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Steel 60SiCr8 QT-48

Hardness band · default condition

EN 60SiCr8 · JIS SUP12 · GB 60Si2CrA

QT-48 = q&T 46–50 HRC

The normal working condition for coil and suspension springs — best balance of strength, relaxation resistance and toughness.

Budget cost $

Values for the QT-48 condition

Other 60SiCr8 tempers and conditions

60SiCr8 is listed in 9 conditions; see the grade overview at 60SiCr8.

Compare all 9 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Solution annealed
Softest supply condition for machining, cold coiling of heavy bar, or upsetting before hardening.48080016235 HB—
Normalized
Grain-refined intermediate condition used after hot forming and before final hardening.6201,0001230 HRC5.6 % IACS
Hot rolled
Mill supply condition for leaf-spring and bar stock that will be hot formed and then quenched and tempered.6501,0501131 HRC5.5 % IACS
Cold drawn
Close-tolerance bright bar or pre-drawn wire for machining and subsequent hardening.780950829 HRC5.4 % IACS
Q&T 42–46 HRC
Choose when impact toughness and shot-blast tolerance matter more than maximum stress, e.g. leaf springs and torsion bars.1,3001,4501044 HRC—
QT-48DefaultThis page
Q&T 46–50 HRC
The normal working condition for coil and suspension springs — best balance of strength, relaxation resistance and toughness.1,5501,750848 HRC—
Q&T + stress relieved and shot peened spring
Finished-spring condition: compressive surface residual stress raises fatigue limit substantially over the as-tempered state.1,5501,750848 HRC5.2 % IACS
Q&T 50–54 HRC
Maximum stress capacity for small-section, highly stressed springs; accept low ductility and high notch/decarburization sensitivity.1,7501,950652 HRC—
oil hardened and tempered valve-spring wire (EN 10270-2 VDSiCr type)
Continuously oil-hardened-and-tempered clean-steel wire for valve and high-cycle suspension springs; highest strength and cleanliness class.1,8502,050654 HRC—

What is 60SiCr8 QT-48?

60SiCr8 QT-48 is 60SiCr8 heat treated to QT-48 — the normal working condition for coil and suspension springs — best balance of strength, relaxation resistance and toughness. 60SiCr8 QT-48 has a yield strength of 1,550 MPa (225 ksi) and a tensile strength of 1,750 MPa (254 ksi) — stronger than 97% of steel grades. Elongation at break is 8% and the elastic modulus is 206 GPa (29.9 Msi). 60SiCr8 QT-48 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 — 1,550 MPa (225 ksi), better than 97% of steel grades

Limitations

  • Difficult to machine — 15/100, worse than 98% of steel grades
  • Low fracture toughness — 30 MPa·√m (27.3 ksi·√in), worse than 96% of steel grades
  • Difficult to weld — 12/100, worse than 96% of steel grades
  • Limited ductility — 8%, worse than 95% of steel grades
  • Limited formability — 10/100, worse than 95% of steel grades

60SiCr8 QT-48 properties

Typical room-temperature values for 60SiCr8 QT-48; 13 are specific to this condition. Other listed values are 60SiCr8 reference data and may not represent this condition. Bars are the position among steel grades.

Physical3

60SiCr8 QT-48 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

60SiCr8 QT-48 has a yield strength of 1,550 MPa (225 ksi) and a tensile strength of 1,750 MPa (254 ksi) — stronger than 97% of steel grades. Elongation at break is 8% and the elastic modulus is 206 GPa (29.9 Msi).

Elastic (Young's) Modulus206 GPa29.9 Msi
Shear Modulus79 GPa11.5 Msi
Bulk Modulus160 GPa23.2 Msi
Poisson's Ratio0.29
Tensile Strength (Ultimate)1,750 MPa254 ksi
Yield Strength (0.2% offset)1,550 MPa225 ksi
Elongation at Break8%
Reduction in Area30%
Compressive Strength1,600 MPa232 ksi
Shear Strength1,050 MPa152 ksi
Fatigue Strength (Endurance Limit)750 MPa109 ksi
Fracture Toughness (K_IC)30 MPa·√m27.3 ksi·√in
Charpy V-Notch Impact (RT)15 J11.1 ft·lbf
Hardness, Brinell460 HB
Hardness, Rockwell C48 HRC
Hardness, Vickers490 HV

Thermal6

60SiCr8 QT-48 is rated for continuous service to 250°C (482 °F). It conducts heat at 30 W/m·K (17.3 BTU/hr·ft·°F), worse than 83% of steel grades. Thermal expansion is 11.5 µm/m·K (6.39 µin/in·°F).

Thermal Conductivity30 W/m·K17.3 BTU/hr·ft·°F
Specific Heat Capacity475 J/kg·K0.11 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)11.5 µm/m·K6.4 µin/in·°F
Latent Heat of Fusion250 J/g107 BTU/lb
Max Service Temperature (continuous)250°C482 °F
Min Service Temperature-50°C-58 °F

Electrical3

60SiCr8 QT-48 conducts electricity at 5.2 % IACS, worse than 81% of steel grades.

Electrical Conductivity5.2 % IACS
Electrical Resistivity3.3×10⁻⁷ Ω·m13 µΩ·in
Magnetic Responseferromagnetic

Chemical & Environmental3

Corrosion resistance is not recommended (12/100), worse than 53% of steel grades.

