Metal Laser Sintering DMLS/SLM - Zare€¦ · Metal Laser Sintering DMLS/SLM Metal End-Use Parts...

Metal Laser Sintering DMLS/SLM Metal End-Use Parts

TECHNOLOGIES

Technology which allows a direct manufacturing of metallic parts, ready to be tested or used as functional parts. Available metals include Aluminium HTA, Scalmalloy ®, developed by Airbus’ APWorks, Alloy 263, Titanium Ti6Al4v, Cobalt-Chrome (F75 and Remanium Star CL), Aluminium (AlSi7Mg0.6 (A357), AlSi10Mg), Stainless Steel (15-5ph, 17-4 and AISI 316L), Inconel 625 and 718, Copper, Bronze and Silver.

DMLS/SLM offers a remarkable precision and the materials are suitable for post-processings like milling and CNC turning, heat treating and surface treatments, both esthetical and protective.

Metal powders are produced using atomiz-ers designed to off er the best particle sizefor SLM/DLMS production. The production process starts with a 3D fi le specifi cally re-engineered for additive manufacturing. Optimizing the fi le is crucial: it allows us to use the peculiarities of our production plant and materials at their best, to obtain high quality products.

For industrial sectors it’s important to guarantee:•QUICK LEAD TIMES;•HIGH QUALITY;•CONFIDENTIALITY.

Thanks to our 50-year history in the fi eld of precision mechanics we have developed a spe-cial sensitiveness towards what we are manu-facturing: the technology may be diff erent, but the raw material and our accuracy when dealing with DIMENSIONAL TOLERANCES and surface fi nishing haven’t changed.

MATERIALS FOR METAL 3D PRINTING

There are several materials available for metal 3D printing, they off er peculiar me-chanical properties and specifi c response to heat treatment to best suit the intended use of the product.

The materials available include high-per-forming materials like Scalmalloy®, devel-oped by Airbus’ APWorks or Alloy 263, but also widely used alloys such as Titanium, Aluminium, Stainless Steel and Inconel. The technology doesn’t change with the material, what changes is the pre-production process: all the steps we take to obtain the best result possible.

Metal Additive Manufacturing allows to calculate the geometries of the product so to signifi cantly reduce its weight with-out aff ecting its strength. The fi nal product will have the same physical and mechani-cal properties obtained with a traditional manufacturing process, but the fl exibility that characterizes our pre-production pro-cess off ers important advantages, in particu-lar in fi elds such as aeronautics, motor sports, extreme sports, aerospace.

THE AM PRODUCTION FACTORY

Metal Laser Sintering DMLS / SLMMetal End-Use Parts

MATERIALS DESCRIPTION

Scalmalloy® Scalmalloy® powder, produced and distributed by APWorks of the Airbus group, combines the extreme lightness of sintered alu-minium with a specific strength comparable with titanium, thus guaranteeing top performances.

Aluminium HTA Aluminium HTA - High Temperature Aluminium – is a material developed with the objective of ensuring high performance even at 190—200°C.

Alloy 263 Alloy 263 is a nickel-cobalt-chromium-molybdenum alloy designed specifically to combine very good strength properties with excellent fabrication characteristics in the annealed condition; it’s also age hardenable.

Böhler M789 The M789 Böhler material combines the easy printability of a Maranging Steel with the corrosion resistance of a 17-4PH (Stainless Steel AISI630).

Böhler W360 The W360 Böhler material is a hot work tool steel with high hardness, specially developed for use in warm forging applications or for forging dies.

Böhler E185 The E185 Böhler material is a low alloyed steel with easy printability and the possibility for surface treatment like case hardening or nitrinding.

Titanium Ti6Al4V Titanium Ti6Al4v has excellent mechanical properties and corrosion resistance combined with low specific weight and bio-compatibility. Parts built from Titanium Ti64 can be machined, spark-eroded, welded, micro shot-peened, polished and coated if required.

Titanium TA15 This alloy is actually used in various high-tech sectors such as motorsport and aerospace, for the production of highly stressed parts of racing engines, frames and blades for compressors and impellers for turbine

Inconel 718 Inconel 718 is a heat and corrosion resistant nickel alloy. This kind of precipitation-hardening nickel-chromium alloy is character-ized by good tensile, fatigue, creep and rupture strength at temperatures up to 980 °C (1290 °F).

Inconel 625Inconel 625 is characterized by high tensile, creep and rupture strength. Components in this type of nickel alloy have typically excellent fatigue and thermal-fatigue properties combined with good oxidation resistance. It’s the material of choice especially in sea-water applications requiring high pitting and crevice corrosion resistance.

Al Alloys (AlSi7Mg0.6 - A357, AlSi10Mg)

Al-Si Alloys are typical casting Aluminium alloys with good casting properties and it’s typically used for cast parts with thin walls and complex geometry. They offer good strength, hardness and dynamic properties and are therefore also used for parts subject to high loads.

15-5PH Stainless Steel 15-5PH Stainless Steel provides an outstanding combination of high strength, good corrosion resistance, good mechanical prop-erties at temperatures up to 600 °F (316 °C).

17-4PH Stainless Steel 17-4PH Stainless Steel is characterized by good corrosion resistance and mechanical properties, with an excellent ductility in laser processed state.

AlSl316L Stainless SteelAlSl316L Stainless Steel is a corrosion resistant iron based alloy. This material is ideal for lifestyle/consumer products such as watches, jewelry, spectacle frames. Thanks to its corrosion resistance properties it’s an entry level for the DMLS / SLM technolo-gies.

Maraging SteelMaraging Steel has very good mechanical properties and can be easily heat-treated using a simple thermal age-hardening process to obtain excellent hardness and strength. The parts are easily machinable after the building process and can be post-hardened to more then 50 HRC by age-hardening at 490 °C (914 °F) for 6 hours.

