Maraging 350 (Equivalent to VASCOMAX® 350, UNS S35000, UNS K93540) Forged Parts | China Leading Forging Manufacturer — Complete Technical Guide

Maraging 350 Forged Parts — VASCOMAX 350 UNS S35000 custom forgings from ISO 9001 certified China manufacturer Jiangsu Liangyi
Quick Definition

Maraging 350 — commonly referenced by the trade name VASCOMAX® 350 (a registered trademark of Carpenter Technology Corporation), UNS designations S35000 / K93540, also called Maraging C-350 — is the highest-strength grade in the commercial maraging steel family. The name "maraging" fuses martensitic and aging, describing the two-stage hardening mechanism: first forming a tough, near-carbon-free martensite matrix on air cooling, then precipitating nanoscale intermetallic compounds (Ni₃Mo, Ni₃Ti, Fe₂Mo) during a 480°C aging cycle. The result is an ultimate tensile strength of 350,000 psi (2,415 MPa) combined with 7% elongation, excellent weldability, and a dimensional change during aging of only 0.04–0.06% — properties that are collectively unattainable in any conventional high-strength steel.

Note: VASCOMAX® is a registered trademark of Carpenter Technology Corporation. Inconel® is a registered trademark of Special Metals Corporation. Jiangsu Liangyi manufactures Maraging 350 (UNS S35000/K93540) forged parts that meet the same material specifications and are not affiliated with or endorsed by these trademark holders.

Jiangsu Liangyi is an ISO 9001:2015 certified China-based leading manufacturer of Maraging 350 (VASCOMAX 350, UNS S35000, UNS K93540, Maraging C-350) open die forgings and seamless rolled rings. With 25+ years of forging experience, an 80,000 m² modern production base, and 6,300-ton hydraulic forging presses, we supply fully custom Maraging 350 forged parts to over 50 countries across North America, Europe, the Middle East, Asia Pacific, and Australia. Every part is produced under complete metallurgical traceability and backed by EN10204 3.1/3.2 mill test certificates.

Founded
1997
25+ years forging expertise
Max Press Force
6,300 T
Hydraulic forging press
Export Markets
50+ Countries
NA, EU, ME, APAC, AU
Quality System
ISO 9001:2015
EN10204 3.1 / 3.2 MTCs

The Metallurgical Science of Maraging 350 — Why It Achieves 350,000 psi

To specify and use Maraging 350 correctly, it is important to understand why this alloy gets its excellent properties — not just memorize the numbers. The following explanation reflects our 25+ years of production experience with this material and is not available from commodity datasheet sources.

Core principle: Maraging 350 achieves ultra-high strength through precipitation of nanoscale intermetallic compounds within a near-carbon-free, ductile martensitic matrix — a mechanism fundamentally different from conventional hardened steels, and responsible for the unique combination of strength, toughness, weldability, and dimensional stability that no other commercially available steel grade can replicate.

What Does "Maraging" Actually Mean?

The term "maraging" is a portmanteau of martensitic and aging, coined in the late 1950s by researchers at the International Nickel Company (INCO) who first developed this alloy family. It describes the two-stage hardening process with precision: the steel first transforms to martensite (upon air cooling from the solution anneal temperature), then is "aged" at a lower temperature to precipitate strengthening compounds within that martensitic matrix.

This is categorically different from conventional high-strength steels such as 4340, where strength comes from carbon-rich carbide precipitation and where hardening requires rapid quenching to trap carbon in a supersaturated lattice. In Maraging 350, carbon is held to ≤0.03% — effectively treating it as an impurity — and the strengthening mechanism is entirely based on intermetallic precipitation.

Stage 1: How the Soft Martensite Forms (No Quenching Required)

When Maraging 350 is heated to 820°C (1508°F) and then air cooled, the austenite transforms to martensite during the slow air cooling cycle. This seems counterintuitive — conventional wisdom holds that martensite requires rapid quenching — but Maraging 350 achieves this because:

Stage 2: Precipitation Hardening — The Intermetallic Mechanism

During age hardening at 480°C (896°F), three main intermetallic compounds are coherently precipitated into the martensite matrix:

Jiangsu Liangyi Process Insight

In our production experience, achieving consistent 350,000 psi tensile strength requires tight furnace temperature control of ±8°C and careful uniformity across the section thickness. For large cross-sections (>300mm), we use extended aging hold times (up to 5–6 hours) to ensure full precipitation at the core. This is not specified in most datasheets but is critical for large forgings in oil & gas and nuclear applications.

The Critical Role of Cobalt — Why Grade 350 Has 12%

The most important distinguishing feature of Maraging 350 versus lower grades is its 12% cobalt content — the highest in the family. Cobalt serves a critical metallurgical function that is often misunderstood: it does not itself form strengthening precipitates. Instead, cobalt reduces the solubility of molybdenum in the martensite matrix. With higher cobalt, more molybdenum is forced out of solution and precipitates as Ni₃Mo during aging, producing a denser precipitate dispersion and therefore higher strength. This is why increasing cobalt from 9% (Grade 300) to 12% (Grade 350) produces a strength jump from 300 ksi to 350 ksi — not because cobalt itself strengthens the steel, but because it amplifies the molybdenum precipitation response.

The Dimensional Stability Advantage — Critical for Precision Components

One of the most practically valuable properties of Maraging 350 is its predictable dimensional change during aging: only 0.04–0.06% linear expansion. This is an order of magnitude smaller and far more consistent than the dimensional distortion caused by quenching in conventional steels. For precision components such as turbine disks, valve stems, or missile guidance components, this means parts can be machined close to final dimensions in the soft annealed condition and then aged with confidence that they will fall within drawing tolerances without further grinding — a significant cost saving in high-precision applications.

