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Stainless Steel 1.4612 +AT (Solution annealed)

Heat-treated state

EN 1.4612

Delivery/intermediate condition for rough machining, forming and welding before precipitation hardening.

High cost $$$$

Values for the +AT condition

Other 1.4612 tempers and conditions

1.4612 is listed in 3 conditions; see the grade overview at 1.4612.

Compare all 3 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
+ATThis page
Solution annealed
Delivery/intermediate condition for rough machining, forming and welding before precipitation hardening.7509501630 HRC—
+P1510Default
Precipitation hardened, Rm ≥ 1510 MPa
Standard high-strength ageing condition: best compromise of ~1500–1700 MPa strength with usable toughness and ductility.1,4501,5801146 HRC—
Precipitation hardened, Rm ≥ 1650 MPa
Peak-strength ageing for the most heavily stressed rings/shafts; accept lower toughness and higher SCC/hydrogen sensitivity.1,5801,720950 HRC—

What is 1.4612 +AT?

1.4612 +AT is 1.4612 heat treated to +AT — delivery/intermediate condition for rough machining, forming and welding before precipitation hardening. 1.4612 +AT has a yield strength of 750 MPa (109 ksi) and a tensile strength of 950 MPa (138 ksi) — stronger than 93% of stainless steel grades. Elongation at break is 16% and the elastic modulus is 200 GPa (29 Msi). 1.4612 +AT has a density of 7.8 g/cm³ (0.282 lb/in³), heavier than 50% of stainless steel grades. It melts at 1,400°C (2,552 °F). +P1510 is the default condition FabDigit quotes; +AT is available on request or by drawing note.

Advantages

  • Polishes to a fine finish — 85/100, better than 97% of stainless steel grades
  • High strength — 750 MPa (109 ksi), better than 93% of stainless steel grades

Limitations

  • Limited ductility — 16%, worse than 88% of stainless steel grades
  • Limited service temperature — 350°C (662 °F), worse than 84% of stainless steel grades

1.4612 +AT properties

Typical room-temperature values for 1.4612 +AT; 19 are specific to this condition. Other listed values are 1.4612 reference data and may not represent this condition. Bars are the position among stainless steel grades.

Physical3

1.4612 +AT has a density of 7.8 g/cm³ (0.282 lb/in³), heavier than 50% of stainless steel grades. It melts at 1,400°C (2,552 °F).

Density7.8 g/cm³0.28 lb/in³
Melting Point (Solidus)1,400°C2,552 °F
Liquidus Temperature1,450°C2,642 °F

Mechanical16

1.4612 +AT has a yield strength of 750 MPa (109 ksi) and a tensile strength of 950 MPa (138 ksi) — stronger than 93% of stainless steel grades. Elongation at break is 16% and the elastic modulus is 200 GPa (29 Msi).

Elastic (Young's) Modulus200 GPa29 Msi
Shear Modulus77 GPa11.2 Msi
Bulk Modulus167 GPa24.2 Msi
Poisson's Ratio0.3
Tensile Strength (Ultimate)950 MPa138 ksi
Yield Strength (0.2% offset)750 MPa109 ksi
Elongation at Break16%
Reduction in Area65%
Compressive Strength770 MPa112 ksi
Shear Strength590 MPa85.6 ksi
Fatigue Strength (Endurance Limit)430 MPa62.4 ksi
Fracture Toughness (K_IC)150 MPa·√m137 ksi·√in
Charpy V-Notch Impact (RT)90 J66.4 ft·lbf
Hardness, Brinell290 HB
Hardness, Rockwell C30 HRC
Hardness, Vickers300 HV

Thermal6

1.4612 +AT is rated for continuous service to 350°C (662 °F). It conducts heat at 17 W/m·K (9.82 BTU/hr·ft·°F), better than 71% of stainless steel grades. Thermal expansion is 10.5 µm/m·K (5.83 µin/in·°F).

Thermal Conductivity17 W/m·K9.8 BTU/hr·ft·°F
Specific Heat Capacity460 J/kg·K0.11 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)10.5 µm/m·K5.8 µin/in·°F
Latent Heat of Fusion270 J/g116 BTU/lb
Max Service Temperature (continuous)350°C662 °F
Min Service Temperature-70°C-94 °F

Electrical3

1.4612 +AT conducts electricity at 2.3 % IACS, better than 55% of stainless steel grades.

Electrical Conductivity2.3 % IACS
Electrical Resistivity7.5×10⁻⁷ Ω·m29.5 µΩ·in
Magnetic Responseferromagnetic

Chemical & Environmental3

Corrosion resistance is good (55/100), worse than 71% of stainless steel grades.

Galvanic Potential (seawater, vs SCE)-0.28 V
Corrosion ResistanceGood55/100
Chemical Resistance SummaryPassive in atmosphere, fresh water, mild industrial and steam environments; the 2 % Mo helps mildly chloride-bearing service but pitting/crevice attack and hydrogen-assisted cracking are real risks at full strength — not for seawater or acids.

