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Maraging Steel Ingot: Advanced Manufacturing Processes, Microstructural Control, And Performance Optimization For High-Strength Applications

MAY 15, 202657 MINS READ

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Maraging steel ingot represents a critical intermediate product in the production chain of ultra-high-strength maraging steels, which are precipitation-hardened martensitic alloys widely employed in aerospace, tooling, and advanced manufacturing sectors. The ingot production process—primarily via vacuum arc remelting (VAR) and vacuum induction melting (VIM)—directly determines the size, distribution, and chemistry of non-metallic inclusions, thereby governing fatigue strength, toughness, and dimensional consistency in downstream components. This article examines state-of-the-art ingot manufacturing techniques, inclusion refinement strategies, compositional control, and thermomechanical processing routes that enable maraging steel ingots to meet stringent performance criteria for mission-critical applications.
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Compositional Design And Alloy Chemistry Of Maraging Steel Ingot

Maraging steel ingots are typically formulated with nickel (Ni) contents ranging from 7.0 to 22.0 wt%, cobalt (Co) from 5.0 to 25.0 wt%, molybdenum (Mo) from 0.1 to 17.0 wt%, and titanium (Ti) from 0.2 to 4.5 wt%, with the balance being iron and unavoidable impurities 1,6,8,9,11. Recent high-performance formulations specify Co contents of 12–17 wt%, Mo of 6–8 wt%, and Ti of 0.4–1.5 wt% to achieve both high strength (≥250 kg/mm²) and high plasticity 1. Aluminum (Al) is often limited to ≤0.3 wt% to control oxide inclusion formation, while carbon (C) is kept below 0.01–0.02 wt% to maintain a predominantly martensitic microstructure free from carbide embrittlement 6,9,11.

Nitrogen (N) and oxygen (O) are critical interstitial impurities that must be tightly controlled: target levels are <10 ppm O and <15 ppm N to minimize the formation of coarse nitride (TiN, TiCN) and oxide (Al₂O₃, spinel) inclusions that act as fatigue crack initiation sites 6,10,13. Controlled nitrogen introduction during vacuum melting—typically 0.0025–0.0050 mass% N—has been shown to promote uniform dispersion of fine Ti-based nitride inclusions (≤15 µm maximum length), thereby reducing variability in fatigue test results and mitigating size effects in large-diameter ingots (≥650 mm) 3,7. Magnesium (Mg) addition at 5–20 ppm in the consumable electrode serves as a nucleation agent for MgO, which subsequently dissociates under high vacuum to refine oxide inclusions and suppress the influence of coarse alumina particles 6,10,13.

Key compositional targets for advanced maraging steel ingots include:

  • Ni: 15–18 wt% for austenite stabilization and precipitation hardening 1
  • Co: 12–17 wt% to enhance intermetallic precipitate coherency 1
  • Mo: 6–8 wt% for solid-solution strengthening and precipitate refinement 1
  • Ti: 0.4–1.5 wt% (or 0.2–3.0 wt% in fatigue-critical grades) for Ni₃Ti precipitation 1,3,7
  • Al: ≤0.3 wt% to limit oxide formation 1
  • C: <0.01 wt% to avoid carbide networks 6,11
  • N: 0.0025–0.0050 wt% (controlled addition) for nitride dispersion 3,7
  • O: <10 ppm to minimize oxide inclusions 6,10
  • Mg: 5–20 ppm (in electrode) for inclusion refinement 10,13

These compositional windows are optimized through iterative vacuum melting trials and statistical analysis of inclusion populations, ensuring that the ingot microstructure supports subsequent solution treatment, aging, and thermomechanical processing without premature fatigue failure or ductility loss.

Primary Melting And Consumable Electrode Production For Maraging Steel Ingot

The production of maraging steel ingot begins with primary vacuum melting, typically conducted in a vacuum induction furnace (VIF) or vacuum arc furnace (VAF) under a controlled atmosphere to minimize gas pickup and oxidation 5,6,13. Raw materials—including virgin alloys, high-purity scrap, and master alloys—are melted at temperatures exceeding 1,600°C to achieve complete dissolution of alloying elements and homogenization of the melt 5. During this stage, Mg is introduced as a Ni–Mg alloy (0–20 mass% Mg) to form MgO nuclei, which serve as heterogeneous nucleation sites for subsequent nitride precipitation and facilitate oxide refinement during remelting 6,10,13.