Cobalt-Chrome (F75, Remanium Star CL)

Cobalt-Chrome is a superalloy with excellent mechanical properties commonly used in biomedical applications (i.e. medical implants) and also for high-temperature engineering applications.

Copper Alloy CuNi2SiCrCuNi2SiCr is a copper alloy combining electrical and thermal conductivity with high stiffness, also at elevated temperatures. Fur-thermore, CuNi2SiCr-alloy is very well suited for highly thermally-stressed construction elements and for the use of a beryllium-free copper alloy.

BronzeThe Bronze alloy is a material whose melting properties make it outstandingly suited for additive manufacturing. It can be used for the production of original or master models in the fields of jewelry and artistically crafted sculptures. The material is very easy to polish and has a higher hardness than silver alloy.

NickelAlloy HXNickelAlloy HX is a nickel-chromium-iron-molybdenum alloy in fine powder form. This type of alloy is characterized by high strength and oxidation resistance also at elevated temperatures and is often used up to 1200°C. Therefore, its applications can be found in aero-space technology, Oil & Gas and gas turbine parts.

Alloy 282Alloy 282 is a superalloy suitable for the aerospace and Oil & Gas industries developed for use in critical applications ,at temperatures close to 1000 ° C , like turbine parts and exhausts. The piece obtained can be subjected to heat treatment to improve the mechanical and fatigue characteristics at high temperatures.

AISI 420AISI 420 is a self-hardening martensitic steel which has complementary characteristics to ferritic and austenitic steels. The hard-ening process to which it is subjected makes it very useful for cutlery, structural parts, surgical and dental instruments, parts of valves, crankshafts.

Tungsten Tungsten is a material with high wear resistance used for the production of tools for the metalworking, mining, petroleum and construction industries. Tungsten is radiation-resistant and is widely used for aerospace applications.

Other Materials Corrax Stainless SteelSilver (925 and 750)


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MATERIALS

Mechanical PropertiesTest Method As Built Heat Treated

Tensile Strength ISO 6892-1:2009(B) Annex D 393 ± 1 MPa 433 ± 1 MPa

Yield Strength (Rp 0.2%) ISO 6892-1:2009(B) Annex D 336 ± 3 MPa 361 ± 21 MPa

Elongation at Break ISO 6892-1:2009(B) Annex D 15 ± 2% 12 ± 13%

Young’s Modulus - - - - - - - - - 76 ± 2 GPa 85 ± 4 GPa

Hardness DIN EN ISO 6506-1 108 ± 2 HBW 130 ± 2 HBW

Thermal PropertiesThermal conductivity ASTM E1461-13 - - - - - - - - - 120 W/m°C

Specific heat capacity ASTM E1461-13 - - - - - - - - 880 ± 50 J/Kg°C

Aluminium HTA – High Temperature Aluminium – is a material developed with the objective of ensuring high performance even at elevated temperatures. Aluminium HTA belongs to the Aluminium-Copper system and its excellent mechanical properties remain unchanged even at temperatures of 190-200°C

Objects made via Additive Manufacturing using Aluminium HTA can have ultra-thin walls, with a thickness of as little as 1/1,5mm.

Material Data Sheet

DMLS/SLM technology

Aluminium HTA

Physical PropertiesRelative Density Approx. 99,8 %

Density 2,85 g/cm3

Mechanical Properties - Tested at 150°CTest Method As Built Heat Treated

Tensile Strength ISO 6892-2 - - - - - - - - - 371 ± 2 MPa

Yield Strength (Rp 0.2%) ISO 6892-2 - - - - - - - - - 336 ± 21 MPa

Elongation at Break ISO 6892-2 - - - - - - - - - 20 ± 3%

Young’s Modulus - - - - - - - - - - - - - - - - - - 70 ± 1 GPa


Tensile Strength ISO 6892-1:2009(B)Annex D 900 ± 40 MPa 1100 ± 30 MPa

Yield Strength (Rp 0.2%) ISO 6892-1:2009(B)Annex D 650 ± 40 MPa 800 ± 30 MPa

Elongation at Break ISO 6892-1:2009(B)Annex D 40 ± 5% 35 ± 5%


Chemical CompositionNi Balance

Cr 19,2 %

Co 19,4 %

Mo 5,8 %

Ti 2,1 %

Al 0,4 %

Mn ≤ 0,1 %

Fe ≤ 0,06 %

C ≤ 0,04 %

Si ≤ 0,02 %

P ≤ 0,01 %

Alloy 263 is a nickel-cobalt-chromium-molybdenum alloy designed specifi cally to combine very good strength propertieswith excellent fabrication characteristics in the annealed condition. The alloy is also age hardenable. While its strength at elevated temperatures is not quite as high as materials such as Waspaloy or alloy R-41, it is far easier to form and weld. Alloy 263 exhibits excellent intermediate temperature tensile ductility, and is not normally subject to strain age cracking problems common for gamma prime strengthened alloys.

Typical Applications: gas turbine components heat treat equipment, high temperature / high strength applications.

Material Data Sheet

DMLS/SLM technology

Alloy 263


Density 8,36 g/cm3

Heat TreatmentSolution Annealing Precipitation Hardening

Temperature Time Temperature Time

RT - 1150°C - RT - 800°C -

1150°C 2h 800°C 8h

1150°C - RT - RT - 800°C -


Yield Modulus EN ISO 6892-1 175-185 GPa 185-195 GPa

Yield Strength EN ISO 6892-1 700-800 MPa 1390-1710 MPa

Tensile strength EN ISO 6892-1 1000-1040 MPa 1570-1800 MPa

Elongation at Break EN ISO 6892-1 7-14 % 2-6 %

Charpy V-notch test EN ISO 148-1 - 6-14 J

Hardness EN ISO 6508-1 20-30 HRC 52-58 HRC

The M789 – Precipitation Hardenable Stainless Steel – Böhler material combines the easy printability of Maraging Steel with the corrosion resistance of a 17-4PH (Stainless Steel AISI630).