Full Range of Maraging 350 Forged Products We Supply

We manufacture custom Maraging 350 (equivalent to VASCOMAX® 350, UNS S35000) forged steel products in full specifications, strictly complying with ASTM, AMS, API, EN, DIN, and JIS international standards, and your custom drawings. Our forging capabilities for Maraging 350 cover the full product spectrum:

Maraging 350 Steel: Chemical Composition, Mechanical & Physical Properties

Standard Chemical Composition of Maraging 350 (UNS S35000 / UNS K93540)

Table 1 — Maraging 350 chemical composition per AMS 6521 / AMS 6522. All values in weight %.
ElementSpecification LimitMetallurgical Role
Carbon (C)≤ 0.03%Kept ultra-low to prevent carbide formation; ensures strengthening relies entirely on intermetallic precipitation, preserving weldability and toughness
Nickel (Ni)18.50%Core matrix element; lowers Ms temperature to ~155°C enabling air-cool martensite transformation; provides ductile martensite matrix with good toughness
Cobalt (Co)12.00%Primary strengthening enabler; reduces Mo solubility in martensite, forcing denser Ni₃Mo precipitation during aging; responsible for Grade 350's superior strength over Grade 300
Molybdenum (Mo)4.80%Forms Ni₃Mo and Fe₂Mo precipitation strengthening phases during aging; improves corrosion resistance; reduces susceptibility to temper embrittlement
Titanium (Ti)1.40%Forms Ni₃Ti precipitates; synergizes with Mo precipitation; suppresses austenite reversion during overaging
Silicon (Si)≤ 0.10%Residual deoxidizer; controlled to minimize impurity inclusions that degrade toughness
Manganese (Mn)≤ 0.10%Residual deoxidizer; controlled to minimize MnS inclusions; improves hot workability during forging
Aluminum (Al)0.10%Deoxidizer; assists in grain refinement during solidification; supports uniform precipitate distribution
Iron (Fe)BalanceBase matrix element

Mechanical Properties After Standard Heat Treatment

Table 2 — Maraging 350 mechanical properties after solution anneal (820°C/1h/AC) + age hardening (480°C/3h/AC). Test direction: longitudinal.
PropertyMinimum ValueTypical ValueUnit
Ultimate Tensile Strength (UTS)350,000 (2,415 MPa)355,000–365,000psi
0.2% Offset Yield Strength340,000 (2,345 MPa)342,000–355,000psi
Elongation (gauge length 50mm)7%8–10%%
Reduction of Area35%40–50%%
Notch Tensile Strength (K=9.0)330,000340,000–350,000psi
Hardness (as-aged)52–56 HRCHRC
Hardness (solution annealed)28–32 HRCHRC
Charpy V-Notch Impact (25°C)15–25 JJ
Fracture Toughness KIC35–50 MPa√mMPa√m

Physical Properties of Maraging 350 Steel

Physical properties are critical for design engineers performing thermal analysis, FEA modeling, and fitment calculations. The following values apply to the aged condition at room temperature (20°C) unless noted:

Table 3 — Maraging 350 physical properties (aged condition, 20°C)
Physical PropertyValueUnit
Density8.00g/cm³ (0.289 lb/in³)
Elastic (Young's) Modulus190GPa (28 × 10⁶ psi)
Shear Modulus73GPa
Poisson's Ratio0.30
Thermal Conductivity25W/m·K
Specific Heat Capacity460J/kg·K
Coefficient of Thermal Expansion (20–100°C)10.0 × 10⁻⁶/°C
Electrical Resistivity0.75μΩ·m
Magnetic PermeabilityFerromagnetic at RT
Melting Range1,413–1,430°C
Dimensional Change During Aging+0.04 to +0.06%Linear, predictable

Inspection Standards We Follow

Maraging Steel Grade Comparison: 200 / 250 / 300 / 350 — Which Grade to Choose?

The four commercial maraging steel grades share the same iron-nickel base and the same two-stage heat treatment process, but differ in cobalt content and the resulting strength-toughness balance. Understanding this comparison is essential for correct grade selection — specifying Grade 350 when Grade 250 would suffice wastes significant material cost, while under-specifying the grade risks premature fatigue failure in service.

Table 4 — Commercial maraging steel grade comparison (aged condition properties). Grade 350 data per AMS 6521/6522; other grades per respective AMS specifications.
PropertyGrade 200Grade 250Grade 300Grade 350 (This Grade)
UNS DesignationK92810K92890K93120S35000 / K93540
Min UTS (ksi / MPa)200 / 1380250 / 1724300 / 2069350 / 2415 ★ Highest
Min Yield Strength (ksi)190240290340 ★ Highest
Min Elongation (%)10877
Fracture Toughness KIC (MPa√m)~150~80–110~55–70 ★ Best balance~35–50
Nickel Content18%18%18%18.50%
Cobalt Content8%7.5%9%12% ★ Highest
Typical Hardness (aged)42–46 HRC47–52 HRC50–54 HRC52–56 HRC
Primary ApplicationsTooling, dies, moderate-strength structuralAerospace structural, general high-strengthRocket motor cases, defense, aerospaceMaximum-strength applications where Grade 300 is insufficient
Relative Material Cost$$$$$$$$$$
Grade Selection Guidance from Our Engineering Team

Grade 350 is the correct choice when your component design is already optimized for Grade 300 and still cannot meet the fatigue life or static strength requirement. If you are selecting a grade for a new design, consider starting with Grade 300 and evaluating whether the higher fracture toughness (KIC ~60 vs ~40 MPa√m) offers a longer fatigue crack propagation life — often more valuable than the additional 50 ksi of tensile strength. We are glad to provide free grade selection consultation for your specific application.

Maraging 350 vs. Competing Ultra-High-Strength Materials

Engineers considering Maraging 350 are often evaluating it against other high-strength materials. The following comparison is based on our production experience and published material data — not marketing claims — to help engineers make technically sound decisions.

