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Steel 18Ni(190) VIM-VAR

Grade

also T-190, VascoMax 190

VIM-VAR = vacuum induction melted + vacuum arc remelted

Order this melt route for aerospace/critical rotating parts: lowest inclusion content, best transverse ductility and fracture toughness at the same nominal strength.

High cost $$$$

Values for the VIM-VAR condition

Other 18Ni(190) tempers and conditions

18Ni(190) is listed in 6 conditions; see the grade overview at 18Ni(190).

Compare all 6 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Annealed
Soft, tough nickel-martensite as supplied for machining, forming and welding before aging.8001,0001829 HRC2.9 % IACS
As-welded deposit
Condition of a weldment before the mandatory 480 °C re-age; strength is well below the aged parent and should not be used as a design basis.8601,0501231 HRC3.1 % IACS
Cold drawn
Cold-drawn bar and wire for tighter tolerance and better surface before aging; strain hardening also raises the final aged strength.1,0301,1701034 HRC3 % IACS
AgedDefault
Solution annealed + aged 480 °C / 3–6 h, air cool
Standard delivered-strength condition: ~190 ksi UTS with the best toughness of the 18 % Ni maraging series and almost no distortion during aging.1,2801,3301440 HRC3.8 % IACS
VIM-VARThis page
Vacuum induction melted + vacuum arc remelted
Order this melt route for aerospace/critical rotating parts: lowest inclusion content, best transverse ductility and fracture toughness at the same nominal strength.1,3001,3401540 HRC3.8 % IACS
Cold worked then aged 480 °C
Pick when extra strength is needed from thin bar, strip or wire; ductility and toughness drop relative to the plain aged condition.1,4501,500845 HRC—

What is 18Ni(190) VIM-VAR?

18Ni(190) VIM-VAR is 18Ni(190) in the VIM-VAR grade — order this melt route for aerospace/critical rotating parts: lowest inclusion content, best transverse ductility and fracture toughness at the same nominal strength. 18Ni(190) VIM-VAR has a yield strength of 1,300 MPa (189 ksi) and a tensile strength of 1,340 MPa (194 ksi) — stronger than 95% of steel grades. Elongation at break is 15% and the elastic modulus is 190 GPa (27.6 Msi). 18Ni(190) VIM-VAR has a density of 8 g/cm³ (0.289 lb/in³), heavier than 95% of steel grades. It melts at 1,413°C (2,575 °F). Aged is the default condition FabDigit quotes; VIM-VAR is available on request or by drawing note.

Advantages

  • Tough — resists crack growth — 175 MPa·√m (159.3 ksi·√in), better than 98% of steel grades
  • Polishes to a fine finish — 80/100, better than 97% of steel grades
  • High strength — 1,300 MPa (189 ksi), better than 95% of steel grades
  • Good corrosion resistance — 25/100, better than 92% of steel grades
  • Readily welded — 90/100, better than 90% of steel grades

Limitations

  • High embodied carbon — 4.6 kg CO₂/kg, worse than 96% of steel grades
  • Poor heat conductor — 20.9 W/m·K (12.1 BTU/hr·ft·°F), worse than 95% of steel grades
  • Low electrical conductivity — 3.8 % IACS, worse than 84% of steel grades
  • Difficult to machine — 35/100, worse than 84% of steel grades
  • Limited formability — 20/100, worse than 80% of steel grades

18Ni(190) VIM-VAR properties

Typical room-temperature values for 18Ni(190) VIM-VAR; 22 are specific to this condition. Other listed values are 18Ni(190) reference data and may not represent this condition. Bars are the position among steel grades.

Physical3

18Ni(190) VIM-VAR has a density of 8 g/cm³ (0.289 lb/in³), heavier than 95% of steel grades. It melts at 1,413°C (2,575 °F).

Density8 g/cm³0.29 lb/in³
Melting Point (Solidus)1,413°C2,575 °F
Liquidus Temperature1,454°C2,649 °F

Mechanical16

18Ni(190) VIM-VAR has a yield strength of 1,300 MPa (189 ksi) and a tensile strength of 1,340 MPa (194 ksi) — stronger than 95% of steel grades. Elongation at break is 15% and the elastic modulus is 190 GPa (27.6 Msi).

