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Steel GCr15SiMn QT-S1

Heat-treated state

EN 100CrMn6

QT-S1 = q&T stabilized S1

Pick the ~250 °C stabilizing temper for bearings running to about 200 °C where dimensional stability outranks hardness; 57 HRC reduces hardness and fatigue life.

Budget cost $

Values for the QT-S1 condition

Other GCr15SiMn tempers and conditions

GCr15SiMn is listed in 9 conditions; see the grade overview at GCr15SiMn.

Compare all 9 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
ADefault
Solution annealed
Order the standard supply condition — fine spheroidal carbides at 195 HB — for turning, cold extrusion and as preparation for final hardening.42075022195 HB—
Normalized
Normalize after forging to break up carbide networks and refine grain at 300 HB; treat it as a pre-treatment before spheroidize annealing, not a machining condition.5609801231 HRC7.5 % IACS
Hot rolled
Take the as-rolled or as-forged blank only as raw stock; hardness reaches 330 HB and is uneven, so spheroidize annealing is required before machining.6201,0501035 HRC7.5 % IACS
Cold drawn
Choose annealed-then-cold-drawn bar for close size and good surface when machining small roller and pin blanks directly, accepting 240 HB and low formability.7008801022 HRC7.5 % IACS
QT-S1This page
Q&T stabilized S1
Pick the ~250 °C stabilizing temper for bearings running to about 200 °C where dimensional stability outranks hardness; 57 HRC reduces hardness and fatigue life.1,7502,000357 HRC6 % IACS
Q&T 61-64 HRC
Specify the standard finished-bearing route — oil quench from 820–840 °C plus 150–180 °C temper — for peak 62 HRC and contact fatigue life in rings and rollers up to 120 °C.1,9002,300162 HRC36 W/m·K
Martempered () + temper, 60-63 HRC
Choose salt-bath martempering plus tempering for thin-wall, large-diameter rings where distortion and quench cracking must be limited, with 61 HRC close to direct quenching.1,9502,250161 HRC5.6 % IACS
Q&T 58-61 HRC
Use the higher 200–230 °C temper on large or heavily loaded rings, trading a little hardness (59 HRC) for toughness and dimensional stability up to 150 °C.—2,150—59 HRC—
Austempered to lower bainite, 58-62 HRC
Austemper to lower bainite at 58–62 HRC when impact, contaminated lubrication or high compressive surface stress govern — rolling mill, railway and shock-loaded bearings.—2,200—60 HRC—

What is GCr15SiMn QT-S1?

GCr15SiMn QT-S1 is GCr15SiMn heat treated to QT-S1 — pick the ~250 °C stabilizing temper for bearings running to about 200 °C where dimensional stability outranks hardness; 57 HRC reduces hardness and fatigue life. GCr15SiMn QT-S1 has a yield strength of 1,750 MPa (254 ksi) and a tensile strength of 2,000 MPa (290 ksi) — stronger than 99% of steel grades. Elongation at break is 3% and the elastic modulus is 208 GPa (30.2 Msi). GCr15SiMn QT-S1 has a density of 7.81 g/cm³ (0.282 lb/in³), lighter than 84% of steel grades. It melts at 1,420°C (2,588 °F). A is the default condition FabDigit quotes; QT-S1 is available on request or by drawing note.

Advantages

  • Polishes to a fine finish — 88/100, better than 100% of steel grades
  • High strength — 1,750 MPa (254 ksi), better than 99% of steel grades

Limitations

  • Difficult to weld — 3/100, worse than 100% of steel grades
  • Limited ductility — 3%, worse than 99% of steel grades
  • Limited formability — 3/100, worse than 99% of steel grades
  • Low fracture toughness — 23 MPa·√m (20.9 ksi·√in), worse than 98% of steel grades
  • Difficult to machine — 13/100, worse than 98% of steel grades

GCr15SiMn QT-S1 properties

Typical room-temperature values for GCr15SiMn QT-S1; 22 are specific to this condition. Other listed values are GCr15SiMn reference data and may not represent this condition. Bars are the position among steel grades.

