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X10CrNi18-8 Stainless Steel and Maraging Steel for CNC Machining

X10CrNi18-8 is often selected when a stainless CNC part needs corrosion resistance, elasticity, thin-section strength, or reliable forming history. Maraging steel is selected for a different reason: it gives extremely high strength after aging while remaining relatively machinable before heat treatment. This guide explains both materials from a CNC machining perspective, with attention to part design, material properties, machining risks, and the questions engineers usually raise before ordering custom machined components.

What Is X10CrNi18-8 Stainless Steel?

Before discussing CNC machining, it is useful to define the material clearly. X10CrNi18-8 is a European stainless steel designation used for an austenitic chromium-nickel alloy. It is commonly associated with material number 1.4310 and is often compared with AISI 301 or related spring stainless steel grades. The name describes its approximate chemistry: carbon around 0.10%, chromium near 18%, and nickel near 8%, although real specifications use allowable ranges rather than one fixed value.

x10crni18 8 stainless steel

Grade Definition and Equivalent Names

In engineering drawings, the grade may appear as X10CrNi18-8, 1.4310, AISI 301, SUS 301, or a supplier-specific stainless spring steel name. These names are not always perfectly interchangeable because standards, delivery forms, heat treatments, and temper conditions can change the final strength. For CNC machining projects, the safest approach is to confirm both the grade and the supply condition, especially when the part has thin walls, spring features, tight slots, or post-machining forming requirements.

Why This Grade Is Often Described as Spring Stainless Steel

X10CrNi18-8 is valued because it work-hardens strongly during cold working. This makes it suitable for spring strips, clips, flexible plates, retaining elements, and precision components that need better strength than common soft austenitic stainless steel. In CNC machining, this same work-hardening behavior is both an advantage and a challenge: it improves strength in the final part, but it also requires sharp tools, stable cutting, and careful heat control.

Main Performance Profile

The material combines useful corrosion resistance, high cold-worked strength, good elasticity, and non-hardenability by conventional quenching. It is not chosen for the same reason as heat-treatable tool steels or ultra-high-strength maraging steel. Instead, it is preferred where a stainless part must keep a clean surface, maintain moderate corrosion resistance, and withstand repeated elastic loading or assembly stress.

Where It Differs from Common 304 Stainless Steel

Many buyers compare X10CrNi18-8 with 304 stainless steel. X10CrNi18-8 generally offers stronger work-hardening and better spring behavior, while 304 is often easier to source as general-purpose bar or plate. If the part only needs corrosion resistance and simple machining, 304 may be enough. If the design needs spring force, clips, thin resilient features, or high strength from cold working, X10CrNi18-8 becomes more attractive.

Is X10CrNi18-8 Commonly Used for CNC Machining?

X10CrNi18-8 is not the easiest stainless steel to machine, but it is used in CNC machining when the final part benefits from its strength, elasticity, and stainless behavior. It is more common in strip, wire, sheet, and precision spring applications than in large heavy blocks. However, CNC milling, turning, drilling, tapping, and wire cutting can be used when the part requires accurate holes, slots, threads, profiles, or mating surfaces that cannot be achieved by forming alone.

CNC Machining Suitability

The material can be CNC machined, but it should be treated as a work-hardening austenitic stainless steel rather than as free-cutting stainless steel. Its machinability is usually described as medium. Cutting parameters must keep the tool engaged and avoid rubbing, because rubbing can harden the surface and make the next pass more difficult. This is especially important for small precision parts where burrs, tool marks, and hole quality affect assembly.

When CNC Is Used Instead of Stamping or Forming

CNC machining is selected when the part has details that are too accurate, too three-dimensional, or too costly to make by sheet forming alone. Examples include milled pockets, accurate bearing seats, counterbores, threaded holes, controlled edge breaks, flat sealing faces, and small batches where tooling cost is not justified. CNC is also useful for prototype validation before a buyer invests in stamping tools or progressive die production.

Typical CNC Machined Parts

The common CNC applications for X10CrNi18-8 are usually smaller precision components rather than large structural blocks. The grade is suitable for stainless spring-like parts, thin brackets, retaining plates, connector components, medical or instrument parts, wear-resistant clips, precision washers, and compact mechanical elements exposed to moderate corrosion. The following examples show where CNC machining can add value beyond basic material supply.

