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Steel 15B41 QT-33-39HRC

Hardness band · default condition

EN 15B41 · UNS G15411

The workhorse fastener condition: full through-hardening plus ≥425 °C temper for 1040 MPa minimum tensile.

Budget cost $

Values for the QT-33-39HRC condition

Other 15B41 tempers and conditions

15B41 is listed in 9 conditions; see the grade overview at 15B41.

Compare all 9 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Spheroidize annealed
Standard condition for cold-heading and cold-extruding bolt blanks before quench and temper.32055030155 HB—
Solution annealed
Softest ferrite/pearlite condition for machining or severe forming before hardening.35060025170 HB—
Hot rolled
Mill-supply condition for bar and coil that will be re-heated, forged or heat treated by the customer.41572518210 HB—
Normalized
Uniform fine grain and predictable response before hardening; used for forgings.48078018225 HB—
Cold drawn
Sized, straight bar with raised yield strength for as-machined parts not requiring hardening.64076012217 HB—
quenched and high-temper (Grade 5 class)
Choose for tough, moderately strong bolts and machine parts where impact matters more than peak strength.8009501629 HRC—
QT-33-39HRCDefaultThis page
quenched and tempered (Grade 8 class)
The workhorse fastener condition: full through-hardening plus ≥425 °C temper for 1040 MPa minimum tensile.1,0301,1601336 HRC—
quenched and low-temper
Pick for wear-loaded parts, self-drilling/track bolts and shafts where strength and abrasion beat toughness.1,2501,4001042 HRC—
As-quenched
Intermediate process condition only — maximum hardness but brittle; always temper before service.1,5502,000255 HRC7 % IACS

What is 15B41 QT-33-39HRC?

15B41 QT-33-39HRC is 15B41 heat treated to QT-33-39HRC — the workhorse fastener condition: full through-hardening plus ≥425 °C temper for 1040 MPa minimum tensile. 15B41 QT-33-39HRC has a yield strength of 1,030 MPa (149 ksi) and a tensile strength of 1,160 MPa (168 ksi) — stronger than 93% of steel grades. Elongation at break is 13% and the elastic modulus is 205 GPa (29.7 Msi). 15B41 QT-33-39HRC has a density of 7.85 g/cm³ (0.284 lb/in³), heavier than 56% of steel grades. It melts at 1,420°C (2,588 °F).

Advantages

  • High strength — 1,030 MPa (149 ksi), better than 93% of steel grades

Limitations

  • Limited formability — 20/100, worse than 80% of steel grades
  • Limited ductility — 13%, worse than 78% of steel grades
  • Low fracture toughness — 60 MPa·√m (54.6 ksi·√in), worse than 78% of steel grades
  • Limited service temperature — 300°C (572 °F), worse than 78% of steel grades
  • Difficult to machine — 40/100, worse than 77% of steel grades

15B41 QT-33-39HRC properties

Typical room-temperature values for 15B41 QT-33-39HRC; 14 are specific to this condition. Other listed values are 15B41 reference data and may not represent this condition. Bars are the position among steel grades.

Physical3

15B41 QT-33-39HRC has a density of 7.85 g/cm³ (0.284 lb/in³), heavier than 56% of steel grades. It melts at 1,420°C (2,588 °F).

Density7.85 g/cm³0.28 lb/in³
Melting Point (Solidus)1,420°C2,588 °F
Liquidus Temperature1,490°C2,714 °F

Mechanical16

15B41 QT-33-39HRC has a yield strength of 1,030 MPa (149 ksi) and a tensile strength of 1,160 MPa (168 ksi) — stronger than 93% of steel grades. Elongation at break is 13% 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)1,160 MPa168 ksi
Yield Strength (0.2% offset)1,030 MPa149 ksi
Elongation at Break13%
Reduction in Area45%
Compressive Strength1,080 MPa157 ksi
Shear Strength700 MPa102 ksi
Fatigue Strength (Endurance Limit)520 MPa75.4 ksi
Fracture Toughness (K_IC)60 MPa·√m54.6 ksi·√in
Charpy V-Notch Impact (RT)40 J29.5 ft·lbf
Hardness, Brinell336 HB
Hardness, Rockwell C36 HRC
Hardness, Vickers350 HV