Physical3

GCr15SiMn QT-S1 has a density of 7.81 g/cm³ (0.282 lb/in³), lighter than 84% of steel grades. It melts at 1,420°C (2,588 °F).

Density7.81 g/cm³0.28 lb/in³
Melting Point (Solidus)1,420°C2,588 °F
Liquidus Temperature1,470°C2,678 °F

Mechanical16

GCr15SiMn QT-S1 has a yield strength of 1,750 MPa (254 ksi) and a tensile strength of 2,000 MPa (290 ksi) — stronger than 99% of steel grades. Elongation at break is 3% and the elastic modulus is 208 GPa (30.2 Msi).

Elastic (Young's) Modulus208 GPa30.2 Msi
Shear Modulus80 GPa11.6 Msi
Bulk Modulus160 GPa23.2 Msi
Poisson's Ratio0.3
Tensile Strength (Ultimate)2,000 MPa290 ksi
Yield Strength (0.2% offset)1,750 MPa254 ksi
Elongation at Break3%
Reduction in Area8%
Compressive Strength2,900 MPa421 ksi
Shear Strength1,200 MPa174 ksi
Fatigue Strength (Endurance Limit)690 MPa100 ksi
Fracture Toughness (K_IC)23 MPa·√m20.9 ksi·√in
Charpy V-Notch Impact (RT)10 J7.4 ft·lbf
Hardness, Brinell600 HB
Hardness, Rockwell B92 HRB
Hardness, Vickers620 HV

Thermal6

GCr15SiMn QT-S1 is rated for continuous service to 200°C (392 °F). It conducts heat at 36 W/m·K (20.8 BTU/hr·ft·°F), worse than 73% of steel grades. Thermal expansion is 12 µm/m·K (6.67 µin/in·°F).

Thermal Conductivity36 W/m·K20.8 BTU/hr·ft·°F
Specific Heat Capacity460 J/kg·K0.11 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)12 µm/m·K6.7 µin/in·°F
Latent Heat of Fusion270 J/g116 BTU/lb
Max Service Temperature (continuous)200°C392 °F
Min Service Temperature-40°C-40 °F

Electrical3

GCr15SiMn QT-S1 conducts electricity at 6 % IACS, worse than 78% of steel grades.

Electrical Conductivity6 % IACS
Electrical Resistivity2.9×10⁻⁷ Ω·m11.4 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 Summary—

Sustainability4

Producing a kilogram of GCr15SiMn QT-S1 takes about 32 MJ of energy and emits 2.3 kg of CO₂ — more than 70% of steel grades. Typical recycled content is 25%.

Embodied Energy (primary production)32 MJ/kg13,758 BTU/lb
Embodied Carbon (primary production)2.3 kg CO₂/kg
Embodied Water55 L/kg6.6 gal/lb
Typical Recycled Content25%

Manufacturability7

GCr15SiMn QT-S1's machinability is not recommended (13/100, worse than 98% of steel grades); weldability not recommended (3/100); formability not recommended (3/100).

MachinabilityNot recommended13/100
Machinability Rating (AISI 1212 = 100 %)8%
WeldabilityNot recommended3/100
Formability (cold)Not recommended3/100
Brazeability / SolderabilityFair40/100
PolishabilityExcellent88/100
Anodizing Response—

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

Working with GCr15SiMn QT-S1

Is GCr15SiMn easy to machine?

Turn, mill and drill only in the spheroidise-annealed condition (≤229 HB); after hardening restrict work to grinding, CBN hard turning or EDM, and flood-cool grinding to prevent burn and grinding cracks.

Can GCr15SiMn be welded?