Feature-Level Examples for Engineers

In real projects, the material choice is often driven by a feature rather than by the whole part name. A clip may need a precisely machined slot to control deflection. A retaining plate may need tight hole position for assembly. A thin stainless spring element may need a burr-free edge to avoid fatigue initiation. A connector part may need accurate threads and a clean surface finish. These feature requirements are where CNC machining becomes relevant.

CNC Part Type Why X10CrNi18-8 Is Used Important CNC Features
Spring clips and retaining plates Elasticity, stainless surface, cold-worked strength Slots, holes, burr-free edges, controlled thickness
Small brackets and supports Strength in thin sections with corrosion resistance Profiles, tapped holes, counterbores, flat mounting faces
Instrument and sensor parts Clean surface and stable precision Small holes, threads, pockets, fine surface finish
Precision washers and spacers Wear resistance and dimensional consistency OD/ID turning, flatness, chamfer control
Connector components Stainless behavior and repeatable assembly Threads, grooves, mating faces, deburring

 

Chemical Composition of X10CrNi18-8 and Maraging Steel

Chemical composition explains why these two materials behave so differently during CNC machining. X10CrNi18-8 is an austenitic stainless steel based on chromium and nickel. Maraging steel is a low-carbon, nickel-rich martensitic alloy strengthened by aging reactions involving elements such as cobalt, molybdenum, titanium, and aluminum. Because standards and suppliers may use slightly different limits, the following ranges should be treated as typical reference values for engineering comparison.

X10CrNi18-8 Typical Chemical Composition

The stainless behavior of X10CrNi18-8 comes mainly from chromium, while nickel stabilizes the austenitic structure and supports ductility. Carbon is higher than in some common austenitic stainless grades, which helps strength but also requires attention to corrosion and heat exposure. The grade is normally selected for balanced corrosion resistance and mechanical resilience, not for maximum chemical resistance in aggressive environments.

Key Elements and Their CNC Relevance

For CNC machining, chromium and nickel improve corrosion behavior but also contribute to stainless steel cutting challenges. Carbon and cold-worked condition affect hardness and cutting force. Sulfur is typically limited, so chip breaking is not as easy as in free-machining stainless grades. This explains why X10CrNi18-8 often needs more careful tool choice than simple carbon steel or free-cutting alloys.

Element Typical Range Role in Material Behavior
Carbon (C) 0.05-0.15% Raises strength; excessive heat may increase corrosion sensitivity
Chromium (Cr) 16.0-19.0% Provides stainless corrosion resistance
Nickel (Ni) 6.0-9.5% Stabilizes austenite and supports ductility
Manganese (Mn) Max 2.00% Supports deoxidation and austenite stability
Silicon (Si) Max 2.00% Improves oxidation resistance and steelmaking control
Molybdenum (Mo) Max 0.80% May support corrosion resistance depending on specification
Nitrogen (N) Max 0.10% Can strengthen austenitic stainless steel
Sulfur (S) Low limit Low sulfur improves quality but reduces chip-breaking ease

 

Maraging Steel Typical Chemical Composition

Maraging steel has a very different alloy design. Instead of using carbon as the primary strengthening element, it relies on a low-carbon martensitic matrix and precipitation hardening during aging. The most common CNC discussion uses 18Ni maraging grades such as 18Ni(250), 18Ni(300), or 18Ni(350). Among them, maraging 300 is often used as a reference for ultra-high-strength CNC parts.

Why Low Carbon Matters in Maraging Steel

Low carbon helps maraging steel remain tough, weldable, and relatively stable during machining in the solution-treated or annealed condition. After CNC machining, aging can greatly increase strength and hardness without the severe distortion often associated with conventional quench-and-temper steels. This is one reason engineers choose maraging steel when they need both tight machining accuracy and very high final strength.