Sustainability4

Producing a kilogram of 1.4612 +AT takes about 58 MJ of energy and emits 4.8 kg of CO₂ — more than 66% of stainless steel grades. Typical recycled content is 25%.

Embodied Energy (primary production)58 MJ/kg24,936 BTU/lb
Embodied Carbon (primary production)4.8 kg CO₂/kg
Embodied Water140 L/kg16.8 gal/lb
Typical Recycled Content25%

Manufacturability8

1.4612 +AT's machinability is fair (40/100, better than 72% of stainless steel grades); weldability good (60/100); formability fair (45/100).

MachinabilityFair40/100
Machinability Rating (AISI 1212 = 100 %)35%
WeldabilityGood60/100
Formability (cold)Fair45/100
CastabilityPoor30/100
Brazeability / SolderabilityFair35/100
PolishabilityExcellent85/100
Anodizing Responsen/a — ferrous alloy; use passivation (ASTM A967) or thin dense chrome instead

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

Working with 1.4612 +AT

Is 1.4612 easy to machine?

Rough machine in +AT (≈30 HRC) and leave finish stock; in +P conditions use rigid setups, coated carbide, low speed/high feed and flood coolant — work hardens and burnishes readily.

Can 1.4612 be welded?

Weld only in the solution-annealed condition with matching low-C filler under clean/inert conditions, then re-solution and re-age; welding in the aged state locally overages the HAZ.

Can 1.4612 be formed, bent or molded?

Hot forge/roll well above ~1000 °C and cool controlled; cold forming is limited to light straightening and only in +AT.

What surface finishes work on 1.4612?

Passivate per ASTM A967 after machining; grinding/polishing gives a fine surface, and thin dense chrome or nitriding can be used where wear resistance is needed — no anodizing.

1.4612 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
Cultra-low carbon, VIM/VAR melted≤ 0.010.01
Si≤ 0.10.05
Mn≤ 0.10.05
P≤ 0.020.01
S≤ 0.010
Cr11 – 12.511.8
Nihighest Ni of the 12Cr-Ni-Mo-Al-Ti series10 – 11.511
Mo1.5 – 21.8
TiNi3Ti precipitation hardener0.5 – 1.40.9
AlNiAl precipitation hardener0.2 – 0.80.4
Febalance—

1.4612 +AT — frequently asked

What is 1.4612 +AT used for?

1.4612 +AT is typically used for large turbogenerator retaining rings, rotor forgings, non-magnetic rotor rings, high-strength shafts and pins and heavily loaded clamping rings. In short: highest-strength retaining ring; 1580 MPa tensile; non-magnetic when aged.

What is the yield strength of 1.4612 +AT?

1.4612 +AT has a typical yield strength of 750 MPa (109 ksi) and a tensile strength of 950 MPa (138 ksi) — stronger than 93% of stainless steel grades. Strength varies by condition: see the 3 listed tempers.

Is 1.4612 +AT easy to machine?

Not especially — machinability is rated fair (40/100, better than 72% of stainless steel grades). Rough machine in +AT (≈30 HRC) and leave finish stock; in +P conditions use rigid setups, coated carbide, low speed/high feed and flood coolant — work hardens and burnishes readily.

Can 1.4612 +AT be welded?

Yes — weldability is rated good (60/100). Weld only in the solution-annealed condition with matching low-C filler under clean/inert conditions, then re-solution and re-age; welding in the aged state locally overages the HAZ.

What surface finishes work on 1.4612 +AT?

Passivate per ASTM A967 after machining; grinding/polishing gives a fine surface, and thin dense chrome or nitriding can be used where wear resistance is needed — no anodizing.

Can 1.4612 +AT be formed, bent or molded?

Hot forge/roll well above ~1000 °C and cool controlled; cold forming is limited to light straightening and only in +AT.

What is the maximum service temperature of 1.4612 +AT?

1.4612 +AT is rated for continuous use to about 350°C (662 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

Sources

  1. EN 10088-3 Stainless steels — Technical delivery conditions for semi-finished products, bars, rods — CEN (2014)
  2. EN 10088-1 Stainless steels — List of stainless steels (physical properties) — CEN (2014)
  3. ASM Handbook Vol. 1 — Properties and Selection: Irons, Steels, and High-Performance Alloys (PH stainless steels) — ASM International (1990)
  4. ASTM A564/A564M — Hot-Rolled and Cold-Finished Age-Hardening Stainless Steel Bars (UNS S13800 comparison) — ASTM (2019)
  5. Maraging-type 12Cr-Ni-Mo-Al-Ti stainless forging grades (comparative producer data) — Special steel producers (e.g. Böhler/voestalpine, Aubert & Duval) (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.