The M789 reaches high tensile strength (up to 1800 MPa) and hardness values (up to 52HRC) after heat treatment, which makes usable for structural components that usually where made using high performance structural steels, such as AISI 4340 and Maraging M300. Furthermore, the M789 steel is a corrosion resistance steel rather than other high performance structural steels, hence it is possible to avoid to use galvanic coatings (e.g. cadmium and chromium, VI and III).

These properties allow to use the M789 steel for shafts, brackets, dies, gears and impellers operating in mild to heavy corrosive environments.

Material Data Sheet

DMLS/SLM technology

BÖHLER M789

Chemical CompositionC <0,02 %

Cr 12,2 %

Ni 10 %

Mo 1 %

Al 0,6 %

Ti 1 %

Physical PropertiesDensity 7,85 g/cm3


Yield Modulus EN ISO 6892-1 - 185-195 GPa*

Yield Strength EN ISO 6892-1 - 1450-1650 MPa*

Tensile strength EN ISO 6892-1 - 1859-1950 MPa

Elongation at Break EN ISO 6892-1 - 5-8 %

Charpy V-notch test EN ISO 148-1 - 8-14 J

Hardness EN ISO 6508-1 51-59 HRC* depending on HT parameters

Hot Work Tool Steel Böhler W360 has all the characteristics necessary for the production of components used for hot work such as: high thermal conductivity (comparable to that of cast iron), good wear resistance and compressive strength, possibility of being heat treated in vacuum, hardness between 42 - 60 HRC and good weldability, a particularly useful feature in case of restoration and regeneration of existing products.

Compared with the classic H11/H13/1.2367 hot work steels, the Böhler W360 has decidedly superior performance, making it particularly suitable for the production of moulds and inserts for the following machining: gravity casting and die casting, open and closed die forging, hot forming (direct and indirect), blanking, blowing and moulding of glass, stamping and blanking.

Finally, thanks to its properties, Böhler W360 steel can be used for the manufacture of nozzles, extractors and inserts in the moulding of filled (up to 60% vol of fibreglass) and unloaded polymers and high-tech polymers.

Material Data Sheet

DMLS/SLM technology

BÖHLER W360


Si 0,2 %

Mn 0,25 %

Cr 4,5 %

Mo 3,0 %

V 0,55 %

Physical PropertiesDensity 7,85 g/cm3

Mechanical PropertiesTest Method As Built Heat Treated*

Yield Modulus EN ISO 6892-1 180-190 GPa 180-190 GPa

Yield Strength EN ISO 6892-1 900-1050 MPa 1080-1200 MPa

Tensile strength EN ISO 6892-1 950-1150 MPa 1300-1400 MPa

Elongation at Break EN ISO 6892-1 9-15 % 7-13 %

Charpy V-notch test EN ISO 148-1 120-150 J 70-90 J

Hardness EN ISO 6508-1 35-42 HRC 40-50 HRC

* depending on HT parameters

The low alloy Böhler E185 steel is designed for components to be used in particularly demanding sectors such as motorsport, automotive, earthmoving machinery and precision mechanics.The low carbon content facilitates moulding and can be used for both fi nal elements and prototypes.

Thanks to its chemical composition, it is also the fi rst steel specifi cally designed for the production of 3D printing components that undergo classic thermochemical treatments, such as case hardening, nitriding and carbonitriding.Böhler E185 is therefore the ideal material for the production, by means of 3D printing with metals, of components for transmission parts such as gears, pinions, pins, crowns, shafts, synchronisers and bevel gears.

Material Data Sheet

DMLS/SLM technology

BÖHLER E185


Si 0,22 %

Mn 0,3 %

Cr 0,95 %

Ni 1,25 %

Mo 0,2 %

Case HardnessSurface Hardness 720-770 HV30

Case Hardening Depth 0.8-0.9 mm

Mechanical PropertiesTest Method As Built Annealing

Tensile Strength ASTM E8 1200 ± 40 MPa 1059 ± 43 MPa

Proof Stress (Rp0.2) ASTM E8 1013 ± 55 MPa 973 ± 68 MPa

Elongation at Break ASTM E8 8 ± 2% 10 ± 2%

Young’s Modulus ASTM E8 113 ± 8 GPa 115 ± 5 GPa

Hardness ISO 6508-1 46 ± 3 HRC 45 ± 3 HRC

Chemical CompositionTi Balance

Al 5,5 - 6,75%

V 3,5 - 4,5%

O ≤ 0,13%

N ≤ 0,05%

C ≤ 0,08%

H ≤ 0,012%

Fe ≤ 0,25%

Titanium grade 23 (Ti6Al4V ELI) has excellent properties: ELI is an acronym for Extra Low Interstitial, indicating that this alloy has a very low amount of interstitial elements (carbon, oxygen, nitrogen, hydrogen). The interstitial elements are inserted in the crystalline lattice of the material making the structure more fragile and reducing elongation at break; however, they also result in an increase in the mechanical properties, for this reason, it is preferable to vary the amount according to the alloy’s intended use.

If an extremely ductile and tough material is required, the interstitial elements should be reduced as much as possible, just as it was done for grade 23 titanium which contains 6% aluminium, 4% vanadium, 0.13% (maximum) of oxygen and the rest titanium. Also, grade 23 titanium has better ductility than grade 5.