Element Typical 18Ni(300) Range Role in Material Behavior
Nickel (Ni) 18.0-19.0% Forms the nickel-rich maraging system and supports toughness
Cobalt (Co) 8.5-9.5% Strengthens aging response and final hardness
Molybdenum (Mo) 4.7-5.2% Contributes to precipitation hardening
Titanium (Ti) 0.5-0.8% Forms strengthening precipitates during aging
Aluminum (Al) Small addition Supports aging reaction and precipitation
Carbon (C) Usually <=0.03% Kept low to preserve toughness and weldability
Iron (Fe) Balance Base metal matrix

 

Physical and Mechanical Properties

Property data must always be tied to product form and heat treatment. X10CrNi18-8 can vary widely because cold working changes strength and hardness. Maraging steel also varies dramatically before and after aging. For CNC projects, the supplier should know whether the part will be machined in a soft condition, cold-worked condition, aged condition, or finished after heat treatment. The tables below give useful planning ranges rather than one guaranteed value.

X10CrNi18-8 Property Profile

X10CrNi18-8 has a density close to many stainless steels and a relatively low thermal conductivity compared with carbon steel or aluminum. This means heat can concentrate at the cutting edge during machining. Its mechanical strength depends heavily on temper and cold work. Soft or solution-annealed material is easier to machine, while cold-worked spring material can be much harder on tools.

CNC Meaning of These Properties

Low thermal conductivity increases the need for coolant and sharp cutting edges. High work-hardening tendency means the tool should cut cleanly instead of rubbing. Strong cold-worked conditions may improve final part strength but increase tool wear, burr formation, and cutting force. These properties explain why quoting X10CrNi18-8 CNC parts requires more detail than simply naming the grade.

Property Typical Value or Range CNC Machining Meaning
Density About 7.9 g/cm3 Similar weight class to common stainless steels
Elastic modulus About 200 GPa Good stiffness for thin precision parts
Thermal conductivity About 15 W/m-K Heat stays near the cutting zone
Thermal expansion About 16 x 10-6/K at low temperature range Dimension control needs stable temperature
Hardness Often below 230 HB in softer condition; higher when cold worked Condition strongly affects tool wear
Tensile strength Approx. 500-900 MPa or higher in hard tempers Strength depends on cold work and delivery form
Elongation Can be high in soft condition and lower in hard tempers Affects burr behavior and forming after machining

 

Maraging Steel Property Profile

Maraging steel is known for its exceptional strength after aging. In the solution-treated condition it is much easier to machine than its final strength would suggest. After aging, it can reach very high tensile strength and hardness, making it suitable for demanding precision parts. This two-stage behavior is central to CNC process planning.

Why Heat Treatment Changes the Quotation

A maraging steel quote must consider whether the part will be rough machined, aged, and finish machined, or fully machined before aging. Aging distortion is usually lower than conventional hardening distortion, but it is not zero. Critical bores, flatness, grinding allowance, and final inspection method should be planned before production starts.

Property Typical Value or Range CNC Machining Meaning
Density About 8.0-8.1 g/cm3 Slightly heavier than many stainless steels
Elastic modulus About 180-200 GPa High stiffness for precision load-bearing parts
Hardness after aging Often around HRC 50+ depending on grade Finish machining becomes more difficult
Ultimate tensile strength after aging Approx. 1700-2100+ MPa depending on grade Used where ordinary stainless steel is not strong enough
Yield strength after aging Can exceed 1600 MPa depending on grade Supports compact high-load designs
Elongation after aging Lower than soft stainless, grade-dependent Stress concentration and radii must be controlled
Corrosion resistance Limited compared with stainless steel Surface protection may be needed

 

Why Engineers Choose Maraging Steel for CNC Machined Parts

Engineers normally choose maraging steel for CNC parts when ordinary stainless steel, alloy steel, or aluminum cannot meet strength, toughness, or dimensional stability requirements. It is not chosen as a general corrosion-resistant material. It is chosen because a machined component can be produced in a relatively machinable condition and then aged to reach very high strength. This makes it attractive for compact, high-load, high-precision components.

Ultra-High Strength After Aging

The main reason to choose maraging steel is its final strength-to-size advantage. A smaller component can carry higher load, which helps when the design envelope is limited. In CNC machining, this is valuable for tooling inserts, high-load shafts, precision couplings, aerospace-type mechanisms, test fixtures, motorsport components, and other parts where failure margin matters more than material cost.

Prototype to Functional Component

Maraging steel is also attractive when a prototype must behave like a real high-strength production component. A designer can machine the part, inspect the geometry, age it, and then test it under realistic load. This reduces the gap between prototype appearance and functional performance. For buyers, the most important point is to specify the required final condition, not only the material name.