Galvanic Potential (seawater, vs SCE)-0.6 V
Corrosion ResistanceNot recommended12/100
Chemical Resistance SummaryNo inherent corrosion resistance: rusts in humid air and readily in chlorides; high-strength condition is susceptible to hydrogen embrittlement from acid pickling or electroplating — use mechanical/zinc-flake coatings and bake after plating.

Sustainability4

Producing a kilogram of 60SiCr8 QT-48 takes about 30 MJ of energy and emits 2.1 kg of CO₂ — more than 56% of steel grades. Typical recycled content is 30%.

Embodied Energy (primary production)30 MJ/kg12,898 BTU/lb
Embodied Carbon (primary production)2.1 kg CO₂/kg
Embodied Water60 L/kg7.2 gal/lb
Typical Recycled Content30%

Manufacturability5

60SiCr8 QT-48's machinability is poor (15/100, worse than 98% of steel grades); weldability not recommended (12/100); formability not recommended (10/100).

MachinabilityPoor15/100
Machinability Rating (AISI 1212 = 100 %)15%
WeldabilityNot recommended12/100
Formability (cold)Not recommended10/100
PolishabilityGood60/100

Common Calculations5

Specific Strength (UTS / density)calculated223 kN·m/kg
Specific Stiffness (E / density)calculated26.2 MN·m/kg
Modulus of Resiliencecalculated5,831 kJ/m³
Thermal Diffusivitycalculated8 mm²/s
Thermal Shock Resistance Indexcalculated22

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

Working with 60SiCr8 QT-48

Is 60SiCr8 easy to machine?

Machine in the spheroidize-annealed state (≈235 HB) with coated carbide; above 45 HRC use grinding or CBN only, and keep decarburized skin off spring surfaces.

Can 60SiCr8 be welded?

Effectively non-weldable for spring duty (C ≈ 0.60 %, high Si); if unavoidable, preheat 300–400 °C, low-hydrogen consumables and re-quench/temper the joint.

Can 60SiCr8 be formed, bent or molded?

Cold coil in annealed or oil-tempered wire condition; heavy sections hot form at 900–1050 °C, then austenitize 860–900 °C, oil quench and temper 400–480 °C for 45–50 HRC.

What surface finishes work on 60SiCr8?

Shot peen springs after stress relief for fatigue life; protect with zinc-flake, phosphate+oil or powder coat — avoid acid pickling and electroplating without post-bake due to hydrogen embrittlement risk.

60SiCr8 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
C0.55 – 0.650.6
SiGB 60Si2CrA uses 1.40–1.80 %1.6 – 2.11.85
Mn0.6 – 10.8
CrGB 60Si2CrA and JIS SUP12 run 0.60–1.00 % Cr0.2 – 0.450.3
P≤ 0.03—
S≤ 0.03—
Curesidual, max≤ 0.2—
Febalance—

60SiCr8 QT-48 — frequently asked

What is 60SiCr8 QT-48 used for?

60SiCr8 QT-48 is typically used for valve springs, suspension coil springs and clutch springs. In short: high sag resistance; valve-spring quality steel; not a fabrication steel.

What is the yield strength of 60SiCr8 QT-48?

60SiCr8 QT-48 has a typical yield strength of 1,550 MPa (225 ksi) and a tensile strength of 1,750 MPa (254 ksi) — stronger than 97% of steel grades. Strength varies by condition: see the 9 listed tempers.

Is 60SiCr8 QT-48 easy to machine?

Not especially — machinability is rated poor (15/100, worse than 98% of steel grades). Machine in the spheroidize-annealed state (≈235 HB) with coated carbide; above 45 HRC use grinding or CBN only, and keep decarburized skin off spring surfaces.

Can 60SiCr8 QT-48 be welded?

Not readily — weldability is rated not recommended (12/100). Effectively non-weldable for spring duty (C ≈ 0.60 %, high Si); if unavoidable, preheat 300–400 °C, low-hydrogen consumables and re-quench/temper the joint.

What surface finishes work on 60SiCr8 QT-48?

Shot peen springs after stress relief for fatigue life; protect with zinc-flake, phosphate+oil or powder coat — avoid acid pickling and electroplating without post-bake due to hydrogen embrittlement risk.

Can 60SiCr8 QT-48 be formed, bent or molded?

Cold coil in annealed or oil-tempered wire condition; heavy sections hot form at 900–1050 °C, then austenitize 860–900 °C, oil quench and temper 400–480 °C for 45–50 HRC.

What is the maximum service temperature of 60SiCr8 QT-48?

60SiCr8 QT-48 is rated for continuous use to about 250°C (482 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between 60SiCr8 QT-48 and 60SiCr8-A?

QT-48 is the default condition — the normal working condition for coil and suspension springs — best balance of strength, relaxation resistance and toughness. A: softest supply condition for machining, cold coiling of heavy bar, or upsetting before hardening. Yield strength is 1,550 MPa in QT-48 versus 480 MPa in A.

Sources

  1. EN 10089 — Hot rolled steels for quenched and tempered springs — CEN (2002)
  2. EN 10270-2 — Steel wire for mechanical springs: oil hardened and tempered spring steel wire — CEN (2011)
  3. GB/T 1222 — (60Si2CrA) — SAC (2016)
  4. JIS G 4801 — Spring steels (SUP12) — JISC (2011)
  5. ASM Handbook Vol.1 — Properties and Selection: Irons, Steels, and High-Performance Alloys — ASM International (1990)
  6. ASM Handbook Vol.19 — Fatigue and Fracture — ASM International (1996)
  7. EN 13906-1 — Cylindrical helical springs, design and calculation — CEN (2013)

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.