Material Data Sheet

DMLS/SLM technology

Titanium Ti6Al4V ELI

Heat TreatmentAnnealing

Temperature Time Atmosphere

RT -> 840°C 4h Inert/Vacuum

840°C 2h Inert/Vacuum

840°C -> RT - - - - - - - - - Inert


Density 4,41 g/cm3

Mechanical PropertiesTest Method As Built

Tensile Strength (Rm) ASTM E8 1358 ± 34 MPa

Yield strength (Rp0.2) ASTM E8 1186 ± 27 MPa

Elongation at Break ASTM E8 4 ± 1%

Young’s Modulus ASTM E8 110 ± 7 GPa

Hardness ASTM E92 385 ± 4 HV10

Chemical CompositionTi Balance

Al 5,5 - 7,1%

Zr 1,5 - 2,5%

Mo 0,5 - 2,0%

V ≤ 2,5%

Si ≤ 0,15%

C ≤ 0,008%

Fe ≤ 0,25%

O ≤ 0,15%

N ≤ 0,05%

H ≤ 0,015%

Others ≤ 0,1%

Total Others ≤ 0,3%

When the excellent mechanical properties of grades 5 and 23 are not enough, there is the alloy TA 15. This alloy is formed with aluminium and vanadium, like grades 5 and 23, but also with other elements such as zirconium and molybdenum, which bestow greater mechanical strength, especially in hot applications.

This alloy is actually used in various high-tech sectors such as motorsport and aerospace, for the production of highly stressed parts of racing engines, frames and blades for compressors and impellers for turbine.

Material Data Sheet

DMLS/SLM technology

Titanium TA 15

Physical PropertiesRelative Density > 99,5 %

Density 4,5 g/cm3


Tensile Strength ISO 6892-1:2009(B) Annex D 980 ± 50 MPa Min. 1250 MPa

Yield Strength (Rp 0.2%) ISO 6892-1:2009(B) Annex D 700 ± 50 MPa Min. 1050 MPa

Elongation at Break ISO 6892-1:2009(B) Annex D 28 ± 3% Min. 10%


Hardness DIN EN ISO 6508-1 Approx. 30 HRC Approx. 45 HRC

Thermal PropertiesMax. Operating Temp. ASTM E1461-13 Approx. 650° C

Oxidation Resistance to ASTM E1461-13 Approx. 980° C

Chemical CompositionNi 50 - 55%

Cr 17 - 21%

Nb 4,75 - 5,50%

Mo 2,80 - 3,30%

Ti 0,65 - 1,15%

Al 0,20 - 0,80%

Co ≤ 1%

Cu ≤ 0,3%

C ≤ 0,08%

Si / Mn ≤ 0,35%

P / S ≤ 0,015%

INCONEL 718 is a heat and corrosion resistant nickel alloy. Parts built from INCONEL 718 have chemical composition corresponding to UNS N07718, AMS 5662, AMS 5664, W.Nr 2.4668, DIN NiCr19Fe19NbMo3. This kind of precipitation-hardening nickel-chromium alloy is characterized by having good tensile, fatigue, creep and rupture strength at temperatures up to 980 °C (1290 °F).

This material is ideal for many high temperature applications such as gas turbine parts, instrumentation parts, power and process industry parts etc. It also has excellent potential for cryogenic applications. Parts built from INCONEL 718 can be easily post-hardened by precipitation-hardening heat treatments. In both as-built and age-hardened states the parts can be machined, sparkeroded, welded, micro shot-peened, polished and coated if required.

Material Data Sheet

DMLS/SLM technology

Inconel 718

Physical ProprietiesRelative Density Approx. 99,99 %

Density 8,15 g/cm3

Heat TreatmentSolution Annealing Precipitation Hardening

Temperature Time Temperature Time

RT - 980°C - RT - 720°C -

980°C 1h 720°C 8h

980°C - RT - 720° C - 620°C 2h

620°C 8h

620°C - RT -






Hardness DIN EN ISO 6508-1 - - - - - - - - - Approx. 30 HRC

Thermal PropertiesMax. Operating Temp. ASTM E1461-13 Approx. 650° C

Oxidation Resistance to ASTM E1461-13 Approx. 980° C

Chemical CompositionNi Balance (> 58%)

Cr 20 - 23%

Mo 8 - 10%

Nb 3,15 - 4,15%

Fe ≤ 5%

Ti ≤ 0,4%

Al ≤ 0,4%

Co ≤ 1%

C ≤ 0,1%

Ta ≤ 0,05%

Si / Mn ≤ 0,5%

INCONEL 625 is a heat and corrosion resistant nickel alloy. Parts built in INCONEL 625 have chemical composition corresponding to UNS N06625, AMS 5666F, AMS 5599G, W.Nr 2.4856, DIN NiCr22Mo9Nb. This type of alloy is characterized by having high tensile, creep and rupture strength. Conventionally cast or wrought components in this type of nickel alloy have typically excellent fatigue and thermal-fatigue properties combined with good oxidation resistance. INCONEL 625 is expected to have good corrosion resistance in various corrosive environments.

Especially sea-water applications require high pitting and crevice corrosion resistance, stress-corrosion resistance against chloride-ions, high tensile and corrosion fatigue strength. Parts built from INCONEL 625 can be heat treated and material properties can be varied within specified range. Parts can be machined, spark-eroded, welded, micro shot-peened, polished and coated in both as-built and in heat treated conditions.

Material Data Sheet

DMLS/SLM technology

Inconel 625


Density 8,4 g/cm3

Heat TreatmentStress Relief


RT - 875°C - - - - - - - - - Inert

875°C 30min Inert

875°C - RT - - - - - - - - - Inert






Hardness DIN EN ISO 6506-1 110 ± 5 HBW - - - - - - - - -

Thermal PropertiesThermal conductivity ASTM E1461-13 120-140 W/m°C 180-190 W/m°C

Specific heat capacity ASTM E1461-13 910 ± 50 J/Kg°C 890 ± 50 J/Kg°C

Chemical CompositionAl Balance

Si 6,5 - 7,5%

Mg 0,5 - 0,7%

Ti 0,1 - 0,18%

Fe ≤ 0,15 %

Zn ≤ 0,07 %

Mn ≤ 0,05 %

Cu ≤ 0,02 %

AlSi7Mg0.6 is a hardenable aluminium-based alloy with a density of about 2,68 g/cm³. It is suitable for thin-walled components and for parts with complex geometries. AlSi7Mg0.6 is highly suitable for processing and displays good corrosion resistance and good tolerance against strain.

