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Type Metal Powder
Material Nickel-Chromium Alloy
Density ≥8.18 g/cm3
Tensile Strength ≥1060 Mpa
Yield Strength ≥720 Mpa
Elongation at Break ≥21 %
Vickers Hardness ≥280 HV5/15
Hardness (Rockwell C Scale) 280-320
Thermal Conductivity 9.3W/mK - 11.5W/mK
Surface Roughness Ra 5 μm-10 μm
Surface Roughness Rz 10 μm-15 μm
Post Processing
Tensile Strength ≥1400 Mpa
Yield Strength ≥1120 Mpa
Elongation at Break ≥12 %
Vickers Hardness ≥410 HV5/15
Hardness (Rockwell C Scale) 400-460
Surface Roughness Ra (sintered) <2 μm
Surface Roughness Rz (sintered) <2μm

SLM Nickel Based Alloy In 718

  • Excellent high-temperature resistance – Usable up to approx. 700 °C

  • High strength & creep resistance – Maintains performance under continuous load

  • Very good corrosion & oxidation resistance – Suitable for aggressive environments

  • Outstanding dimensional accuracy in SLM process – Ideal for complex, precise geometries

  • Excellent weldability and heat treatment properties

  • Durable and reliable – Designed for safety-critical applications

Inconel 718 is a high-performance nickel-chromium alloy known for exceptional strength and corrosion resistance at extreme temperatures. It is ideally suited for applications requiring high mechanical durability under thermal stress. Its outstanding mechanical properties are maintained during continuous operation above 600 °C — a critical advantage for turbine components, engine parts, and high-pressure systems.

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Advantages:

  • Long-term high-temperature resistance

  • Excellent corrosion resistance

  • Very high mechanical strength

  • Low thermal expansion

Typical applications:

  • Engine parts and exhaust systems

  • Turbine blades and housings

  • High-pressure seals and valves

  • Structural components in aerospace and motorsport