Table 5 — Maraging 350 (UNS S35000) vs competing ultra-high-strength materials. Values at room temperature.
CriterionMaraging 350 (UNS S35000)AISI 4340 (Q&T to ~270 ksi)17-4PH Stainless (H900)H13 Tool SteelInconel® 718
Max UTS (ksi)350 ★~270~200~230~185 (RT)
Yield Strength (ksi)340 ★~240~175~210~165
Elongation (%)7%~8% (at 270 ksi)10%~12%12%
WeldabilityExcellent ★
No preheat required
Fair
Preheat 175–230°C required
GoodDifficult
High preheat required
Good
Quench Cracking RiskNone ★
Air cool, no quench
High
Oil/water quench required
LowHigh
Air hardening but sensitive
None
Dimensional Stability (HT)Excellent ★
±0.05% aging change
Poor
Significant distortion
GoodFairGood
Corrosion ResistanceLow
Requires coating/plating
LowExcellent ★
Stainless grade
LowExcellent
High-Temp Strength (>450°C)Poor
Overages above 500°C
PoorModerateGood (up to 600°C)Excellent ★
Rated to 650°C
Machinability (annealed)Excellent ★
28–32 HRC soft state
GoodGoodFairDifficult
Work hardens rapidly
Relative Cost (forged)$$$$$$$$$$$$$$

When to choose Maraging 350 over alternatives: Specify Maraging 350 when your application requires tensile strength >300 ksi that cannot be achieved with any other commercially available steel, combined with: (a) weldability — critical if the forging will be welded into a larger assembly; (b) predictable post-machining dimensional change — critical for precision components machined before aging; (c) operation at ambient to 400°C — if operating continuously above 500°C, Inconel® 718 is superior. The material cost premium is substantial, but for applications where failure is not an option, Maraging 350 offers performance that no lower-cost alternative can match.

Maraging 350 Complete Heat Treatment Protocol — From Our Production Floor

Heat treatment is the most critical step in Maraging 350 production. The following protocol is based on AMS 6521/6522 requirements combined with our process-controlled production experience across thousands of forged components. Deviation from these parameters — even minor furnace temperature non-uniformity — can reduce tensile strength by 10,000–20,000 psi or cause inconsistent properties across the cross-section of large forgings.

Solution Annealing (Homogenization)

Temperature: 820°C ± 14°C (1508°F ± 25°F)
Hold time: Minimum 1 hour per 25 mm of maximum cross-section thickness
Atmosphere: Vacuum, inert gas (argon), or controlled atmosphere to prevent oxidation
Cooling: Air cool to room temperature — do NOT water or oil quench
Result: Homogeneous lath martensite, 28–32 HRC, fully machinable

Purpose: Dissolves all prior precipitates and homogenizes the alloy composition. The air cooling cycle is sufficient to transform austenite to lath martensite (Ms ≈ 155°C) without quench cracking risk. This step establishes the uniform martensite matrix into which precipitates will grow during aging.

Precision Machining Window (Between Stages)

Hardness: 28–32 HRC (similar to AISI 4340 at 30 HRC)
Recommended operations: Rough and semi-finish machining, drilling, tapping, boring, and grinding to near-net dimensions
Allowance for aging: Leave +0.05–0.10% stock on critical diameter dimensions to account for the predictable 0.04–0.06% linear expansion during aging

Purpose: This is the optimal machining window. The soft annealed martensite cuts freely with conventional carbide tooling at high speeds. Doing major machining in this condition — rather than after aging — dramatically reduces cycle time and tooling costs, and avoids the risk of grinding burn on the hard aged surface.

Age Hardening (Precipitation Hardening)

Temperature: 480°C ± 8°C (896°F ± 15°F)
Hold time: 3 hours minimum; 5–6 hours for sections >300 mm to ensure full core precipitation
Atmosphere: Vacuum or inert gas preferred; air permissible if surface oxidation is acceptable
Cooling: Air cool to room temperature
Result: 52–56 HRC, 350,000 psi UTS, 0.04–0.06% linear expansion

Purpose: Ni₃Mo, Ni₃Ti, and Fe₂Mo precipitates nucleate and grow coherently within the martensite matrix. Hardness increases from ~30 HRC to 52–56 HRC over the 3-hour hold. The reaction is largely complete within 3 hours at 480°C; extending to 5 hours adds minimal additional strength (<2%) but ensures full core properties in thick sections.

Finish Grinding / Final Inspection (Post-Aging)

Stock removal: Grinding or hard turning to final drawing dimensions
Surface integrity: Monitor for grinding burn (tempers precipitates and reduces local hardness); use cool grinding parameters and check with temper etch or Barkhausen noise
NDT: Final UT, MT, dimensional inspection, and hardness verification

Purpose: Removes the small dimensional expansion from aging and achieves final drawing tolerances. Because the aging expansion is predictable and repeatable, many precision components require only minor final grinding — often just 0.05–0.15 mm per surface.

⚠ Critical Overaging Warning

Aging above 510°C (950°F) or for excessively long hold times causes overaging: the intermetallic precipitates coarsen and austenite begins to revert within the martensite matrix. Strength drops sharply — typically by 30,000–60,000 psi — and cannot be recovered without a full re-anneal and re-age cycle. In our production we monitor furnace temperatures with calibrated Type-K thermocouples at ±5°C accuracy, and document every heat treatment cycle on the mill test certificate. We do not accept ±15°C tolerance furnaces for Maraging 350 production.

Maraging 350 Forging Process & Grain Flow Advantage

Forging is not merely a shaping operation for Maraging 350 — it is a critical metallurgical process step that determines grain structure, inclusion alignment, and therefore the directional mechanical properties of the final component. The following describes our proprietary forging approach developed over 25 years of Maraging steel production.

Why Forging Outperforms Casting for Maraging 350

Maraging 350 is produced exclusively as wrought (forged or rolled) material — not cast — for critical applications, because:

Our Maraging 350 Forging Process Parameters

Table 6 — Maraging 350 forging process parameters used at Jiangsu Liangyi production facility
Process ParameterSpecificationReason
Forging Temperature Range1,120–1,200°C (2,050–2,190°F)Optimal hot ductility; avoids hot-short cracking above 1,220°C and poor deformability below 1,050°C
Minimum Finish Forging Temperature> 870°C (1,600°F)Prevents cold working of austenite which can produce undesirable fibrous texture
Minimum Total Reduction Ratio4:1 (ingot-to-forging section)Achieves grain refinement to ASTM 5+ and closes solidification porosity
Maximum Single-Hit Reduction≤ 25% per pass (for sections > 300mm)Prevents adiabatic shear band formation in large sections
Reheat CyclesAs required to maintain temperature > 870°CUnlimited reheats permissible without property penalty provided final condition is solution annealed
Press Capacity Used2,000–6,300 ton hydraulic pressHydraulic press preferred over hammer for large Maraging 350 forgings to ensure slow, penetrating deformation to the core
Post-Forge CoolingAir cool or slow cool in sand/ashesPrevents thermal shock; martensite transformation completes during slow cooling — no furnace anneal required before machining if section is uniform

Hydraulic Press vs. Forging Hammer for Large Maraging 350 Sections

For Maraging 350 forgings with cross-sections exceeding 200 mm, we specifically use our 6,300-ton hydraulic press rather than a forging hammer. The reason is fundamental to metallurgy: hydraulic presses apply force slowly (0.1–0.5 m/s ram speed), allowing the deformation force to penetrate to the center of the billet. Hammer blows (5–8 m/s) are fast enough to produce surface deformation while leaving the core relatively unworked — particularly problematic for large-diameter bars and discs where core properties are critical for applications such as turbine disks and drill collar forgings.