The components are optimal for use in areas such as aerospace engineering, the automotive industry and food industry.

Material Data Sheet

DMLS/SLM technology

Aluminium AlSi7Mg0.6


Density 2,67 g/cm3



RT - 300°C 1h Inert

300°C 2h Inert

300°C - RT - - - - - - - - - Inert






Hardness DIN EN ISO 6506-1 120 ± 5 HBW 120 ± 5 HBW

Thermal PropertiesThermal conductivity ASTM E1461-13 110 ± 5 W/m°C 170 ± 5 W/m°C


Chemical CompositionAl Balance

Si 9 - 11%

Fe 0 - 0,055%

Cu 0 - 0,1%

Mn 0 - 0,45 %

Mg 0,20 - 0,45 %

Ni 0 - 0,05 %

Zn 0 - 0,10 %

Pb 0 - 0,05 %

Sn 0 - 0,05 %

Ti 0 - 0,15 %

AlSi10Mg is a typical casting alloy with good casting properties and is typically used for cast parts with thin walls and complex geometry. It offers good strength, hardness and dynamic properties and is therefore also used for parts subject to high loads. Parts in Aluminium AlSi10Mg are ideal for applications which require a combination of good thermal properties and low weight. They can be machined, spark-eroded, welded, micro shot-peened, polished and coated if required. Conventionally cast components in this type of aluminium alloy are often heat treated to improve the mechanical properties, for example using the T6 cycle of solution annealing, quenching and age hardening.

The laser-sintering process is characterized by extremely rapid melting and re-solidification. This produces a metallurgy and corresponding mechanical properties in the as-built condition which is similar to T6 heat-treated cast parts.

Material Data Sheet

DMLS/SLM technology

Aluminium AlSi10Mg




240°C 6h Inert

240°C - RT - - - - - - - - - Inert


Density 2,67 g/cm3





Hardness DIN EN ISO 6506-1 - - - - - - - - - 40 HRC


Max. Operating Temp. ASTM E1461-13 550° C

Chemical CompositionFe Balance

Cr 14,5 - 15%

Ni 4,3 - 4,5%

Cu 3,8 - 4,1%

Mn ≤ 0,1%

Si ≤ 0,5%

Mo ≤ 0,02%

Nb ≤ 0,3%

C 0,02% - 0,03%

15-5 PH Stainless Steel is a martensitic precipitation-hardening stainless steel that provides an outstanding combination of high strength, good corrosion resistance, good mechanical properties at temperatures up to 600 °F (316 °C) and good toughness in both the longitudinal and transverse directions in both base metal and welds.

Material Data Sheet

DMLS/SLM technology

StainlessSteel 15-5PH


Density 7,80 g/cm3

Heat TreatmentSolution Annealing


RT - 1125°C - - - - - - - - - Inert

1125°C - RT Rapid cooling down in water, air or oil Inert

Precipitation Hardening

RT - 525°C - - - - - - - - - Inert

525°C 4h Inert

525°C - RT - - - - - - - - - Inert






Hardness DIN EN ISO 6506-1 20 - 22 HRC 38 - 40 HRC


Max. Operating Temp. ASTM E1461-13 550° C


Cr 15 - 17%

Ni 3 - 5%

Cu 3 - 5%

Mn ≤ 1%

Si ≤ 1%

Mo ≤ 0,5%

Nb 0,15 - 0,45%

C ≤ 0,07%

StainlessSteel 17-4PH is a pre-alloyed stainless steel in fine powder form. Its composition corresponds to US classification 17-4 and European 1.4542. This kind of steel is characterized by having good corrosion resistance and mechanicalproperties, especially excellent ductility in laser processed state, and is widely used in a variety of engineering applications.

This material is ideal for many part-building applications such as functional metal prototypes, small series products, individualised products or spare parts. StainlessSteel 17-4PH can be machined, spark-eroded, welded, micro shot-peened, polished and coated if required. Typical applications: engineering applications including functional prototypes, small series products, individualised products or spare parts; parts requiring high corrosion resistance, sterilisability, etc.; parts requiring particularly high toughness and ductility.

Material Data Sheet

DMLS/SLM technology

StainlessSteel 17-4PH


Density 7,90 g/cm3



RT - 1125°C - - - - - - - - - Inert

1125°C - RT Rapid cooling down in water, air or oil Inert


RT - 480°C - - - - - - - - - Inert

480°C 1h Inert

480°C - RT - - - - - - - - - Inert





Young’s Modulus - - - - - - - - - 167 ± 26 GPa 200 GPa

Hardness DIN EN ISO 6508-1 20 HRC 20 HRC



Cr 17 - 19%

Ni 13 - 15%

Mo 2,25 - 3%

C ≤ 0,03%

Mn ≤ 2%

Cu ≤ 0,5%

P ≤ 0,025%

S ≤ 0,01%

Si ≤ 0,75%

N ≤ 0,1%

StainlessSteel AISI316L is a corrosion resistant iron based alloy. The parts built from StainlessSteel 316L have chemical composition corresponding to ASTM F138 “Standard Specification for Wrought 18Cr-14Ni-2.5Mo Stainless Steel Bar and Wire for Surgical Implants (UNS S31673)”. This kind of stainless steel is characterized having a good corrosion resistanceand evidence that there are no leachable substances in cytotoxic concentrations.