With about 1 % C the weldability is very poor and welding should be avoided in principle; if repair is unavoidable, preheat 300–400 °C, use low-hydrogen or nickel-based filler and temper immediately.

Can GCr15SiMn be formed, bent or molded?

In the annealed condition it takes warm upsetting, ring rolling and cold extrusion into raceway blanks; forge at about 1050–1120 °C, finish no lower than 850 °C, then slow-cool plus normalise/spheroidise anneal to break up carbide networks.

What surface finishes work on GCr15SiMn?

Cannot be anodised. Raceways are precision ground and superfinished to a mirror surface, while non-working surfaces are usually black oxided, phosphated, chrome plated or oiled for storage.

GCr15SiMn 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
C0.95 – 1.051
Siabove GCr15; raises hardenability and temper stability0.45 – 0.750.6
Mnmarkedly increases hardenability0.95 – 1.251.1
Cr1.4 – 1.651.5
Niresidual element≤ 0.3—
Curesidual element; Cu+Ni less than or equal to 0.50≤ 0.25—
Moresidual element≤ 0.1—
P≤ 0.03—
S≤ 0.03—
Ooxygen 12 ppm max (quality/high-grade bearing steel)≤ 0—
Febalance—

GCr15SiMn QT-S1 — frequently asked

What is GCr15SiMn QT-S1 used for?

GCr15SiMn QT-S1 is typically used for large rolling bearings, heavy machinery rollers and rail bearings. In short: higher hardenability than GCr15; heavy-section bearing rings; grind-and-superfinish only.

What is the yield strength of GCr15SiMn QT-S1?

GCr15SiMn QT-S1 has a typical yield strength of 1,750 MPa (254 ksi) and a tensile strength of 2,000 MPa (290 ksi) — stronger than 99% of steel grades. Strength varies by condition: see the 9 listed tempers.

Is GCr15SiMn QT-S1 easy to machine?

Not especially — machinability is rated not recommended (13/100, worse than 98% of steel grades). Turn, mill and drill only in the spheroidise-annealed condition (≤229 HB); after hardening restrict work to grinding, CBN hard turning or EDM, and flood-cool grinding to prevent burn and grinding cracks.

Can GCr15SiMn QT-S1 be welded?

Not readily — weldability is rated not recommended (3/100). With about 1 % C the weldability is very poor and welding should be avoided in principle; if repair is unavoidable, preheat 300–400 °C, use low-hydrogen or nickel-based filler and temper immediately.

What surface finishes work on GCr15SiMn QT-S1?

Cannot be anodised. Raceways are precision ground and superfinished to a mirror surface, while non-working surfaces are usually black oxided, phosphated, chrome plated or oiled for storage.

Can GCr15SiMn QT-S1 be formed, bent or molded?

In the annealed condition it takes warm upsetting, ring rolling and cold extrusion into raceway blanks; forge at about 1050–1120 °C, finish no lower than 850 °C, then slow-cool plus normalise/spheroidise anneal to break up carbide networks.

What is the maximum service temperature of GCr15SiMn QT-S1?

GCr15SiMn QT-S1 is rated for continuous use to about 200°C (392 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between GCr15SiMn-A and GCr15SiMn-MQ?

A is the default condition — order the standard supply condition — fine spheroidal carbides at 195 HB — for turning, cold extrusion and as preparation for final hardening. MQ: choose salt-bath martempering plus tempering for thin-wall, large-diameter rings where distortion and quench cracking must be limited, with 61 HRC close to direct quenching. Yield strength is 420 MPa in A versus 1,950 MPa in MQ.

Sources

  1. ISO 683-17 / DIN EN ISO 683-17 (100CrMn6, 1.3520) — ISO (2014)
  2. ASM Handbook Vol.1 Properties and Selection: Irons, Steels, and High-Performance Alloys — ASM International (1990)
  3. Bearing steel grades data (100Cr6 / 100CrMn6) heat treatment and properties — Ovako / SKF (2020)

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.