Elastic (Young's) Modulus190 GPa27.6 Msi
Shear Modulus72 GPa10.4 Msi
Bulk Modulus160 GPa23.2 Msi
Poisson's Ratio0.3
Tensile Strength (Ultimate)1,340 MPa194 ksi
Yield Strength (0.2% offset)1,300 MPa189 ksi
Elongation at Break15%
Reduction in Area70%
Compressive Strength1,320 MPa191 ksi
Shear Strength810 MPa117 ksi
Fatigue Strength (Endurance Limit)660 MPa95.7 ksi
Fracture Toughness (K_IC)175 MPa·√m159 ksi·√in
Charpy V-Notch Impact (RT)85 J62.7 ft·lbf
Hardness, Brinell375 HB
Hardness, Rockwell C40 HRC
Hardness, Vickers395 HV

Thermal6

18Ni(190) VIM-VAR is rated for continuous service to 400°C (752 °F). It conducts heat at 20.9 W/m·K (12.1 BTU/hr·ft·°F), worse than 95% of steel grades. Thermal expansion is 10.1 µm/m·K (5.61 µin/in·°F).

Thermal Conductivity20.9 W/m·K12.1 BTU/hr·ft·°F
Specific Heat Capacity452 J/kg·K0.11 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)10.1 µm/m·K5.6 µin/in·°F
Latent Heat of Fusion270 J/g116 BTU/lb
Max Service Temperature (continuous)400°C752 °F
Min Service Temperature-196°C-321 °F

Electrical3

18Ni(190) VIM-VAR conducts electricity at 3.8 % IACS, worse than 84% of steel grades.

Electrical Conductivity3.8 % IACS
Electrical Resistivity4.5×10⁻⁷ Ω·m17.7 µΩ·in
Magnetic Responseferromagnetic

Chemical & Environmental3

Corrosion resistance is poor (25/100), better than 92% of steel grades.

Galvanic Potential (seawater, vs SCE)-0.6 V
Corrosion ResistancePoor25/100
Chemical Resistance SummaryRusts in humid air and seawater; needs cadmium/nickel plating, phosphating or paint. Resists general uniform attack better than plain carbon steel but is susceptible to hydrogen embrittlement and to stress-corrosion cracking in chloride media at high stress; avoid acid pickling without baking.

Sustainability4

Producing a kilogram of 18Ni(190) VIM-VAR takes about 55 MJ of energy and emits 4.6 kg of CO₂ — more than 94% of steel grades. Typical recycled content is 25%.

Embodied Energy (primary production)55 MJ/kg23,646 BTU/lb
Embodied Carbon (primary production)4.6 kg CO₂/kg
Embodied Water120 L/kg14.4 gal/lb
Typical Recycled Content25%

Manufacturability7

18Ni(190) VIM-VAR's machinability is fair (35/100, worse than 84% of steel grades); weldability excellent (90/100); formability poor (20/100).

MachinabilityFair35/100
Machinability Rating (AISI 1212 = 100 %)32%
WeldabilityExcellent90/100
Formability (cold)Poor20/100
Brazeability / SolderabilityFair50/100
PolishabilityVery good80/100
Anodizing Responsen/a — ferrous alloy; use plating, phosphate or nitriding instead of anodizing

Values are nominal handbook figures for design screening. Confirm any required mill or lot documentation when quoting.

Working with 18Ni(190) VIM-VAR

Is 18Ni(190) easy to machine?

Rough machine in the annealed condition (~30 HRC) with sharp carbide tools, rigid setups and generous coolant; finish after aging where only ~0.05 % growth occurs, using slow, positive-rake cuts.

Can 18Ni(190) be welded?

Excellent GTAW/EBW/laser weldability with matching filler, no preheat and low heat input; keep the joint clean and re-age at 480 °C after welding to restore strength.

Can 18Ni(190) be formed, bent or molded?

Form, bend, deep-draw or cold-draw only in the solution-annealed state; hot work 1150–900 °C, then re-anneal at 815 °C before aging.

What surface finishes work on 18Ni(190)?