This material is ideal in: - Lifestyle/Consumer (watches, other jewellery, spectacle frames, decorations, functional elements in electronic housing and accessories) - Automotive/Industrial (non-corroding common material, food and chemical plants) - Aerospace/Turbine industry (entry-level material for Laser Sintering Technology, mounting parts, brackets, heat exchangers). Parts built from StainlessSteel 316L can be machined, shot-peened and polished in as-built or stress relieved (AMS2759) states if required. Solution annealing is not necessary because the mechanical properties of as-built state are showing desired values (ASTM A403). Parts are not ideal in temperature range 427°C-816°C where precipitation of chromium carbides occurs.

Material Data Sheet

DMLS/SLM technology

StainlessSteel AISI316L


Density 7,90 g/cm3




550°C 6h Inert

550°C - RT - - - - - - - - - Inert






Hardness DIN EN ISO 6508-1 33 - 37 HRC 50 - 55 HRC

Thermal PropertiesMax. Operating Temp. ASTM E1461-13 Approx. 400 °C


Chemical CompositionFe Balance (> 58%)

Ni 17 - 19%

Co 8,5 - 9,5%

Mo 4,5 - 5,2%

Ti 0,6 - 0,8%

Al 0,05 - 0,15%

Cr / Cu ≤ 0,5%

C ≤ 0,03%

Mn / Si ≤ 0,1%

P / S ≤ 0,01%

Parts built in Maraging Steel have a chemical composition corresponding to US classification 18% Ni Maraging 300, European 1.2709 and German X3NiCoMoTi 18-9-5. This kind of steel is characterized by having very good mechanical properties, and being easily heat-treatable using a simple thermal age-hardening process to obtain excellent hardness and strength. Parts built from Maraging Steel are easily machinable after the building process and can be easily post-hardened to more then 50 HRC by age-hardening at 490 °C (914 °F) for 6 hours.

In both as-built and age-hardened states the parts can be machined, spark-eroded, welded, micro shot-peened, polished and coated if required.

Material Data Sheet

DMLS/SLM technology

Maraging Steel


Density 8,1 g/cm3

Heat TreatmentPrecipitation Hardening


RT - 490°C 5,5h Inert

490°C 6-10h Inert

490°C - RT - - - - - - - - - Inert




Elongation at Break ISO 6892-1:2009(B) Annex D Approx. 15 ± 4% Approx. 15 ± 4%


Hardness DIN EN ISO 6508-1 35 ÷ 40 HRC - - - - - - - - -

Thermal PropertiesThermal conductivity ASTM E1461-13 15 ± 3 W/m°C - - - - - - - - -

Max. Operating Temp. ASTM E1461-13 Approx. 1150°C - - - - - - - - -

Chemical CompositionCo 60 - 65%

Cr 26 - 30%

Mo 5 - 7%

Si ≤ 1%

Mn ≤ 1%

Fe ≤ 0,75%

C ≤ 0,16%

Ni ≤ 0,10%

Parts built from CobaltChrome conform to the chemical composition UNS R31538 of high carbon CoCrMo alloy. They are nickel-free (< 0.1 % nickel content) and are characterized by a fine, uniform crystal grain structure. As built CobaltChrome meets the chemical and mechanical specifications of ISO 5832-4 and ASTM F75 for cast CoCrMo implant alloys, as well as the specifications of ISO 5832-12 and ASTM F1537 for wrought CoCrMo implants alloys except remaining elongation.

The remaining elongation can be increased to fulfil even these standards by high temperature stress relieving or hot isostatic pressing (HIP). Parts made from CobaltChrome can be machined, spark-eroded, welded, micro shotpeened, polished and coated if required. They are suitable for biomedical applications and for parts requiring high mechanical properties in elevated temperatures (500 - 1000 °C) and with good corrosion resistance.

Material Data Sheet

DMLS/SLM technology

CobaltChrome F75


Density 8,30 g/cm3




1150°C 6h inert

1150°C - RT - - - - - - - - - Inert


Tensile Strength ISO 6892-1:2009(B) Annex D 1170 ± 20 MPa 1030 MPa

Yield Strength (Rp 0.2%) ISO 6892-1:2009(B) Annex D 840 ± 20 MPa 635 MPa

Elongation at Break ISO 6892-1:2009(B) Annex D 12 ± 2% 10%

Young’s Modulus - - - - - - - - - 230 GPa 230 GPa

Melting range - - - - - - - - - 1320 - 1420°C 1320 - 1420°C

Thermal PropertiesCoe� icient of thermal expansion TEC (25-500°C) ASTM E1461-13 14,1 x 10-6K-1 - - - - - - - - -

Other PropertiesMetal- ceramic bond strength acc. to EN ISO 9693,3-Pt.- bending test (min. 25 MPa acc. to EN ISO 9693) 40 MPa (Carmen CCS, Dentaurum)

Biocompatibility, L 929-Proliferation acc. toEN ISO 10993-5, -12, ISO 9363-1, LM SOP 4-06-01 No deliberation of cell toxic active substances

Corrosion resistance, static immersion test acc. to EN ISO 10271(max. 200 µg/cm2 x 7d acc. to EN ISO 22674) Ion release 3,5 µg/cm2 x 7d

Chemical CompositionCo 60,5%

Cr 28%

W 9%

Si 1,5%

Other elements <1 %: Mn, N, Nb, Fe. free fromnickel, beryllium and gallium

remanium® star CL is a CoCrW alloy for the production of metallic restaurations by means of the metal laser melting process. remanium® star CL is approved for use on laser melting machines from the company Concept Laser GmbH.

remanium® star CL is particularly suitable for crowns and bridges, frames for metal ceramic veneering, cast partials, primary – and secondary parts for combined restorations.