Our 6,300-ton hydraulic forging press generates sufficient force to achieve the target reduction ratio in the core of forgings up to 1,500 mm diameter, ensuring homogeneous grain refinement from surface to center — a capability that directly differentiates our large Maraging 350 forgings from those produced on smaller equipment.

Jiangsu Liangyi 6300-ton hydraulic forging press producing Maraging 350 large-section forgings for aerospace and oil & gas applications

Maraging 350 Machining, Welding & Secondary Operations

Maraging 350 is one of the most forgiving ultra-high-strength steels to machine and weld — but only when processed in the correct sequence and condition. The following guidance reflects our in-house CNC machining and post-weld aging experience with this alloy.

Machining Maraging 350

Always machine in the solution-annealed condition (28–32 HRC), not after aging. In the annealed state, Maraging 350 machines comparably to AISI 4340 at 30 HRC — conventional carbide tooling, standard cutting speeds, and normal flood coolant all produce excellent results. After aging (52–56 HRC), machinability drops sharply; cutting speeds must be reduced by 60–70% and carbide tooling wear increases dramatically.

Welding Maraging 350

Maraging 350 offers one of the best weldabilities of any ultra-high-strength steel — a direct consequence of its near-zero carbon content. There is no risk of hydrogen-induced cold cracking (which plagues high-carbon steels) and no need for high preheat temperatures.

Surface Protection

Maraging 350 has limited intrinsic corrosion resistance and will rust in humid environments without surface protection. For most applications, we recommend: cadmium plating (aerospace, AMS 2400), hard chrome plating (valve stems and hydraulic components), electroless nickel plating (oil & gas, API service), or phosphating + painting (general industrial). Specify the required surface treatment on your drawing or RFQ so we can apply it after final inspection before packaging and shipment.

Why Choose Jiangsu Liangyi for Maraging 350 Forged Parts

There are many forging manufacturers in China, but relatively few with the metallurgical experience, equipment capacity, and quality systems required to produce Maraging 350 forgings that meet aerospace, oil & gas, and nuclear standards. Here is what specifically differentiates our Maraging 350 production capability:

1. Full Melting Method Control — AM/VR, VIM/VAR, AM/VAR

Maraging 350 raw material quality starts at the melting stage. We supply all three AMS-recognized melting methods:

We keep records of heat number, melt method, ingot lot, and chemical certificate for 100% traceability from final forging back to the original melt — a requirement we fulfill as standard practice, not as a premium add-on.

2. Strict Heat Treatment Process Control

We run temperature controlled box furnaces and vacuum furnaces with documented ±8°C uniformity, calibrated according to industry standard pyrometry procedures as described in the heat treatment section above. The aging cycles are recorded on computerized chart recorders and attached to the mill test certificate for each part. Such documentation is sufficient for quality-conscious aerospace customers. We supply full heat treatment records with every shipment.

3. Full Machining Capability — No Outsourcing

All machining of Maraging 350 forgings is performed in-house on our CNC turning centers, machining centers, and cylindrical grinders. We do not outsource machining to subcontractors — a common source of quality control gaps. Our machining capability covers: OD turning up to Ø2,500 mm, boring up to Ø3,000 mm depth 5,000 mm, CNC milling 5-axis up to 6,000 mm × 3,000 mm, surface and cylindrical grinding to Ra 0.8 μm or better.

4. Global Export Experience & Localized Compliance

With 25+ years of export experience and clients in over 50 countries, we have deep practical knowledge of international standards and documentation requirements. We know that a North American client needs ASTM E8 test reports with dual psi/MPa units; that a European nuclear client requires RCC-M Appendix ZG traceability; that a Middle East oil & gas client needs NACE MR0175/ISO 15156 compliance documentation with H₂S partial pressure exposure records. These are not items we research when an order arrives — they are embedded in our standard quality procedures.

Quality Control — NDT Methods, Acceptance Criteria & Certification Details

Every Maraging 350 forged part we produce passes through a documented inspection sequence before shipment. The following describes each inspection method, the defects it detects, and the acceptance standards we apply — not as marketing language, but as the technical basis for our quality claims.

Table 7 — NDT and mechanical test sequence for Maraging 350 forged parts at Jiangsu Liangyi
Inspection MethodReference StandardDefects DetectedAcceptance Criteria
Ultrasonic Testing (UT)ASTM A388 / AMS 2154Internal volumetric defects: shrinkage, pipe, cracks, inclusions, hydrogen flakes at depthAMS 2154 Class A or B depending on specification; typical rejection threshold: flat-bottom hole equivalent FBH 1/64″ (0.4mm) for aerospace
Magnetic Particle Testing (MT)ASTM E1444 / AMS 2641Surface and near-surface linear discontinuities: forging laps, seams, cold shuts, grinding cracksNo linear indications; rounded indications <1/16″ (1.6mm) acceptable per ASTM E1444
Liquid Penetrant Testing (PT)ASTM E165 / AMS 2647Open surface defects on non-magnetic surfaces or after machining: porosity, cracking, EDM cracksType I (fluorescent) Method A; no relevant linear indications; rounded indications per AMS 2647 class
Tensile TestingASTM E8 / E8MConfirmation of UTS, yield strength, elongation, and reduction of area meeting specification minimumsPer AMS 6521: UTS ≥350,000 psi, YS ≥340,000 psi, Elong ≥7%, RA ≥35%
Hardness TestingASTM E10 (Brinell) / ASTM E18 (Rockwell)Verification of aging completion and uniformity across the cross-section52–56 HRC across all test locations; variation <2 HRC from surface to core (coupon sectioning)
Charpy Impact (V-Notch)ASTM E23Verification of toughness; detection of overaging, underaging, or inclusion-induced embrittlementPer customer specification; typical minimum: 15 J at 25°C for most applications
Chemical AnalysisASTM E354 / OES spectrometerVerification that all 9 alloying elements meet composition specificationPer AMS 6521 composition limits; heat and product analysis both performed
Dimensional InspectionDrawing requirements / CMMAll critical dimensions verified against drawing tolerances100% dimensional inspection on CNC-machined surfaces; final report with actual values

Our Factory Certification & Available Documentation

Transparency Notice

Our factory holds ISO 9001:2015 certification — this is our quality management system certification. The following documents are inspection records and test certificates we can provide per order, not separate body certifications.

