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Steel A321-N (Normalized)

Heat-treated state

ASTM A321

Pick for uniform fine-grain structure, better toughness and predictable machining before final Q&T or for as-supplied service parts.

Budget cost $

Values for the N condition

Other A321 tempers and conditions

A321 is listed in 8 conditions; see the grade overview at A321.

Compare all 8 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Solution annealed
Softest condition — choose for heavy machining, cold forming or when maximum ductility is needed before hardening.27049530143 HB51 W/m·K
HRDefault
Hot rolled
Standard stocked plate condition — cheapest, adequate for weldments and machined parts of moderate duty.30555018163 HB—
NThis page
Normalized
Pick for uniform fine-grain structure, better toughness and predictable machining before final Q&T or for as-supplied service parts.34558525170 HB—
Cold drawn
Bar/shaft stock with raised yield, close tolerance and good surface — use where no further heat treatment is planned.51060012179 HB—
quenched and high-temperature tempered (~600 °C)
Use quenching plus high-temperature tempering near 600 °C for shafts and connecting parts that need 620 MPa yield with 20% elongation and remain reasonably machinable.6208002024 HRC47 W/m·K
Induction hardened
Use for journals, spline and cam surfaces needing wear resistance and compressive residual stress over a tough Q&T core.6408201652 HRC9.5 % IACS
quenched and tempered (~540 °C)
Choose tempering near 540 °C when moderately loaded shafts, pins and gear blanks in sections under about 40 mm need 780 MPa yield, accepting 17% elongation and slower machining.7809501730 HRC—
quenched and low/medium tempered (~450 °C)
Maximum practical through-hardened strength for 0.35 %C steel; limited to thin sections and applications tolerating reduced toughness.9501,1201435 HRC—

What is A321-N?

A321-N is A321 heat treated to N — pick for uniform fine-grain structure, better toughness and predictable machining before final Q&T or for as-supplied service parts. A321-N has a yield strength of 345 MPa (50 ksi) and a tensile strength of 585 MPa (84.8 ksi) — weaker than 75% of steel grades. Elongation at break is 25% and the elastic modulus is 205 GPa (29.7 Msi). A321-N has a density of 7.85 g/cm³ (0.284 lb/in³), heavier than 56% of steel grades. It melts at 1,425°C (2,597 °F). HR is the default condition FabDigit quotes; N is available on request or by drawing note.

Advantages

  • High electrical conductivity — 10.5 % IACS, better than 89% of steel grades
  • Easy to machine — 62/100, better than 89% of steel grades
  • Conducts heat well — 50 W/m·K (28.9 BTU/hr·ft·°F), better than 87% of steel grades
  • Ductile — tolerates forming and impact — 25%, better than 77% of steel grades

Limitations

  • Low fracture toughness — 60 MPa·√m (54.6 ksi·√in), worse than 78% of steel grades
  • Low strength — 345 MPa (50 ksi), worse than 75% of steel grades

A321-N properties

Typical room-temperature values for A321-N; 12 are specific to this condition. Other listed values are A321 reference data and may not represent this condition. Bars are the position among steel grades.

Physical3

A321-N has a density of 7.85 g/cm³ (0.284 lb/in³), heavier than 56% of steel grades. It melts at 1,425°C (2,597 °F).

Density7.85 g/cm³0.28 lb/in³
Melting Point (Solidus)1,425°C2,597 °F
Liquidus Temperature1,495°C2,723 °F

Mechanical16

A321-N has a yield strength of 345 MPa (50 ksi) and a tensile strength of 585 MPa (84.8 ksi) — weaker than 75% of steel grades. Elongation at break is 25% and the elastic modulus is 205 GPa (29.7 Msi).

Elastic (Young's) Modulus205 GPa29.7 Msi
Shear Modulus80 GPa11.6 Msi
Bulk Modulus160 GPa23.2 Msi
Poisson's Ratio0.29
Tensile Strength (Ultimate)585 MPa84.8 ksi
Yield Strength (0.2% offset)345 MPa50 ksi
Elongation at Break25%
Reduction in Area50%
Compressive Strength310 MPa45 ksi
Shear Strength385 MPa55.8 ksi
Fatigue Strength (Endurance Limit)275 MPa39.9 ksi
Fracture Toughness (K_IC)60 MPa·√m54.6 ksi·√in
Charpy V-Notch Impact (RT)58 J42.8 ft·lbf
Hardness, Brinell170 HB
Hardness, Rockwell B86 HRB
Hardness, Vickers172 HV

Thermal6

A321-N is rated for continuous service to 400°C (752 °F). It conducts heat at 50 W/m·K (28.9 BTU/hr·ft·°F), better than 87% of steel grades. Thermal expansion is 11.7 µm/m·K (6.5 µin/in·°F).

Thermal Conductivity50 W/m·K28.9 BTU/hr·ft·°F
Specific Heat Capacity477 J/kg·K0.11 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)11.7 µm/m·K6.5 µin/in·°F
Latent Heat of Fusion247 J/g106 BTU/lb
Max Service Temperature (continuous)400°C752 °F
Min Service Temperature-20°C-4 °F

Electrical3

A321-N conducts electricity at 10.5 % IACS, better than 89% of steel grades.