Stable Machining Before Heat Treatment

Another common reason is the process route. Many high-strength steels are difficult to machine once hardened. Maraging steel can often be machined before aging with better control, then hardened by aging with relatively low distortion. This allows CNC shops to produce accurate features before the material reaches its final strength level.

Accuracy Planning After Aging

Even though maraging steel is known for dimensional stability, precision parts still need planning. A supplier may leave small stock on critical features, age the part, then finish grind, mill, turn, or polish the final surfaces. This is especially important for bores, sealing faces, guide surfaces, and tight mating features. The process sequence should be matched to the drawing tolerance, not chosen only from a generic material datasheet.

Common CNC Machined Components for Both Materials

X10CrNi18-8 and maraging steel are both used for precision CNC parts, but their application logic is different. X10CrNi18-8 is used when corrosion resistance, elasticity, and thin-section strength matter. Maraging steel is used when very high strength and controlled heat treatment are more important than stainless corrosion resistance. Understanding this difference helps prevent over-specification and unnecessary cost.

X10CrNi18-8 CNC Component Examples

The strongest fit for X10CrNi18-8 is a component that needs stainless appearance, moderate corrosion resistance, and elastic or spring-like behavior. It is especially useful for parts that combine formed stock with CNC finishing. CNC machining can add the critical geometry that makes the part assemble correctly or perform consistently.

Examples by Industry Use

Typical parts include spring clips for instruments, precision retaining plates, sensor brackets, stainless washers, compact connector parts, small covers, thin support frames, medical device hardware, packaging machinery parts, and electrical contact supports. In these parts, the key CNC value is often burr control, hole accuracy, edge quality, and flatness rather than heavy material removal.

Maraging Steel CNC Component Examples

Maraging steel parts are usually specified for higher mechanical demand. The material is more expensive, so it should be used where the design gains real performance from the strength and aging response. CNC machining is common because the parts often require tight geometry before and after heat treatment.

Examples by Performance Requirement

Typical maraging steel CNC parts include high-load shafts, precision tooling components, mold inserts, aerospace-type brackets, robotics transmission parts, load-bearing pins, testing fixtures, couplings, high-strength fastener-like custom parts, and motorsport components. The shared requirement is not decorative finish; it is controlled strength, fatigue resistance, and dimensional reliability under load.

CNC Machinability Comparison Between X10CrNi18-8 and Maraging Steel

A direct CNC machinability comparison is useful because both materials can appear in precision mechanical designs, yet they behave very differently at the machine. X10CrNi18-8 challenges the machinist through work hardening, gummy chip behavior, burrs, and heat concentration. Maraging steel is often easier before aging, but much more demanding after aging. The best material is therefore not the one with the highest strength; it is the one that matches the working environment, geometry, cost, and inspection plan.

Cutting Behavior and Tooling Risk

The cutting behavior of X10CrNi18-8 is closer to austenitic stainless steel: it can smear, harden at the surface, and create stringy chips. Maraging steel in the solution-treated condition cuts more predictably, but aged maraging steel requires hard-material strategies. A buyer should tell the supplier the required final condition because the same maraging grade can have two very different machining difficulty levels.

Machinability Comparison Table

The table below compares the two materials from a shop-floor perspective. It focuses on risk factors that affect CNC quotation, tool life, lead time, and final part quality. These comparisons are general; exact results depend on bar condition, hardness, geometry, machine rigidity, coolant, and tool supplier recommendations.

Factor X10CrNi18-8 Stainless Steel Maraging Steel
Main CNC challenge Work hardening, burrs, heat, chip control Heat-treatment sequence and aged hardness
Best machining condition Softer or controlled temper when possible Solution-treated before aging
Tooling approach Sharp carbide tools, positive geometry, strong coolant Carbide for pre-aging; hard-material tools after aging
Dimensional risk Heat and burrs affect small features Aging movement and final hardness affect finishing
Surface finishing Polishing or passivation can improve corrosion behavior Protection may be needed because it is not stainless
Cost driver Cycle time, tool wear, burr removal Material cost, heat treatment, finish machining
Best fit Elastic stainless precision parts Ultra-high-strength precision parts

 

Cost and Selection Risk

Selecting maraging steel when X10CrNi18-8 is enough can make the part unnecessarily expensive. Selecting X10CrNi18-8 when maraging steel is required can create a strength or fatigue risk. The key is to define the real requirement: corrosion resistance, elastic behavior, compact strength, final hardness, heat-treatment stability, or surface appearance. Once the requirement is clear, CNC process planning becomes much more reliable.