Industry-Specific Applications & GEO-Targeted Project Cases

Our Maraging 350 (equivalent to VASCOMAX® 350, UNS S35000) forged parts are selected for applications where failure has severe consequences and where no lower-strength alternative can meet the design requirement. The following describes our core application industries with specific component types and regional project examples.

Aerospace & Defense Industry

Engineering Challenge: Aerospace structures demand the highest possible strength-to-weight ratio. Every kilogram of excess structural mass reduces payload capacity. At the same time, fracture mechanics calculations require a minimum fracture toughness (KIC) to ensure that any undetected crack below the inspection resolution limit will not propagate to failure during a single flight cycle.

Why Maraging 350: For components where Grade 300 (300 ksi) provides insufficient fatigue life or where weight savings from the additional 50 ksi allow a smaller cross-section that KIC analysis confirms is still safe, Maraging 350 is the correct selection. The lack of quench cracking risk and excellent weldability allow complex assemblies to be fabricated without the stress-corrosion cracking concern present in other ultra-high-strength steels.

Specific Components We Produce: Missile and rocket motor cases (cylindrical seamless rings, rolled and seam-welded); aircraft landing gear actuator housings and side struts; high-performance drive shafts and gear shafts for propulsion systems; precision fasteners and stud bolts for critical structural joints complying with NAS/MS aerospace hardware standards.

GEO Capability & Compliance: Our AMS 6521 VIM/VAR Maraging 350 seamless rings and discs are produced to meet aerospace prime contractor quality requirements, with documentation suitable for customer source inspection programs. Regional standards supported: AMS 6521, AMS 6522.

Oil & Gas Industry

Engineering Challenge: Downhole components in deep wells operate under combined loads: hydrostatic pressure (up to 1,400 bar), torsional load (drill strings), bending fatigue (caused by wellbore curvature in directional drilling), and aggressive chemical environments including H₂S, CO₂, and chlorides. A single component failure in a deep wellbore can cost millions in workover operations.

Why Maraging 350: For mud motor drive shafts and ESP motor shafts, the combination of ultra-high fatigue strength (high UTS/yield ratio) and excellent machinability for precision splined profiles makes Maraging 350 the preferred material. Its NACE MR0175/ISO 15156 qualification for controlled hardness H₂S environments (when used below Rockwell C 40 maximum in sour service — verify specific application requirements) makes it suitable for wellhead and valve applications.

Specific Components We Produce: Mud motor (positive displacement motor, PDM) splined drive shafts and universal joints; electric submersible pump (ESP) splined motor shafts up to 6 meters length; high-pressure valve balls, bodies, and stems for wellhead equipment per API 6A; double studded adapter flanges (DSAF) for Christmas tree connections; casing head housings and tubing head spools.

GEO Project Experience: Our Maraging 350 ESP motor shafts (Method C, AM/VAR) meet the specifications required by Middle East oilfield service operations in Saudi Arabia, UAE, and Iraq. VIM/VAR Method B is available for North American shale gas drill motor component requirements. Compliance: API 6A, NACE MR0175/ISO 15156, API 11D1.

Nuclear Power Industry

Engineering Challenge: Nuclear components should maintain mechanical properties under long term irradiation (neutron fluence), thermal cycling and coolant chemistry (boric acid, lithium hydroxide) at temperatures up to 325°C (PWR primary circuit). Material traceability and quality documentation shall meet the regulatory requirements of the national nuclear safety authorities.

Why Maraging 350: For reactor coolant pump (RCP) components where the combination of high strength, excellent fatigue resistance, and the ability to produce large-diameter seamless ring forgings with consistent properties is required. The lack of carbon-carbide structures deletes concerns about sensitization and intergranular corrosion in the coolant environment.

Specific Components We Produce: RCP rotor impellers (large-diameter seamless rings up to Ø2,500 mm); pump casing shells; containment liner seal chambers; pressure vessel reactor nozzle forgings; coolant pump shaft forgings.

GEO Project Experience: Our Maraging C-350 forged components are produced with EN10204 3.2 documentation packages designed to support customers' compliance with applicable nuclear codes including ASME BPVC Section III and RCC-M — subject to the customer's own regulatory qualifications and authority approvals. We do not hold independent nuclear facility approvals (HAF102, N-stamp); these remain the customer's responsibility.

Power Generation & Turbomachinery Industry

Engineering Challenge: Gas and steam turbine rotor components rotate at 3,000–3,600 RPM continuously under combined centrifugal, thermal, and pressure loads. High-cycle fatigue (HCF) life — typically >10⁸ cycles over the turbine's 30-year design life — determines the critical section sizing, not static strength alone. Materials must also maintain properties during start-stop thermal cycling without dimensional creep.

Why Maraging 350: The high yield-to-UTS ratio (340/350 = 0.971) of Maraging 350 — higher than any other commercially available steel — is particularly valuable for rotating components, where high yield strength minimizes plastic deformation under centrifugal load and the near-unity ratio means there is minimal "creep" from the nominal working stress to yield. The predictable dimensional stability during aging also allows turbine disk bores to be machined before aging with confidence.

Specific Components We Produce: Gas turbine disks (up to Ø1,800 mm); steam turbine disks and wheels; centrifugal compressor impellers and blisks; valve spindles, main steam valve seats and cores; reheat valve discs; labyrinth shaft seals and guide rings for industrial gas compressors.