Thermal6

15B41 QT-33-39HRC is rated for continuous service to 300°C (572 °F). It conducts heat at 44 W/m·K (25.4 BTU/hr·ft·°F), better than 57% of steel grades. Thermal expansion is 11.7 µm/m·K (6.5 µin/in·°F).

Thermal Conductivity44 W/m·K25.4 BTU/hr·ft·°F
Specific Heat Capacity470 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 Fusion250 J/g107 BTU/lb
Max Service Temperature (continuous)300°C572 °F
Min Service Temperature-40°C-40 °F

Electrical3

15B41 QT-33-39HRC conducts electricity at 8.6 % IACS, better than 66% of steel grades.

Electrical Conductivity8.6 % IACS
Electrical Resistivity2×10⁻⁷ Ω·m7.87 µΩ·in
Magnetic Responseferromagnetic

Chemical & Environmental3

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

Galvanic Potential (seawater, vs SCE)-0.6 V
Corrosion ResistanceNot recommended10/100
Chemical Resistance SummaryRusts freely in humid air and water; no resistance to acids or chlorides. Q&T parts above ~1000 MPa are susceptible to hydrogen embrittlement — electroplating requires post-plate baking; prefer zinc flake or mechanical galvanizing.

Sustainability4

Producing a kilogram of 15B41 QT-33-39HRC takes about 26 MJ of energy and emits 2 kg of CO₂ — less than 64% of steel grades. Typical recycled content is 30%.

Embodied Energy (primary production)26 MJ/kg11,178 BTU/lb
Embodied Carbon (primary production)2 kg CO₂/kg
Embodied Water45 L/kg5.4 gal/lb
Typical Recycled Content30%

Manufacturability6

15B41 QT-33-39HRC's machinability is fair (40/100, worse than 77% of steel grades); weldability poor (25/100); formability poor (20/100).

MachinabilityFair40/100
Machinability Rating (AISI 1212 = 100 %)40%
WeldabilityPoor25/100
Formability (cold)Poor20/100
Brazeability / SolderabilityFair45/100
PolishabilityGood60/100

Common Calculations5

Specific Strength (UTS / density)calculated148 kN·m/kg
Specific Stiffness (E / density)calculated26.1 MN·m/kg
Modulus of Resiliencecalculated2,588 kJ/m³
Thermal Diffusivitycalculated11.9 mm²/s
Thermal Shock Resistance Indexcalculated21

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

Working with 15B41 QT-33-39HRC

Is 15B41 easy to machine?

Machine in the annealed or spheroidized state (~55 % of 1212); in Q&T at 33–39 HRC use coated carbide, rigid setups and reduced speeds, and finish-grind after hardening for tight tolerances.

Can 15B41 be welded?

Poor — high carbon equivalent plus boron gives a hard, crack-prone HAZ; if welding is unavoidable use low-hydrogen consumables, 200–300 °C preheat and immediate stress-relief/temper, and expect loss of the Q&T properties.

Can 15B41 be formed, bent or molded?

Cold-head and cold-extrude in the spheroidize-annealed condition (excellent CHQ behaviour); hot forge 1100–1220 °C, then normalize before hardening. Austenitize ~840–860 °C, oil or polymer quench, temper 425–540 °C to the required hardness band.

What surface finishes work on 15B41?

No inherent corrosion resistance — zinc, zinc-nickel, phosphate-and-oil or zinc-flake (Dacromet/Geomet) coatings are standard; for parts above ~1000 MPa avoid or bake after electroplating (ASTM F1941/B850) to prevent hydrogen embrittlement.