Material Data Sheet

DMLS/SLM technology

remanium® star CL


Density 8,60 g/cm3



RT - 1150°C 3h Argon

1150°C 1h Argon

1150°C - RT - - - - - - - - - Argon

Mechanical PropertiesTest Method As Built Precipitation Hardering

Tensile Strength DENI EN 10002 Approx. 250 ± 10 MPa Approx. 630 ± 50 MPa

Yield Strength (Rp 0.2%) DENI EN 10002 Approx. 190 ± 10 MPa Approx. 580 ± 50 MPa

Elongation at Break DENI EN 10002 Approx. 34 ± 5% Approx. ~ 10 %

Young’s Modulus - - - - - - - - - Approx. 90 ± 5 GPa Approx. 130 ± 10 GPa

Hardness - - - - - - - - - - - - - - - - - - HB 220

Thermal Properties

Thermal Conductivity 90 W/mK 190 W/mk

Electrical Properties

Electrical Conductivity 8 MS/m 23 MS/m

Chemical CompositionCu Balance

Ni 2 - 2,5 %

Si 0,65 %

Cr 0,45 %

Ti < 0,03 %

Co < 0,02 %

Fe < 0,02 %

CuNi2SiCr is a thermal curable copper alloy. Typical for CuNi2SiCr is a favorable combination of electrical and thermal conductivity accompanied by high stiffness, also at elevated temperatures. This copper alloy features a high corrosion resistance and is very well suited for wear and sliding applications. Furthermore, CuNi2SiCr fulfi lls the requirements of a conductive contact material in electrical engineering and for electrodes in welding.

CuNi2SiCr is used for tooling because of its strong hardness and its high level of wear resistance. Furthermore, CuNi2SiCr-alloy is very well suited for highly thermally-stressed construction elements and for the use of a beryllium-free copper alloy.

Material Data Sheet

DMLS/SLM technology

Copper Alloy CuNi2SiCr

Physical CompositionRelative Density Approx. 99,8 %

Density 8,85 g/cm3

Mechanical PropertiesTest Method As Built

Tensile Strength UNI EN 10002 Approx. 400 ± 20 MPa

Yield Strength (Rp 0.2%) UNI EN 10002 Approx. 500 ± 20 MPa

Elongation at Break UNI EN 10002 Approx. 5 ± 2%

Young’s Modulus - - - - - - - - - Approx. 120 GPa

Hardness HV 0.2 UNI EN 10002 171 ± 7 HBW

Thermal PropertiesThermal conductivity ASTM E1461-13 59 W/m°C

Specific heat capacity ASTM E1461-13 370 J/Kg°C

Chemical CompositionCu 90%

Sn 10 %

The Bronze alloy is a material whose melting properties make it outstandingly suited to generative processing. It is the material of choice for the fabrication of original or master models in the fields of jewellery and artistically crafted sculptures. The material is very easy to polish and has a higher hardness than silver alloy.

Material Data Sheet

DMLS/SLM technology

Bronze


Density 8,80 g/cm³


Tensile strength ISO 6892-1:2009(B) Annex D 820 ± 50 MPa 618 ± 32 MPa


Young’s Modulus ISO 6892-1:2009(B) Annex D 195 ± 20 GPa 211 ± 1 GPa

Elongation at break ISO 6892-1:2009(B) Annex D 27 ± 8% 56 ± 14%

Thermal PropertiesThermal conductivity ASTM E1461-13 9,7 W/m°C 170 ± 5 W/m°C


Chemical CompositionNi 47%

Cr 22%

Fe 18%

Mo 9%

Co 1,5 %

W 0,6 %

C 0,1 %

Mn 1%

Si 1%

B 0,008 %

Nb 0,5 %

Al 0,5 %

Ti 0,15 %

NickelAlloy HX alloy is a nickel-chromium-iron-molybdenum alloy that possesses an exceptional combination of oxidation resistance, fabricability and high-temperature strength. It has also been found to be exceptionally resistant to stresscorrosion cracking in petrochemical applications. It exhibits good ductility after prolonged exposure at temperatures of 1200, 1400, 1600°F (650, 760 and 870°C).

NickelAlloy HX has wide use in gas turbine engines for combustion zone components such as transition ducts, combustor canes, spray bars and flame holders as well as in afterburners, tailpipes and cabin heaters. It is recommended for use in industrial furnace applications because it has unusual resistance to oxidizing, reducing and neutral atmosphere.

Material Data Sheet

DMLS/SLM technology

NickelAlloy HX

Physical PropertiesRelative Density 100 %

Density 8,2 g/cm3




1180°C 6h Inert

1180°C - RT - - - - - - - - - Inert




Elongation at Break ISO 6892-1:2009(B) Annex D Approx. 37 ± 6% Approx. 24 ± 4%


Hardness DIN EN ISO 6506-1 35 ÷ 40 HRC - - - - - - - - -

Thermal PropertiesThermal conductivity ASTM E1461-13 10.3 W/m°C - - - - - - - - -

Specific heat capacity ASTM E1461-13 436 J/kg°C - - - - - - - - -

Chemical CompositionNi 57%

Cr 19.5%

Co 10%

Mo 8.5%

Ti 2.1%

Al 1.5%

Mn 0.3%

Fe 1.5%

C 0.06%

Si 0.015%

B 0.005%

Alloy 282 is a new, wrought, gamma-prime strengthened superalloy developed for high temperature structural applications, especially those in aero and industrial gas turbine engines. It possesses a unique combination of creep strength, thermal stability, weldability, and fabricability not found in currently available commercial alloys.

The new alloy has excellent creep strength in the temperature range of 1200 to 1700°F (649 to 927°C). The features of Alloy 282 make it suitable for critical gas turbine applications, such as sheet fabrications, seamless and flash butt-welded rings, and cases found in compressor, combustor, and turbine sections.