GEO Project Experience: Our Maraging 350 labyrinth shaft seal rings and gas turbine compressor disk forgings are produced to meet specifications required by LNG plant gas compressor and turbine applications in Asia, Europe, and Australia. Compliance: EN 10222-4, ASME SA-288, API 617.

Industrial Valve & Flow Control Industry

Engineering Challenge: In high pressure, high temperature or cryogenic service, industrial valves require components for which dimensional stability over millions of operating cycles, resistance to galling on sealing surfaces and high fatigue strength for valve stems with repeated operating torque are important requirements.

Why Maraging 350: The excellent hardness (52–56 HRC aged) provides outstanding galling resistance on sealing surfaces without requiring separate hard-facing. The high strength allows valve stems and shafts to be designed with smaller cross-sections than lower-strength alloys, reducing actuator torque requirements and overall valve weight. The predictable aging behavior allows valve stems to be machined with threaded and profiled sections in the annealed state and aged after machining with minimal dimensional correction.

Specific Components We Produce: Cryogenic high-performance butterfly valve shafts (LNG service, operating at −196°C liquid nitrogen temperature); gate valve bodies and bonnets for ANSI 2500 class pressure service; ball valve balls and seats for high-differential pressure applications; check valve seat rings; ultrasonic flow meter body forgings; H-type two-way valve bodies.

GEO Project Experience: Our Maraging 350 cryogenic butterfly valve shafts and ANSI 2500 gate valve body forgings are produced to API 6D and ASME B16.34 specifications for LNG terminal and natural gas pipeline applications in Europe, North America, and globally. Compliance: API 6D, BS EN 10222-4, ASME B16.34.

Procurement Guide: How to Order Maraging 350 Forgings Correctly

Based on our 25+ years of working with global procurement teams and engineers, the following guide covers the critical information required for an accurate quotation and the most common specification mistakes that cause delays, cost overruns, or quality failures. This is original guidance that we have developed from real procurement experience — not copied from general sourcing articles.

What to Include in Your RFQ (Request for Quotation)

⚠ 5 Common Specification Mistakes — and How to Avoid Them

1. Not specifying the melting method: Results in getting AM/VR (lowest cost, lowest cleanliness) when VIM/VAR is wanted. Fix: Always state Method A, B, or C according to AMS 6521, Section 6.1.

2. Specifying aged condition for a part that will be welded: Welding an aged Maraging 350 part creates a HAZ that is locally overaged and permanently weakened. Fix: always weld in the annealed condition and age the assembly post-welding.

3. Not specifying reduction ratio for important forging applications: A forging made with only 2:1 reduction may meet all chemical and tensile requirements but will have a larger grain size and lower fatigue life than a 4:1 reduction forging. Fix: put “minimum 4:1 reduction ratio” in your forging specs, especially for aerospace and rotating equipment

4. Ordering aged forgings for in-house finish machining: Machining aged Maraging 350 at 52–56 HRC requires slow speeds and expensive CBN tooling. Fix: order forgings in the annealed state, machine to near-final dimensions, then age at your facility — or let us do the complete sequence.

5. Assuming NACE MR0175 compliance automatically: Maraging 350 is listed in NACE MR0175/ISO 15156 for sour service, but only below specific hardness limits for the intended application environment. Review Table B.3 of ISO 15156-3 with your corrosion engineer before specifying for H₂S service.

Standard Lead Times

Table 8 — Typical lead times for Maraging 350 forging orders at Jiangsu Liangyi. Subject to material availability and production schedule.
Order TypeTypical Lead TimeNotes
Standard forgings, Method A (AM/VR), in stock15–20 working daysForging + HT + UT/MT + MTC
Standard forgings, Method B (VIM/VAR), from stock ingot20–28 working daysSame as above; VIM/VAR ingot typically in stock
Large section forgings (>500mm diameter or >5 tons)28–40 working daysExtended aging hold time required for core properties
Fully machined to drawing (annealed + machined)Add 10–20 working days to forging lead timeDepends on machining complexity
Fully machined + aged + finish groundAdd 15–28 working days to forging lead timeFull turnkey production
Third-party inspection (BV/SGS/TÜV witness)Add 3–7 working days for inspector schedulingWe coordinate inspector visit
Expedited production (urgent)Contact us — case by casePossible subject to production schedule

GEO-Targeted Market Compliance & Regional Solutions

As a global Maraging 350 forging supplier, we provide documentation and compliance packages specifically tailored to each export market's regulatory and purchasing requirements:

North America Market (USA, Canada, Mexico)

Our Maraging 350 forged parts fully meet ASTM, AMS, API standards. Mill test certificates include dual psi/MPa units as standard. We support third-party inspection by SGS, BV, and other AISC/A2LA-accredited institutions. For US aerospace applications, we can supply VIM/VAR material with full ingot-to-forging traceability documentation. For applications subject to ITAR or EAR controls, customers should verify applicability with their own export control counsel.

Europe Market (EU, UK, Germany, France)

Our products comply with EN 10222-4, EN 10269, ISO standards and carry CE compliance documentation where applicable. EN10204 3.2 (third-party witness countersignature by Bureau Veritas or TÜV, arranged on customer request) is available for European nuclear and petrochemical projects. We have deep understanding of European market requirements including PED (Pressure Equipment Directive) and ATEX, and our products are produced to EN standards suitable for European aerospace, petrochemical, and power generation applications.

Middle East Market (Saudi Arabia, UAE, Iraq, Kuwait)

We provide oil & gas special Maraging 350 forgings to API 6A (Wellhead & Christmas Tree Equipment), API 6D (Valves) and NACE MR0175/ISO 15156 for sour service applications. Our documentation packages designed for the Saudi Aramco, ADNOC and Iraqi SOC vendor qualification requirements include NACE compliance declarations and certificates of material hardness tests.

Asia Pacific Market (Japan, South Korea, Singapore, Australia)

We provide custom Maraging 350 forging solutions for mining, power generation, and oil & gas industries across Asia Pacific, and all parts meet JIS G 3214, AS 1548, and project-specific standards. Our forging capabilities and documentation standards are well-suited for Australian LNG plant gas compressor components, Southeast Asian power plant turbomachinery, and Korean shipbuilding projects requiring ABS, DNV-GL, or LR class society inspection.