No anodizing; protect with cadmium, nickel or electroless-nickel plating, phosphate or paint, and bake after any plating/pickling to avoid hydrogen embrittlement — nitriding gives a hard 65+ HRC case during aging.

18Ni(190) chemical composition (wt %)

Limits by weight percent from the governing specification, written the way the spec states them — a single maximum for impurities, a range for alloying elements, and the base element as balance. Nominal is the typical mid-range value.

ElementSpec limit (wt %)Nominal
Ckept very low; carbon degrades toughness≤ 0.030.02
Ni17 – 1918
Copromotes Mo precipitation8 – 98.5
MoNi3Mo / Fe2Mo aging precipitates2.8 – 3.43.1
Tilower Ti than 250/300 grades — sets the 190 ksi level0.1 – 0.250.18
Al0.05 – 0.150.1
Si≤ 0.10.05
Mn≤ 0.10.05
S≤ 0.010
P≤ 0.010.01
Bgrain-boundary addition, optional≤ 00
Zroptional≤ 0.020.01
Caoptional deoxidizer≤ 0.050.02
Febalance—

18Ni(190) VIM-VAR — frequently asked

What is 18Ni(190) VIM-VAR used for?

18Ni(190) VIM-VAR is typically used for fracture-critical aerospace fittings, tooling requiring high toughness, pressure vessel components and rocket motor cases (lower-load variants). In short: toughest 18Ni maraging grade; weldable ultra-high-strength steel; near-zero ageing distortion.

What is the yield strength of 18Ni(190) VIM-VAR?

18Ni(190) VIM-VAR has a typical yield strength of 1,300 MPa (189 ksi) and a tensile strength of 1,340 MPa (194 ksi) — stronger than 95% of steel grades. Strength varies by condition: see the 6 listed tempers.

Is 18Ni(190) VIM-VAR easy to machine?

Not especially — machinability is rated fair (35/100, worse than 84% of steel grades). Rough machine in the annealed condition (~30 HRC) with sharp carbide tools, rigid setups and generous coolant; finish after aging where only ~0.05 % growth occurs, using slow, positive-rake cuts.

Can 18Ni(190) VIM-VAR be welded?

Yes — weldability is rated excellent (90/100). Excellent GTAW/EBW/laser weldability with matching filler, no preheat and low heat input; keep the joint clean and re-age at 480 °C after welding to restore strength.

What surface finishes work on 18Ni(190) VIM-VAR?

No anodizing; protect with cadmium, nickel or electroless-nickel plating, phosphate or paint, and bake after any plating/pickling to avoid hydrogen embrittlement — nitriding gives a hard 65+ HRC case during aging.

Can 18Ni(190) VIM-VAR be formed, bent or molded?

Form, bend, deep-draw or cold-draw only in the solution-annealed state; hot work 1150–900 °C, then re-anneal at 815 °C before aging.

What is the maximum service temperature of 18Ni(190) VIM-VAR?

18Ni(190) VIM-VAR is rated for continuous use to about 400°C (752 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between 18Ni(190) Aged and 18Ni(190)-ANN?

Aged is the default condition — standard delivered-strength condition: ~190 ksi UTS with the best toughness of the 18 % Ni maraging series and almost no distortion during aging. ANN: soft, tough nickel-martensite as supplied for machining, forming and welding before aging. Yield strength is 1,280 MPa in Aged versus 800 MPa in ANN.

Sources

  1. ASTM A538/A538M — Pressure Vessel Plates, Alloy Steel, Precipitation Hardening (Maraging), 18 % Nickel — ASTM International (2019)
  2. AMS 6512 / AMS 6520 — 18Ni maraging steel bar, plate and sheet — SAE International (2018)
  3. ASM Handbook Vol.1, Properties and Selection: Irons, Steels and High-Performance Alloys — Maraging Steels — ASM International (1990)
  4. ASM Specialty Handbook: Carbon and Alloy Steels — ASM International (1996)
  5. VascoMax / Marval 18 Ni maraging steel technical data — Carpenter / Aubert & Duval (2020)
  6. MMPDS-17 maraging steel design allowables (18Ni series) — Battelle (2022)

Property data is compiled from published supplier and standards handbooks and normalised for comparison. Nothing on this page is a certification — request mill certs, CoC or material test reports with your order.