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Cobalt-Chrome Alloy F75 vs Haynes 188

Cobalt-Chrome Alloy · grade comparison

Cobalt-Chrome Alloy F75 and Haynes 188 are both cobalt-chrome alloy grades. F75 is the stronger of the two: yield strength 510 MPa (74 ksi) against 464 MPa (67.3 ksi) for Haynes 188, about 10% more. In exchange, Haynes 188 is the more ductile: elongation 53% versus 10% for F75, and F75 is harder (300 HB vs 215 HB). F75 is lighter (8.3 g/cm³ vs 8.98 g/cm³ for Haynes 188) and Haynes 188 is stiffer (232 GPa vs 220 GPa). On the shop floor, Haynes 188 welds better (very good vs poor) and F75 sits in a lower cost tier (premium, $$$) than Haynes 188 (high, $$$$).

F75Choose it when strength drives the design, or when weight is the constraint.

Haynes 188Choose it when the part is bent, formed or impact-loaded, or when the part sees heat.

F75 vs Haynes 188: properties

F75Haynes 188

Mechanical

Strength, stiffness, ductility and hardness at room temperature.

Elastic (Young's) Modulus

220 GPa31.9 Msi
232 GPa33.6 Msi

Shear Modulus

85 GPa12.3 Msi
89 GPa12.9 Msi

Bulk Modulus

183 GPa26.5 Msi
193 GPa28 Msi

Tensile Strength (Ultimate)

720 MPa104 ksi
960 MPa139 ksi

Yield Strength (0.2% offset)

510 MPa74 ksi
464 MPa67.3 ksi

Elongation at Break

10%
53%

Reduction in Area

12%
50%

Compressive Strength

1,500 MPa218 ksi
—

Shear Strength

500 MPa72.5 ksi
620 MPa89.9 ksi

Fatigue Strength (Endurance Limit)

250 MPa36.3 ksi
380 MPa55.1 ksi

Fracture Toughness (K_IC)

50 MPa·√m45.5 ksi·√in
—

Charpy V-Notch Impact (RT)

20 J14.8 ft·lbf
110 J81.1 ft·lbf

Hardness, Brinell

300 HB
215 HB

Hardness, Rockwell C

30 HRC
—

Hardness, Vickers

320 HV
225 HV

Hardness, Rockwell B

—
95 HRB

Same in both: Poisson's Ratio 0.3

Physical

Density and transition temperatures.

Density

8.3 g/cm³0.3 lb/in³
8.98 g/cm³0.32 lb/in³

Melting Point (Solidus)

1,330°C2,426 °F
1,302°C2,376 °F

Liquidus Temperature

1,410°C2,570 °F
1,330°C2,426 °F

Thermal

How each material carries heat and how hot it can run.

Thermal Conductivity

14 W/m·K8.1 BTU/hr·ft·°F
10.8 W/m·K6.2 BTU/hr·ft·°F

Specific Heat Capacity

450 J/kg·K0.11 BTU/lb·°F
403 J/kg·K0.1 BTU/lb·°F

Thermal Expansion (CTE, 20–100 °C)

13 µm/m·K7.2 µin/in·°F
11.9 µm/m·K6.6 µin/in·°F

Latent Heat of Fusion

270 J/g116 BTU/lb
—

Max Service Temperature (continuous)

600°C1,112 °F
1,095°C2,003 °F

Same in both: Min Service Temperature -196°C-321 °F

Electrical

Conductivity and insulation.

Electrical Conductivity

1.9 % IACS
1.7 % IACS

Electrical Resistivity

9.1×10⁻⁷ Ω·m35.8 µΩ·in
1.01×10⁻⁶ Ω·m39.8 µΩ·in

Chemical & Environmental

Corrosion and environmental resistance (0–100 scores).

Galvanic Potential (seawater, vs SCE)

-0.3 V
-0.15 V

Corrosion Resistance

87 / 100
78 / 100

Manufacturability

FabDigit workshop ratings (0–100 scores) — how each material behaves on the machine.

Machinability

12 / 100
15 / 100

Machinability Rating (AISI 1212 = 100 %)

10%
12%

Weldability

25 / 100
75 / 100

Formability (cold)

10 / 100
65 / 100

Castability

78 / 100
35 / 100

Brazeability / Solderability

45 / 100
60 / 100

Polishability

88 / 100
70 / 100

Sustainability

Primary-production footprint per kilogram.

Embodied Energy (primary production)

150 MJ/kg64,488 BTU/lb
280 MJ/kg120,378 BTU/lb

Embodied Carbon (primary production)

11 kg CO₂/kg
19 kg CO₂/kg

Embodied Water

400 L/kg47.9 gal/lb
500 L/kg59.9 gal/lb

Typical Recycled Content

25%
30%

Common Calculations

Ratios derived from the values above.

Specific Strength (UTS / density)

87 kN·m/kg
107 kN·m/kg

Specific Stiffness (E / density)

26.5 MN·m/kg
25.8 MN·m/kg

Modulus of Resilience

591 kJ/m³
464 kJ/m³

Thermal Diffusivity

3.7 mm²/s
3 mm²/s

Same in both: Thermal Shock Resistance Index 4

Strength versus weight

Yield strength against density for every cobalt-chrome alloy grade in the FabDigit library; the compared grades are highlighted. Up and left is stronger for its weight.

5007001,0001,5002,0008.28.48.68.89Density (g/cm³)Yield strength (MPa) — log scaleF75Haynes 188

Manufacturing and finishing

CapabilityF75Haynes 188
CNC machiningYes—
3D printingYes—
Default conditionAs Cast—
Relative cost$$$ Premium$$$$ High
Min. machined wall——
Best machined surface——
ElectropolishingYes—
Passivation (Stainless Steel)Yes—

F75 vs Haynes 188 — frequently asked

Is F75 stronger than Haynes 188?

Yes. F75 has a typical yield strength of 510 MPa (74 ksi) against 464 MPa (67.3 ksi) for Haynes 188 — about 10% more. Tensile strength is 720 MPa (104 ksi) vs 960 MPa (139 ksi).

Which is cheaper, F75 or Haynes 188?

F75 is the lower-cost material: it sits in the premium tier ($$$) while Haynes 188 is high ($$$$). Part price depends far more on geometry, tolerance and quantity than on raw stock — upload a CAD file for a live quote.

Which welds better, F75 or Haynes 188?

Haynes 188. Its weldability rates very good (75/100) against poor (25/100) for F75.

Ready to make it?

Upload a CAD file and FabDigit prices the part in F75 and Haynes 188 side by side — material, machining time, tolerance and finish in one quote. Certified material data ships with the order on request.

Typical handbook values for the conditions named above, normalised for comparison. Hardness on non-Brinell scales is converted approximately for charting only. Request certified data with your order for design-critical properties.