielding to prevent oxygen/nitrogen pickup. When procedures are followed, weld joints achieve high integrity and acceptable strength.
Machining and finishing
Both groups are work-hardening or reactive; cutting tool selection, feed rates, and coolant strategies differ. Inconel is notorious for poor machinability and rapid tool wear; titanium chatters and galling, requiring rigid setups and careful tooling. Expect higher fabrication hours than with carbon steels or stainless steels.
Typical industry use cases and examples
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Aerospace:
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Inconel: hot-section turbine components, combustor liners, exhaust seals.
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Titanium: airframe structural parts, landing gear components (where weight matters), fasteners, and fan-blades in cooler sections.
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Oil & Gas / Chemical:
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Inconel: downhole tools, flue gas environments, heat exchangers, pipework in corrosive streams.
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Titanium: heat exchanger tubing for seawater service, some chemical contact parts where chlorides and oxidizers are moderate.
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Medical:
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Titanium: implants, prosthetics, surgical instruments due to biocompatibility.
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High-performance motorsport and marine:
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Titanium: lightweight suspension, fasteners, exhaust systems (where temps are manageable).
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Inconel: racing exhaust headers that see very high temperatures.
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Procurement, supply chain, and MWAlloys offering
Raw material market dynamics drive lead times and pricing. Both Inconel and titanium are specialty metals with variable availability. MWAlloys sources from certified mills in China, maintains fast-turn stock for common forms (bar, plate, sheet, ring, fasteners), and offers export documentation and mill test reports (MTRs). MWAlloys emphasizes 100% factory pricing, volume discounts, and quick shipments from inventory for many standard sizes. For engineered components, MWAlloys supports cutting, machining, and export packing to customer specification.
How to pick
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If operating temperature > 400–500°C or oxidation/corrosion at high temperature is a driver: pick Inconel.
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If minimizing mass while keeping high stiffness/strength is crucial (airframes, implants): pick titanium.
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If the environment is hot seawater or reducing acids at high temps: favor Inconel for many service cases.
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If fabrication cost, machinability, or standard workshop processes are top concerns: review both; neither will be as cheap or easy as common steels — factor processing into total cost.
Table — quick selection checklist
Requirement | Likely pick |
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Ultra high temperature, oxidation > 500°C | Inconel |
Lowest possible mass for structural parts | Titanium |
Biomedical implant | Titanium |
Long-term creep resistance under load and heat | Inconel |
Seawater heat exchanger tube | Titanium (many cases) or Inconel if chlorides + high T |
High temperature fasteners | Inconel |
Rapid prototyping with additive manufacturing | Both possible; powder availability and process windows differ |
Surface treatments, coatings, and lifecycle tips
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Inconel: coatings seldom required for oxidation resistance but thermal barrier coatings help reduce thermal fatigue in turbine parts. Regular inspection for surface cracking in thermal cycles recommended.
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Titanium: anodizing improves cosmetic finish and slightly alters corrosion behavior; nitriding and hard coatings can reduce wear for sliding contacts. Prevent fretting and galling through appropriate bearing surfaces or coatings.
Frequently Asked Questions
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Which is stronger: Inconel or titanium?
Strength depends on which grade and heat treatment. Inconel 718 can achieve very high absolute strength, particularly after age-hardening. Titanium alloys offer higher specific strength (strength per unit weight), making them stronger for mass-sensitive designs. -
Can I use titanium in a jet engine hot section?
No. Titanium cannot withstand the sustained high temperatures inside turbine hot sections. Inconel and other nickel superalloys are used there for retention of strength, oxidation resistance, and creep resistance. -
Which alloy resists seawater better?
Titanium offers excellent seawater resistance and is common for condensers and heat exchanger tubing. Inconel also resists many marine environments; selection depends on temperature, flow, and local chemistry. Perform corrosion testing for critical service. -
What about cost differences?
Both are premium materials. Titanium raw prices track different market drivers than nickel superalloys. For an apples-to-apples comparison, evaluate total system cost: material, fabrication, weight-related savings, and maintenance. -
Are both suitable for additive manufacturing?
Yes. Inconel and Ti-6Al-4V powders are commonly used in powder bed fusion and directed energy deposition, but process parameters, powder quality, and post-processing differ. -
Which one is easier to weld?
Welding requires controls for both. Inconel often needs filler and post-weld heat treatment for precipitation-strengthened grades. Titanium needs immaculate shielding gas coverage to prevent contamination. With correct procedure, both produce sound welds. -
Which corrodes in acids or chlorides?
Inconel-grade 625 resists many aggressive acids and chloride attack better than titanium in coated or hot chloride environments. Titanium resists many oxidizing conditions but can be vulnerable in hot halogenated streams. Match chemistry and temperature to alloy. -
Which has better fatigue life?
Fatigue depends on geometry, surface finish, and environment. Titanium often shows excellent fatigue performance when properly treated. Inconel retains fatigue resistance at elevated temperatures where titanium would lose performance. -
Is titanium biocompatible?
Yes. Titanium and many titanium alloys are widely used in implants and prosthetics for their alloy stability and osseointegration. -
Where can I buy reliable stock and fast delivery?
Choose suppliers who provide mill test reports, traceability, and inventory programs. MWAlloys maintains factory direct pricing, stocked items, and export documentation for global customers requiring Inconel and titanium shapes and machined parts.