Frequently Asked Questions (15 FAQs) — Maraging 350 Forged Parts

What is Maraging 350 steel and why is it called "maraging"?

The name "maraging" combines martensitic and aging, describing the two-stage hardening mechanism: the steel first transforms to a soft, ductile lath martensite on air cooling (because its martensite start temperature Ms ≈ 155°C is well above room temperature), and is then "aged" at 480°C to precipitate intermetallic strengthening compounds (Ni₃Mo, Ni₃Ti, Fe₂Mo) within that martensite matrix. The result is 350,000 psi tensile strength with 7% elongation — a combination impossible with any conventional high-carbon steel. The term was coined at the International Nickel Company (INCO) in the late 1950s.

What is the difference between Maraging 350, 300, 250, and 200?

The four grades differ primarily in cobalt content and resulting strength. Cobalt reduces the solubility of molybdenum in the martensite matrix, forcing more Mo to precipitate as Ni₃Mo during aging — producing higher strength. Grade 200 (8% Co, 200 ksi UTS) is used for tooling and moderate-strength structural applications; Grade 250 (7.5% Co, 250 ksi) is the most widely used aerospace structural grade; Grade 300 (9% Co, 300 ksi) is used for rocket motor cases and high-performance defense components; Grade 350 (12% Co, 350 ksi) delivers the maximum strength at the trade-off of reduced fracture toughness (KIC ~40 vs. ~60 MPa√m for Grade 300). We supply all four grades and can recommend the correct grade for your specific application and loading conditions.

What is the chemical composition of Maraging 350?

Standard chemical composition of Maraging 350 (UNS S35000, AMS 6521/6522): Carbon max 0.03%, Silicon max 0.10%, Manganese max 0.10%, Nickel 18.50%, Cobalt 12.00%, Molybdenum 4.80%, Titanium 1.40%, Aluminum 0.10%, Iron balance. The ultra-low carbon (≤0.03%) is important as it prevents the formation of carbides meaning all strengthening is from intermetallic precipitation, retaining weldability and toughness that would be lost due to carbide embrittlement at these strength levels.

What are the mechanical properties of Maraging 350 after heat treatment?

After standard heat treatment (solution anneal 820°C/1h/air cool + age 480°C/3h/air cool) per AMS 6521: Ultimate Tensile Strength ≥350,000 psi (2,415 MPa), 0.2% Yield Strength ≥340,000 psi (2,345 MPa), Elongation ≥7% (in 50mm gauge length), Reduction of Area ≥35%, Notch Tensile Strength (K=9.0) ≥330,000 psi. Hardness: 52–56 HRC. In the annealed (pre-aged) condition, hardness is 28–32 HRC — this is the optimal state for machining. Dimensional change during aging: +0.04 to +0.06% linear expansion, predictable and repeatable.

What is the correct heat treatment procedure for Maraging 350?

Two-stage process: Stage 1 — Solution Anneal: 820°C ± 14°C, hold 1 hour minimum per 25mm cross-section, air cool to room temperature. Produces soft lath martensite at 28–32 HRC. Stage 2 — Age Hardening: 480°C ± 8°C, hold 3 hours minimum (5–6 hours for sections >300mm), air cool. Precipitates Ni₃Mo, Ni₃Ti, Fe₂Mo intermetallics, raising strength to 350,000 psi. Critical warning: aging above 510°C causes overaging (austenite reversion, strength loss of 30,000–60,000 psi) that cannot be recovered without a full re-anneal and re-age. Furnace temperature accuracy of ±8°C is required — ±15°C furnaces are not acceptable for this alloy.

What are the physical properties of Maraging 350?

Key physical properties of Maraging 350 (aged, 20°C): Density 8.00 g/cm³ (0.289 lb/in³); Elastic Modulus 190 GPa (28×10⁶ psi); Shear Modulus 73 GPa; Poisson's Ratio 0.30; Thermal Conductivity 25 W/m·K; Coefficient of Thermal Expansion 10.0×10⁻⁶/°C (20–100°C); Electrical Resistivity 0.75 μΩ·m; Melting range 1,413–1,430°C. The material is ferromagnetic at room temperature. These values are needed for FEA analysis, thermal modeling, and interference fit calculations.

How does Maraging 350 compare to AISI 4340 and 17-4PH stainless?

vs. AISI 4340 (quench & tempered to maximum strength ~270 ksi): Maraging 350 provides 30% higher tensile strength, eliminates quench cracking risk (air cool vs. oil quench), offers superior weldability (no preheat), and provides dramatically better dimensional stability during heat treatment. 4340 is lower cost and sufficient for applications with <270 ksi requirement. vs. 17-4PH stainless (H900 condition, ~200 ksi): 17-4PH offers far superior corrosion resistance (stainless grade) but only 57% of Maraging 350's tensile strength. For applications requiring both ultra-high strength and corrosion resistance, a surface coating on Maraging 350 is the practical solution. Maraging 350 vs. Inconel® 718: Maraging 350 has higher room-temperature strength but Inconel® 718 is the correct choice for continuous service above 450°C.

What are the main applications of Maraging 350 forged parts?

Maraging 350 is used where no other steel meets the strength requirement: Aerospace — missile/rocket motor cases, aircraft landing gear, high-performance drive shafts, precision fasteners for critical structural joints; Oil & Gas — mud motor (PDM) splined drive shafts, ESP motor shafts, high-pressure wellhead valve components, double studded adapter flanges (DSAF); Nuclear Power — reactor coolant pump (RCP) rotor impellers, casing shells, pressure vessel nozzles; Turbomachinery — gas turbine disks, steam turbine disks, compressor impellers, blisks, labyrinth shaft seals; Industrial Valves — cryogenic butterfly valve shafts (LNG service), ANSI 2500 class gate valve bodies.

What raw material melting methods do you offer for Maraging 350?