Electrical Conductivity10.5 % IACS
Electrical Resistivity1.65×10⁻⁷ Ω·m6.5 µΩ·in
Magnetic Responseferromagnetic

Chemical & Environmental3

Corrosion resistance is not recommended (10/100), worse than 86% of steel grades.

Galvanic Potential (seawater, vs SCE)-0.65 V
Corrosion ResistanceNot recommended10/100
Chemical Resistance SummaryRusts freely in moist air, chlorides and dilute acids; acceptable in dry, oily or alkaline (pH>10) environments; requires paint, phosphate, zinc or oil protection for service.

Sustainability4

Producing a kilogram of A321-N takes about 25 MJ of energy and emits 2 kg of CO₂ — less than 82% of steel grades. Typical recycled content is 28%.

Embodied Energy (primary production)25 MJ/kg10,748 BTU/lb
Embodied Carbon (primary production)2 kg CO₂/kg
Embodied Water45 L/kg5.4 gal/lb
Typical Recycled Content28%

Manufacturability6

A321-N's machinability is good (62/100, better than 89% of steel grades); weldability fair (50/100); formability fair (45/100).

MachinabilityGood62/100
Machinability Rating (AISI 1212 = 100 %)65%
WeldabilityFair50/100
Formability (cold)Fair45/100
Brazeability / SolderabilityGood65/100
PolishabilityGood55/100

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

Working with A321-N

Is A321 easy to machine?

Machines well in normalized or Q&T ≤30 HRC with carbide tooling; annealed material tends to smear, so prefer normalized structure and positive-rake geometry for good finish.

Can A321 be welded?

Weldable with low-hydrogen electrodes but CE ≈ 0.5 demands 150–250 °C preheat, controlled interpass and post-weld stress relief to avoid HAZ hardening and cold cracking.

Can A321 be formed, bent or molded?

Hot forge/roll at 1100–1200 °C; cold bending is limited — use generous bend radii (≥2t) or form in the annealed condition.

What surface finishes work on A321?

No inherent corrosion resistance: apply phosphate+oil, zinc plating, black oxide or paint; takes a fine mechanical polish and accepts nitriding or induction hardening for wear surfaces.

A321 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
Cmedium-carbon range, GB/T 699 grade 35 / AISI 10350.32 – 0.40.35
Si0.17 – 0.370.27
Mn0.5 – 0.80.65
P≤ 0.040.02
S≤ 0.040.02
Crresidual≤ 0.250.1
Niresidual≤ 0.30.1
Curesidual≤ 0.250.1
Febalance—

A321-N — frequently asked

What is A321-N used for?

A321-N is typically used for machine parts, medium-strength plate components, structural reinforcements and equipment bases. In short: mid-strength machinable plate; responds to induction hardening; needs preheat for welding.

What is the yield strength of A321-N?

A321-N has a typical yield strength of 345 MPa (50 ksi) and a tensile strength of 585 MPa (84.8 ksi) — weaker than 75% of steel grades. Strength varies by condition: see the 8 listed tempers.

Is A321-N easy to machine?

Reasonably — machinability is rated good (62/100, better than 89% of steel grades). Machines well in normalized or Q&T ≤30 HRC with carbide tooling; annealed material tends to smear, so prefer normalized structure and positive-rake geometry for good finish.

Can A321-N be welded?

With care — weldability is rated fair (50/100). Weldable with low-hydrogen electrodes but CE ≈ 0.5 demands 150–250 °C preheat, controlled interpass and post-weld stress relief to avoid HAZ hardening and cold cracking.

What surface finishes work on A321-N?

No inherent corrosion resistance: apply phosphate+oil, zinc plating, black oxide or paint; takes a fine mechanical polish and accepts nitriding or induction hardening for wear surfaces.

Can A321-N be formed, bent or molded?

Hot forge/roll at 1100–1200 °C; cold bending is limited — use generous bend radii (≥2t) or form in the annealed condition.

What is the maximum service temperature of A321-N?

A321-N 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 A321-HR and A321-IH?

HR is the default condition — standard stocked plate condition — cheapest, adequate for weldments and machined parts of moderate duty. IH: use for journals, spline and cam surfaces needing wear resistance and compressive residual stress over a tough Q&T core. Yield strength is 305 MPa in HR versus 640 MPa in IH.

Sources

  1. GB/T 699 (grade 35) — SAC (2015)
  2. ASTM A321 Steel Bars, Carbon, Quenched and Tempered — ASTM (2016)
  3. ASTM A29/A29M Steel Bars, Carbon and Alloy, Hot-Wrought — ASTM (2020)
  4. ASM Handbook Vol.1: Properties and Selection: Irons, Steels, and High-Performance Alloys — ASM International (1990)
  5. ASM Handbook Vol.4: Heat Treating — ASM International (1991)
  6. Machining Data Handbook — machinability ratings vs AISI 1212 — Metcut Research (1980)

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.