Selection Matrix for CNC Projects

A simple selection matrix helps avoid material overuse. X10CrNi18-8 is usually better for stainless spring behavior and moderate corrosion exposure. Maraging steel is better for high-load precision parts where the design cannot become larger or heavier. When both strength and corrosion resistance are required, surface protection, alternate stainless grades, or design changes may need to be evaluated.

Requirement Better First Choice Reason
Stainless corrosion resistance X10CrNi18-8 Chromium-nickel stainless structure
Spring-like thin feature X10CrNi18-8 Strong work-hardening and elasticity
Very high final strength Maraging steel Aging creates ultra-high strength
Lower heat-treatment distortion Maraging steel Aging is generally more stable than quench hardening
Lowest material cost Depends on market and form X10CrNi18-8 is often cheaper, but geometry affects total cost
Clean polished stainless appearance X10CrNi18-8 Better natural stainless surface behavior

 

CNC Machining Challenges of X10CrNi18-8

The main machining difficulty of X10CrNi18-8 comes from its austenitic stainless behavior. It can work harden quickly when the tool rubs instead of cuts. It also has low thermal conductivity, so cutting heat tends to stay near the tool edge. Thin parts can vibrate or distort under clamping. These issues do not make the grade unsuitable for CNC machining, but they do require a stable process.

Work Hardening During Cutting

Work hardening is one of the most common concerns. If the feed is too light, the tool may slide over the surface and create a hardened layer. The next pass then cuts a harder surface, increasing tool wear and making the finish worse. This is especially risky in drilling, reaming, internal turning, slotting, and repeated finishing passes on small features.

Cutting Strategy to Reduce Work Hardening

A good strategy uses sharp carbide tools, adequate feed per tooth, positive rake geometry, and enough depth of cut to stay below the previously affected surface. Coolant should reach the cutting zone. Peck drilling should remove chips without excessive rubbing. For slots and pockets, tool engagement should be controlled to prevent heat spikes. The goal is simple: cut cleanly, evacuate chips, and avoid dwelling.

Chip Control, Burrs, and Heat

X10CrNi18-8 may create long chips and stubborn burrs. Burrs are not just cosmetic; on spring clips, small washers, and connector parts, burrs can change fit, damage mating parts, or create stress concentration. Heat also affects surface finish and dimensional stability, particularly in small thin parts where the material cannot absorb much thermal load.

Coolant and Deburring Measures

Flood coolant, high-pressure coolant where available, sharp tool edges, optimized chip breakers, and stable clamping help control heat and chips. Deburring should be planned as part of the manufacturing route rather than treated as an afterthought. For functional edges, drawings should define acceptable edge break, burr limits, and surface finish. This prevents excessive manual deburring that could change dimensions.

CNC Machining Challenges of Maraging Steel

Maraging steel is often described as machinable before aging, but this does not mean it is simple. The challenge is process control across material condition, heat treatment, final hardness, and inspection. A part that is easy to rough machine before aging can become expensive if the final drawing requires tight tolerances on surfaces that must be machined after aging. CNC planning must therefore include the full route, not only cutting parameters.

Aging Heat Treatment Planning

Aging is the step that gives maraging steel its high final strength. The process is usually less distortion-prone than quench hardening, but dimensional movement can still matter for tight-tolerance CNC parts. Critical features may need finishing allowance. Thin sections, sharp corners, uneven mass, and asymmetric geometry should be reviewed because they can influence stress distribution and final measurement results.

Recommended Process Sequence

A common route is rough machining in the softer condition, stress relief or intermediate stabilization if needed, aging, and then finish machining or grinding of critical features. Some parts can be fully machined before aging if tolerances allow. For precision parts, it is safer to identify datum surfaces, bores, threads, and contact faces that need post-aging verification or finishing.

Tool Wear and High Hardness After Aging

After aging, maraging steel becomes much harder and stronger. Cutting forces rise, tool wear increases, and surface finish becomes more difficult to control. Small tools used for fine slots, threads, or deep features may be at higher risk. If a drawing requires post-aging machining, the quote should reflect slower speeds, more rigid setups, better tooling, and additional inspection.