A critical process parameter in primary melting is the leak rate, which governs the partial pressure of reactive gases (O₂, N₂, H₂O) in the furnace atmosphere. For maraging steel, a leak rate of ≥3 Pa/min (and preferably 3–20 Pa/min) during primary melting ensures sufficient oxygen activity to stabilize MgO formation without excessive oxidation of Ti and Al 13. This controlled leak rate, combined with vacuum levels of 10⁻²–10⁻³ Pa, enables the formation of fine, uniformly distributed MgO particles (≤20 µm) that act as nucleation substrates for TiN and TiCN during solidification 13.

Following primary melting, the molten steel is cast into consumable electrodes (also termed remelting electrodes) with diameters ranging from 300 to 800 mm, depending on the target ingot size 2,3,4,7,13. These electrodes are designed to retain residual MgO and controlled levels of Ti and N (0.2–3.0 mass% Ti, 0.0025–0.0050 mass% N) to ensure optimal inclusion refinement during the subsequent vacuum arc remelting (VAR) step 3,7,13. Electrode chemistry is verified via optical emission spectroscopy (OES) and combustion analysis (for C, N, O, S) to confirm compliance with target specifications before remelting.

Key process steps in consumable electrode production include:

  1. Charge preparation: Blending of virgin alloys, high-purity scrap, and master alloys to achieve target composition 5
  2. Vacuum induction melting: Melting at 1,600–1,700°C under 10⁻²–10⁻³ Pa vacuum with controlled leak rate (≥3 Pa/min) 13
  3. Mg addition: Introduction of Ni–Mg alloy (5–20 ppm Mg) to form MgO nuclei 6,10,13
  4. Casting: Pouring into water-cooled copper molds to form cylindrical electrodes 2,4
  5. Compositional verification: OES and combustion analysis to confirm Ti, N, O, Mg levels 3,7,13
  6. Surface conditioning: Removal of surface defects and oxide scale via machining or grinding 2

The resulting consumable electrode exhibits a fine-grained, equiaxed microstructure with uniformly dispersed MgO particles and minimal macrosegregation, providing an ideal feedstock for VAR processing.

Vacuum Arc Remelting (VAR) Process And Ingot Solidification Control

Vacuum arc remelting (VAR) is the cornerstone technology for producing high-integrity maraging steel ingots with refined inclusion populations and minimal compositional segregation 2,3,4,7,13. In the VAR process, the consumable electrode is suspended above a water-cooled copper crucible and melted by a direct-current (DC) arc struck between the electrode tip and the molten pool surface. Droplets of molten metal detach from the electrode, traverse the arc plasma, and solidify progressively in the crucible to form a cylindrical ingot with diameters typically ranging from 300 to 1,200 mm 2,3,4,7.

A critical innovation in maraging steel VAR is the introduction of rare gas (helium or argon) cooling between the ingot surface and the crucible wall to control the depth of the molten pool and suppress macrosegregation 2,4. Helium gas is introduced at a pressure of 0.9–1.9 kPa (preferably 0.9–1.5 kPa) to enhance heat extraction from the solidifying ingot, thereby reducing the molten pool depth to ≤170 mm 4. This shallow pool geometry minimizes the residence time of inclusions in the liquid phase, promoting their floatation to the top surface (which is subsequently cropped) and reducing the size and number density of residual inclusions in the final ingot 2,4.

The VAR process also facilitates thermal decomposition and dissociation of MgO formed during primary melting. Under the high vacuum (10⁻²–10⁻³ Pa) and elevated temperatures (>1,600°C) of the molten pool, Mg evaporates from the melt surface, causing MgO particles to dissociate and release oxygen, which is then removed by the vacuum system 6,10,13. This mechanism significantly reduces the total oxygen content in the ingot (to <10 ppm) and refines the size distribution of oxide inclusions, with spinel-form inclusions (MgAl₂O₄) exhibiting maximum lengths of ≤20 µm and a content rate exceeding 33% relative to alumina inclusions 10.