We supply all three AMS 6521-recognized melting methods: Method A — Air Melt / Vacuum Refined (AM/VR): for industrial, valve, and power generation applications where aerospace-grade cleanliness is not required; lower cost. Method B — Vacuum Induction Melted / Vacuum Arc Remelted (VIM/VAR): mandatory for aerospace and missile applications per AMS 6521; removes dissolved gases, volatile impurities, and produces refined inclusion ratings; highest cleanliness and fatigue performance. Method C — Air Melt / Vacuum Arc Remelted (AM/VAR): intermediate cleanliness and cost; widely used for oil & gas downhole tools, high-performance valves, and nuclear components. Please specify the required method on your RFQ to ensure correct quotation.

Is Maraging 350 suitable for H₂S sour service (NACE MR0175)?

Maraging 350 is listed in NACE MR0175/ISO 15156-3 for use in sour (H₂S-containing) oil & gas environments, subject to hardness requirements specified in Table B.3 of ISO 15156-3. The maximum permissible hardness limit depends on the specific H₂S partial pressure and application class — typically ≤36 HRC for most downhole applications, which corresponds to the solution-annealed (unaged) condition of Maraging 350. The fully aged condition (52–56 HRC) generally exceeds NACE MR0175 limits for sour service. Verify the applicable hardness limit with your corrosion engineer and the specific H₂S exposure conditions before specifying for sour service. We can provide NACE-compliant documentation for the annealed delivery condition.

Can you provide custom Maraging 350 forgings according to drawings?

Yes. We provide complete custom Maraging 350 forging solutions from VIM/VAR ingot through to precision CNC-machined and fully inspected components, strictly complying with customer drawings, technical requirements, and all applicable international standards (ASTM, AMS, API, EN, DIN, JIS, ASME). Capabilities: single-piece weight 30 kg–30 tons, maximum shaft length 15 meters, maximum ring diameter 6 meters, maximum disc/disk diameter 3,000 mm. We support all melting methods, all delivery conditions (annealed, aged, machined), and all levels of documentation from EN10204 3.1 to full third-party 3.2 certification with source inspection.

What quality control and certifications do you provide?

All Maraging 350 forgings undergo: 100% Ultrasonic Testing per ASTM A388/AMS 2154; Magnetic Particle Inspection per ASTM E1444; Liquid Penetrant Testing per ASTM E165; Tensile testing per ASTM E8/E8M (UTS, YS, elongation, RA); Charpy V-notch impact per ASTM E23 (when specified); Hardness testing per ASTM E10/E18; Chemical analysis per ASTM E354; 100% dimensional inspection per CMM for machined parts. Documentation: EN10204 3.1 Mill Test Certificate as standard; EN10204 3.2 with BV/SGS/TÜV countersignature available on request. Factory ISO 9001:2015 certified. Full heat and lot traceability provided as standard.

What is the machinability of Maraging 350?

In the solution-annealed condition (28–32 HRC), Maraging 350 machines comparably to AISI 4340 at 30 HRC — one of the best machinabilities among ultra-high-strength steels. Use TiAlN-coated carbide inserts; cutting speed 80–120 m/min for turning; standard flood coolant. Always perform major machining before aging. After aging (52–56 HRC), machinability drops sharply — cutting speeds must be reduced by 60–70% and CBN tooling is recommended for finish operations. The dimensional change during aging (+0.04–0.06% linear) is predictable: leave 0.05–0.10% stock on critical diameter dimensions when machining before aging, and you will achieve final drawing tolerances after a light grinding pass.

What is the delivery time and what affects it?

Standard lead times: AM/VR forgings from stock ingot: 15–20 working days; VIM/VAR (Method B) forgings: 20–28 working days; large sections (>500mm or >5 tons): 28–40 working days due to extended aging hold times; fully machined + aged + finish ground: add 15–28 days to forging lead time; third-party inspection adds 3–7 days for inspector scheduling. Key factors affecting delivery: section size (large sections require longer aging), melting method (VIM/VAR ingot availability), certification requirements (3.2 inspection requires third-party witness scheduling), and production schedule at time of order. Expedited production is possible — contact us with your deadline and we will advise feasibility.

Do you export to all countries? What compliance documentation do you provide by region?

We export Maraging 350 forged parts to 50+ countries with region-specific compliance: North America (USA, Canada, Mexico) — ASTM/AMS/API compliance, dual psi/MPa test reports, SGS/BV/TÜV inspection support; Europe (EU, UK, Germany, France) — EN/DIN/ISO compliance, EN10204 3.2 with BV or TÜV countersignature, PED compliance documentation; Middle East (Saudi Arabia, UAE, Iraq, Kuwait) — API 6A, API 6D, NACE MR0175/ISO 15156 compliance, documentation structured for Saudi Aramco and ADNOC vendor requirements; Asia Pacific (Japan, South Korea, Singapore, Australia) — JIS G 3214, AS 1548, ABS/DNV-GL/LR class society inspection support; China domestic — GB/T standards available. For US aerospace applications subject to ITAR, please contact us to discuss material origin and export control compliance.

Contact China's Leading Maraging 350 Forging Manufacturer

Jiangsu Liangyi Co., Limited has been a trusted supplier of Maraging 350 (UNS S35000, UNS K93540, Maraging C-350) forged parts to aerospace, oil & gas, nuclear power, turbomachinery, and industrial valve industries worldwide since 1997. Our technical team — with 25+ years of Maraging steel forging and heat treatment expertise — is ready to review your drawings, answer specification questions, and provide a detailed technical and commercial proposal within 24 hours.

Inquiry Email: sales@jnmtforgedparts.com

Phone / WhatsApp: +86-13585067993

Official Website: https://www.jnmtforgedparts.com

Factory Address: Chengchang Industry Park, Jiangyin City, Jiangsu Province, China

Working Hours: Monday–Friday 08:00–18:00 CST; Saturday 08:00–12:00 CST

To obtain the fastest and most accurate quotation, please send your inquiry with: (1) a dimensioned part drawing (PDF or DWG); (2) specified material standard (AMS 6521/6522, ASTM, or equivalent); (3) required melting method (AM/VR, VIM/VAR, or AM/VAR); (4) delivery condition (annealed or aged, with or without machining); (5) required certifications (EN10204 3.1 or 3.2); and (6) required quantity and target delivery date. Our technical team will respond with a full technical confirmation and commercial proposal within 24 hours.