15B41 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
Csome listings quote 0.36–0.44 (as SAE 1541)0.35 – 0.450.4
Mn1.35 – 1.651.5
Sikilled-steel silicon range; may be restricted for CHQ wire0.15 – 0.350.22
P≤ 0.030.02
Smax, non-resulfurized≤ 0.050.02
Beffective (soluble) boron; requires Ti/Al nitrogen control5×10⁻⁴ – 00
Febalance—

15B41 QT-33-39HRC — frequently asked

What is 15B41 QT-33-39HRC used for?

15B41 QT-33-39HRC is typically used for grade 8 bolts, high-strength fasteners, threaded studs and rods, cold-extruded shafts, suspension and chassis fastenings and wheel studs. In short: grade 8 bolt boron steel; through-hardens to 45 HRC; not for welded assemblies.

What is the yield strength of 15B41 QT-33-39HRC?

15B41 QT-33-39HRC has a typical yield strength of 1,030 MPa (149 ksi) and a tensile strength of 1,160 MPa (168 ksi) — stronger than 93% of steel grades. Strength varies by condition: see the 9 listed tempers.

Is 15B41 QT-33-39HRC easy to machine?

Not especially — machinability is rated fair (40/100, worse than 77% of steel grades). Machine in the annealed or spheroidized state (~55 % of 1212); in Q&T at 33–39 HRC use coated carbide, rigid setups and reduced speeds, and finish-grind after hardening for tight tolerances.

Can 15B41 QT-33-39HRC be welded?

Not readily — weldability is rated poor (25/100). Poor — high carbon equivalent plus boron gives a hard, crack-prone HAZ; if welding is unavoidable use low-hydrogen consumables, 200–300 °C preheat and immediate stress-relief/temper, and expect loss of the Q&T properties.

What surface finishes work on 15B41 QT-33-39HRC?

No inherent corrosion resistance — zinc, zinc-nickel, phosphate-and-oil or zinc-flake (Dacromet/Geomet) coatings are standard; for parts above ~1000 MPa avoid or bake after electroplating (ASTM F1941/B850) to prevent hydrogen embrittlement.

Can 15B41 QT-33-39HRC be formed, bent or molded?

Cold-head and cold-extrude in the spheroidize-annealed condition (excellent CHQ behaviour); hot forge 1100–1220 °C, then normalize before hardening. Austenitize ~840–860 °C, oil or polymer quench, temper 425–540 °C to the required hardness band.

What is the maximum service temperature of 15B41 QT-33-39HRC?

15B41 QT-33-39HRC is rated for continuous use to about 300°C (572 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between 15B41 QT-33-39HRC and 15B41-SA?

QT-33-39HRC is the default condition — the workhorse fastener condition: full through-hardening plus ≥425 °C temper for 1040 MPa minimum tensile. SA: standard condition for cold-heading and cold-extruding bolt blanks before quench and temper. Yield strength is 1,030 MPa in QT-33-39HRC versus 320 MPa in SA.

Sources

  1. SAE J403 — Chemical Compositions of SAE Carbon Steels (incl. boron grades) — SAE International (2014)
  2. ASTM A29/A29M — Steel Bars, Carbon and Alloy, Hot-Wrought, General Requirements — ASTM (2020)
  3. SAE J429 — Mechanical and Material Requirements for Externally Threaded Fasteners — SAE International (2014)
  4. SAE J1268 — Hardenability Bands for Carbon and Alloy H Steels (15B41H) — SAE International (2019)
  5. ASM Handbook Vol.1 — Properties and Selection: Irons, Steels, and High-Performance Alloys — ASM International (1990)
  6. ASM Handbook Vol.4A — Steel Heat Treating Fundamentals and Processes (boron hardenability) — ASM International (2013)
  7. GB/T 3077 — Alloy Structural Steels (40MnB comparison grade) — SAC (2015)

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.