Key VAR process parameters for maraging steel ingot production include:

  • Arc current: 3,000–8,000 A (depending on ingot diameter) to maintain stable arc and controlled melt rate 2,4
  • Arc voltage: 25–35 V to balance energy input and electrode melting rate 2,4
  • Melt rate: 2–5 kg/min to ensure adequate superheat and inclusion floatation 2,4
  • Vacuum level: 10⁻²–10⁻³ Pa to promote Mg evaporation and oxygen removal 6,10,13
  • Helium pressure: 0.9–1.9 kPa (preferably 0.9–1.5 kPa) for pool depth control 2,4
  • Molten pool depth: ≤170 mm to minimize segregation and inclusion entrapment 4
  • Cooling rate: 10–50°C/min (controlled by helium flow and water cooling) to refine solidification microstructure 2,4

The resulting VAR ingot exhibits a columnar-to-equiaxed transition (CET) microstructure with fine prior austenite grain sizes (50–200 µm), uniform distribution of Ti-based nitride inclusions (TiN, TiCN) with maximum lengths of ≤15 µm, and oxide inclusions (spinel, alumina) with maximum lengths of ≤20 µm 10,13. This refined inclusion population is critical for achieving high fatigue strength (≥1,800 MPa ultimate tensile strength with >10⁶ cycle fatigue life) and minimizing variability in mechanical properties across large-diameter ingots (≥650 mm) 3,7.

Inclusion Refinement Strategies And Non-Metallic Inclusion Control In Maraging Steel Ingot

Non-metallic inclusions—particularly nitrides (TiN, TiCN) and oxides (Al₂O₃, MgAl₂O₄, MgO)—are the primary microstructural features governing fatigue crack initiation and propagation in maraging steels 2,3,7,10,13. Coarse inclusions (>20 µm) act as stress concentrators and reduce fatigue strength by up to 30%, while fine, uniformly dispersed inclusions (<15 µm) have minimal impact on fatigue life and may even enhance crack deflection and toughness 3,7,10.

State-of-the-art inclusion refinement strategies for maraging steel ingot production include:

Controlled Nitrogen Addition During Primary Melting

Introducing nitrogen at 0.0025–0.0050 mass% during vacuum induction melting promotes the formation of fine, uniformly dispersed Ti-based nitride inclusions (TiN, TiCN) with maximum lengths of ≤15 µm 3,7. This controlled nitrogen addition exploits the high affinity of Ti for N to nucleate nitrides on pre-existing MgO particles, resulting in a bimodal inclusion population with fine nitrides (5–15 µm) and refined oxides (10–20 µm) 7,13. Fatigue testing of maraging steel produced with controlled nitrogen addition shows a 20–25% reduction in variability of fatigue test results and a 15–20% increase in mean fatigue strength compared to conventional nitrogen-free melting 3,7.

Magnesium Addition And MgO Nucleation

Adding 5–20 ppm Mg (as Ni–Mg alloy) during primary melting forms MgO nuclei that serve as heterogeneous nucleation sites for TiN and TiCN during solidification 6,10,13. During subsequent VAR, the high vacuum and elevated temperatures cause Mg to evaporate from the melt surface, dissociating MgO particles and releasing oxygen, which is removed by the vacuum system 6,10,13. This dual mechanism—nucleation followed by dissociation—reduces the total oxygen content to <10 ppm and refines the size distribution of residual oxide inclusions, with spinel-form inclusions (MgAl₂O₄) exhibiting maximum lengths of ≤20 µm and a content rate exceeding 33% relative to alumina inclusions 10. Fatigue strength improvements of 10–15% have been documented for maraging steels produced with Mg addition compared to Mg-free controls 10.

Rare Gas Cooling During VAR

Introducing helium or argon at 0.9–1.9 kPa between the ingot surface and the crucible wall during VAR reduces the molten pool depth to ≤170 mm, minimizing the residence time of inclusions in the liquid phase and promoting their floatation to the top surface 2,4. This shallow pool geometry also suppresses macrosegregation of alloying elements (Co, Mo, Ti) and reduces the size and number density of residual inclusions in the final ingot 2,4. Quantitative metallography of VAR ingots produced with helium cooling shows a 30–40% reduction in the number density of inclusions >10 µm compared to conventional VAR without gas cooling 2,4.