Finish Machining Strategy

For hard-condition finishing, the process may use coated carbide, ceramic or other hard-material tooling where appropriate, grinding, EDM for specific features, or polishing for contact surfaces. The best solution depends on geometry and tolerance. Designers can reduce machining risk by adding radii, avoiding unnecessary sharp internal corners, and specifying only the surfaces that truly need the tightest tolerance.

Quality Control and Design Considerations for CNC Projects

Material selection alone does not guarantee a good CNC part. X10CrNi18-8 and maraging steel both need clear drawings, realistic tolerances, and process-aware inspection. For X10CrNi18-8, the major quality concerns are burrs, surface finish, work-hardened layers, flatness of thin parts, and corrosion-related finishing. For maraging steel, the major concerns are heat-treatment condition, final hardness, dimensional change, and post-aging verification.

Tolerances and Surface Finish

Tolerances should be assigned according to function. A thin stainless spring clip may need tight width, slot, and edge quality, but not tight tolerance on every non-functional edge. A maraging steel shaft may need tight diameter and runout, but not unnecessary micro-tolerances on hidden relief areas. Over-tolerancing increases CNC cost and can make a good material look unsuitable.

Inspection Points to Confirm

Important inspection points include material certificate, hardness condition, hole size, thread quality, flatness, perpendicularity, surface roughness, burr condition, and final heat-treatment status. For maraging steel, hardness and aging condition should be documented. For X10CrNi18-8, surface finish and edge quality should be checked carefully because they influence corrosion behavior and fatigue life in flexible parts.

Surface Finishing and Corrosion Behavior

X10CrNi18-8 has stainless corrosion resistance, but machining marks, embedded particles, heat tint, and rough surfaces can reduce performance. Maraging steel is not a stainless steel, so it may need protective coating, plating, oiling, painting, or other surface treatment depending on service environment. A polished stainless surface often performs better than a rough machined surface in mild corrosion exposure.

Passivation, Polishing, and Cleaning

For X10CrNi18-8, passivation, polishing, and proper cleaning can improve surface reliability after CNC machining. For maraging steel, finishing is more about protection and functional surface quality. In both materials, abrasive finishing must be controlled so that edges, flatness, and sealing or mating surfaces are not damaged. Surface treatment should be specified early because it can affect dimensions and lead time.

Conclusion

The final choice between X10CrNi18-8 and maraging steel should be based on the real function of the CNC part. X10CrNi18-8 is suitable for stainless spring-like precision parts, clips, brackets, washers, and thin components requiring corrosion resistance and elasticity. Maraging steel is better for compact high-load parts that need ultra-high strength after aging. Both can be CNC machined, but both require careful planning for tool wear, heat, burrs, heat treatment, and final inspection.

FAQ

Is X10CrNi18-8 the same as 304 stainless steel?

No. X10CrNi18-8 is closer to 1.4310 or AISI 301-type stainless steel, while 304 is usually associated with 1.4301. X10CrNi18-8 is stronger in cold-worked conditions and is often used for spring-like parts. 304 is a more general stainless grade with broad availability and easier application in many standard corrosion-resistant components.

Can X10CrNi18-8 be CNC machined accurately?

Yes, it can be CNC machined accurately, but the process must control work hardening, heat, burrs, and tool wear. Sharp tools, correct feed, stable clamping, and good coolant access are important. It is especially useful when precision holes, slots, threads, profiles, or clean edges are required on stainless spring-like parts.

Why not use maraging steel for every high-strength CNC part?

Maraging steel is powerful but expensive and not naturally stainless. It also needs aging heat treatment and careful final inspection. If a part mainly needs corrosion resistance, elasticity, or moderate strength, X10CrNi18-8 or another stainless grade may be more efficient. Maraging steel is best when ultra-high strength justifies the added material and process cost.

Which material is easier to machine?

Maraging steel is often easier to machine before aging than its final strength suggests, while X10CrNi18-8 can be more difficult because of work hardening and burr formation. After aging, however, maraging steel becomes much harder and more demanding. The answer depends on the material condition, geometry, tolerance, and whether finishing is required after heat treatment.

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