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Cobalt-Chrome Alloy L605 vs S-816

Cobalt-Chrome Alloy · grade comparison

Cobalt-Chrome Alloy L605 and S-816 are both cobalt-chrome alloy grades. Both yield at about 460 MPa — strength does not separate them. L605 is the more ductile: elongation 58% versus 18% for S-816, and S-816 is harder (300 HB vs 240 HB). S-816 is lighter (8.68 g/cm³ vs 9.13 g/cm³ for L605) and L605 is stiffer (225 GPa vs 200 GPa). On the shop floor, L605 welds better (very good vs poor) and S-816 sits in a lower cost tier (high, $$$$) than L605 (specialty, $$$$$).

L605Choose it when the part is bent, formed or impact-loaded, or when the part sees heat.

S-816Choose it when weight is the constraint, or when cost is the deciding factor.

L605 vs S-816: properties

L605S-816

Mechanical

Strength, stiffness, ductility and hardness at room temperature.

Elastic (Young's) Modulus

225 GPa32.6 Msi
200 GPa29 Msi

Shear Modulus

87 GPa12.6 Msi
77 GPa11.2 Msi

Bulk Modulus

178 GPa25.8 Msi
172 GPa24.9 Msi

Poisson's Ratio

0.29
0.3

Tensile Strength (Ultimate)

1,010 MPa146 ksi
1,000 MPa145 ksi

Yield Strength (0.2% offset)

460 MPa66.7 ksi
480 MPa69.6 ksi

Elongation at Break

58%
18%

Reduction in Area

55%
20%

Shear Strength

620 MPa89.9 ksi
640 MPa92.8 ksi

Fatigue Strength (Endurance Limit)

440 MPa63.8 ksi
290 MPa42.1 ksi

Charpy V-Notch Impact (RT)

90 J66.4 ft·lbf
22 J16.2 ft·lbf

Hardness, Brinell

240 HB
300 HB

Hardness, Rockwell B

98 HRB
—

Hardness, Vickers

250 HV
315 HV

Hardness, Rockwell C

—
31 HRC

Physical

Density and transition temperatures.

Density

9.13 g/cm³0.33 lb/in³
8.68 g/cm³0.31 lb/in³

Melting Point (Solidus)

1,329°C2,424 °F
1,330°C2,426 °F

Liquidus Temperature

1,410°C2,570 °F
1,400°C2,552 °F

Thermal

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

Thermal Conductivity

9.4 W/m·K5.4 BTU/hr·ft·°F
12.5 W/m·K7.2 BTU/hr·ft·°F

Specific Heat Capacity

385 J/kg·K0.09 BTU/lb·°F
420 J/kg·K0.1 BTU/lb·°F

Thermal Expansion (CTE, 20–100 °C)

12.3 µm/m·K6.8 µin/in·°F
13.9 µm/m·K7.7 µin/in·°F

Max Service Temperature (continuous)

980°C1,796 °F
870°C1,598 °F

Same in both: Latent Heat of Fusion 270 J/g116 BTU/lb · Min Service Temperature -196°C-321 °F

Electrical

Conductivity and insulation.

Electrical Resistivity

8.9×10⁻⁷ Ω·m35 µΩ·in
9.1×10⁻⁷ Ω·m35.8 µΩ·in

Same in both: Electrical Conductivity 1.9 % IACS

Chemical & Environmental

Corrosion and environmental resistance (0–100 scores).

Galvanic Potential (seawater, vs SCE)

-0.25 V
-0.15 V

Corrosion Resistance

82 / 100
74 / 100

Manufacturability

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

Machinability

18 / 100
13 / 100

Machinability Rating (AISI 1212 = 100 %)

12%
10%

Weldability

72 / 100
25 / 100

Formability (cold)

60 / 100
15 / 100

Castability

55 / 100
68 / 100

Brazeability / Solderability

70 / 100
55 / 100

Polishability

80 / 100
65 / 100

Sustainability

Primary-production footprint per kilogram.

Embodied Energy (primary production)

250 MJ/kg107,481 BTU/lb
190 MJ/kg81,685 BTU/lb

Embodied Carbon (primary production)

19 kg CO₂/kg
13 kg CO₂/kg

Embodied Water

500 L/kg59.9 gal/lb
340 L/kg40.7 gal/lb

Same in both: Typical Recycled Content 30%

Common Calculations

Ratios derived from the values above.

Specific Strength (UTS / density)

111 kN·m/kg
115 kN·m/kg

Specific Stiffness (E / density)

24.6 MN·m/kg
23 MN·m/kg

Modulus of Resilience

470 kJ/m³
576 kJ/m³

Thermal Diffusivity

2.7 mm²/s
3.4 mm²/s

Thermal Shock Resistance Index

3
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 scaleL605S-816

Manufacturing and finishing

CapabilityL605S-816
CNC machiningYes—
Default conditionSolution Annealed—
Relative cost$$$$$ Specialty$$$$ High
Min. machined wall——
Best machined surface——
ElectropolishingYes—
Passivation (Stainless Steel)Yes—

L605 vs S-816 — frequently asked

What is the difference between L605 and S-816?

Cobalt-Chrome Alloy L605 and S-816 are both cobalt-chrome alloy grades. Both yield at about 460 MPa — strength does not separate them. L605 is the more ductile: elongation 58% versus 18% for S-816, and S-816 is harder (300 HB vs 240 HB).

Which is cheaper, L605 or S-816?

S-816 is the lower-cost material: it sits in the high tier ($$$$) while L605 is specialty ($$$$$). Part price depends far more on geometry, tolerance and quantity than on raw stock — upload a CAD file for a live quote.

Which is easier to machine, L605 or S-816?

L605. Its machinability rates poor (18/100) against not recommended (13/100) for S-816; for welding the order is L605 first (very good, 72/100) then S-816 (poor, 25/100).

Ready to make it?

Upload a CAD file and FabDigit prices the part in L605 and S-816 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.