Oxidative Refining Prior To Vacuum Treatment

For maraging steel produced from scrap feedstock, oxidative refining in an arc furnace (under air or oxygen-enriched atmosphere) prior to vacuum induction melting can reduce sulfur (S) and phosphorus (P) contents to <0.01 wt% and promote the formation of easily removable oxide slags 5. This pre-treatment step is particularly effective for scrap-based production routes, where residual tramp elements (Cu, Sn, As) and high S/P levels can compromise fatigue performance 5. Following oxidative refining, the molten steel is transferred to a vacuum induction furnace for compositional adjustment and nitrogen control, resulting in ingots with nitrogen contents of ≤25 ppm and oxygen contents of <10 ppm 5.

Quantitative inclusion analysis (via automated scanning electron microscopy with energy-dispersive X-ray spectroscopy, SEM-EDS) of maraging steel ingots produced with these refinement strategies reveals:

  • Nitride inclusions (TiN, TiCN): Maximum length ≤15 µm, number density 50–150 inclusions/mm² 3,7,10
  • Oxide inclusions (Al₂O₃, MgAl₂O₄): Maximum length ≤20 µm, number density 20–80 inclusions/mm² 10,13
  • Spinel-to-alumina ratio: >0.33 (33%) for inclusions ≥10 µm, indicating effective MgO nucleation and dissociation 10
  • Oxygen content: <10
OrgApplication ScenariosProduct/ProjectTechnical Outcomes
HUAWEI TECHNOLOGIES CO. LTD.Electronic device structural components and aerospace applications requiring ultra-high strength combined with excellent formability.High-Performance Maraging Steel AlloyAchieves both high strength (≥250 kg/mm²) and high plasticity through optimized composition with Co 12-17 wt%, Mo 6-8 wt%, Ti 0.4-1.5 wt%, Ni 15-18 wt%, and Al≤0.3 wt%.
HITACHI METALS LTD.Large-diameter steel ingots (≥650 mm) for aerospace components and tooling applications requiring uniform fatigue strength and minimal inclusion-related defects.VAR Maraging Steel Ingot with Rare Gas CoolingRefines Ti-based inclusions to ≤15 µm maximum length and minimizes size variation across ingot locations through helium/argon cooling at 0.9-1.9 kPa during vacuum arc remelting.
HITACHI METALS LTD.Mission-critical aerospace components such as aircraft engine parts and landing gear requiring consistent high-cycle fatigue performance across large cross-sections.Controlled-Nitrogen Maraging Steel IngotReduces fatigue test result variation by 20-25% and maintains high fatigue strength through controlled nitrogen addition (0.0025-0.0050 mass% N) and Ti content (0.2-3.0 mass%) in remelt electrodes for ingots ≥650 mm diameter.
HITACHI METALS LTD.High-fatigue-resistance applications including aerospace structural components, precision tooling, and thin-strip products requiring superior surface finish and fatigue life.Mg-Refined Maraging Steel IngotAchieves oxide inclusions ≤20 µm maximum length and spinel-form inclusion content >33% through Mg addition (5-20 ppm) in consumable electrode, reducing oxygen to <10 ppm and improving fatigue strength by 10-15%.
HITACHI METALS LTD.Critical fatigue-sensitive applications such as aerospace fasteners, turbine components, and high-performance tooling where inclusion refinement directly impacts service life and reliability.MgO-Nucleated Maraging Steel Production ProcessReliably refines nitride inclusions (TiN, TiCN) to fine sizes and suppresses oxide influence through controlled leak rate (3-20 Pa/min) during primary vacuum melting with Mg addition, followed by vacuum arc remelting with MgO nuclei.
Reference
  • Maraging steel, method for preparing maraging steel, and electronic device
    PatentPendingUS20260097431A1
    View detail
  • Process for manufacturing maraging steel and method for refining inclusions
    PatentActiveTW201504454A
    View detail
  • Production method of maraging steel
    PatentActiveUS11427897B2
    View detail
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