Material Data Sheet

DMLS/SLM technology

Alloy 282


Density 8,27 g/cm3



RT - 1150°C 0 Argon/Vacuum

1150°C 2h Argon/Vacuum

1150°C - RT - - - - - - - - - Argon o Nitrogen


RT - 800°C 0 Argon/Vacuum

800°C 8h Argon/Vacuum

800°C - RT - - - - - - - - - Argon o Nitrogen




Elongation at Break ISO 6892-1:2009(B) Annex D 2.5 ± 0.2% 6.3 ± 0.2%


Hardness - Rockwell - - - - - - - - - 55 ± 1 HRC 53 ± 1 HRC

Thermal PropertiesThermal conductivity ASTM E1461-13 30 W/m°C - - - - - - - - -

Specific heat capacity ASTM E1461-13 460 J/kg°C - - - - - - - - -

Chemical CompositionC 0.16 - 0.25%

Mn 1.5%

Si 1.0%

Cr 12-14%

Ni 0.1%

P 0.04%

S 0.03%

AISI 420 is the most common grade of martensitic steel. This tempered steel presents the completely complementary characteristics of the most used ferritic and austenitic steel.

The tempering process to which it is subjected makes it very useful for cutlery, surgical and dental instruments, springs, molds for plastics, spheres, wear resistant components, pump components, parts in control devices, diesel engine pumps. In tempered and annealed state with mirror-polished surfaces it has good resistance to corrosion in highly aggressive, non-chlorinated environments.

Material Data Sheet

DMLS/SLM technology

AISI 420


Density 7.70 g/cm3




315°C 2h Inert

315°C - RT - - - - - - - - - Inert

MATERIAL DESCRIPTION

PROTOTYPES

Stiffness ColorFunctional Aesthetic

DM

LS /

SLM

Scalmalloy® This material is corrosion-resistant and combines the low weight of aluminium with almost the specific strength of titanium.

Suitable materials for definitive parts.

All functional tests can be performed on

prototype parts as they were the final product.

Suitable for finishes and surface treatments.

Ideal for rapid manufacturing products.

Aluminium HTA Aluminium HTA - High Temperature Aluminium – is a material developed with the objective of ensuring high performance even at 190—200°C.

Alloy 263 Alloy 263 is a nickel-cobalt-chromium-molybdenum alloy designed specifically to combine very good strength proper-ties with excellent fabrication characteristics in the annealed condition. The alloy is also age hardenable.

Böhler M789 The M789 Böhler material combines the easy printability of a Maranging Steel with the corrosion resistance of a 17-4PH (Stainless Steel AISI630).

Böhler W360 The W360 Böhler material is a hot work tool steel with high hardness, specially developed for use in warm forging applications or for forging dies.

Böhler E185 The E185 Böhler material is a low alloyed steel with easy printability and the possibility for surface treat-ment like case hardening or nitrinding.

Aluminium AlSi7Mg 0.6 (A357) Definitive aluminum, very workable and extremely resistant.

Very low specific weight (light). AlSi7Mg is an alloy for aerospace applications.Aluminium AlSi10Mg

Titanio Ti6Al4V (Grade 23 ELI)

Titanium grade 23, ideal for use in automotive, medical and jewelery applications according to ASTM F136-02a.

Inconel 718Nickel based alloy for the production of components for high temperatures applications.

Inconel 625

Stainless Steel AISI 316L

It’s an austenitic stainless steel for the production of functional parts or components for pre-production moulds.

Stainless Steel 17-4ph

It’s a precipitation hardening stainless steel for the production of functional parts or medical instruments.

Stainless Steel 15-5PH

15-5 PH Stainless Steel is a martensitic precipitation-hardening stainless steel that provides an outstanding combina-tion of high strength, good corrosion resistance, good mechanical properties at temperatures up to 600 °F (316 °C).

Cobalt-Chrome F75 Material with high mechanical and thermal resistance, ideal for models with thin walls and subjected to high temperatures.

Remanium® Star CL Cobalt Chrome for dental applications.

Bronze It’s a material whose melting properties make it outstandingly suited to generative processing.

Copper Alloy CuNi2SiCr

Material with favorable combination of electrical and thermal conductivity accompanied by high stiffness.

Maraging Steel 1.2709

Material for the production of components for tool inserts with conformal cooling and production of fuctional components.

NickelAlloy HXNickelAlloy HX is a nickel-chromium-iron-molybdenum alloy in fine powder form. This type of alloy is cha-racterized by having high strength and oxidation resistance also at elevated temperatures and is often used up to 1200°. Therefore, its applications can be found in aerospace technology, Oil & Gas and gas turbine parts.

Alloy 282 Alloy 282 is a superalloy suitable for the aerospace and Oil & Gas industries developed for use in critical applications at temperatures close to 1000 ° C as turbine parts and exhausts.

AISI 420The AISI 420 is a self-hardening martensitic steel which has complementary characteristics to ferritic and austenitic steels. The hardening process to which it is subjected makes it very useful for cutlery, structural parts, surgical and dental instruments, parts of valves.

Tungsten Tungsten is a material with high wear resistance used for the production of tools for the metalworking, mining, pe-troleum and construction industries. Tungsten is radiation-resistant and is widely used for aerospace applications.

SLS

PA 603-CF PA 603-CF is a carbon fiber filled nylon 12 easy to process, strong, light weight filled material. Its peculiarities are: low specific weight, good dimensional stability, excellent mechanical properties and excellent resistance to warping. ✓ ✓ Rigid Black

PA 620-MFPA 620-MF is a mineral fiber filled nylon 12 easy to process, performing and heavier weight filled material. Fibers have been optimized to produce a smooth surface finish without sacrificing feature detail for mechanical properties. The material boasts isotropic mechanical properties, excellent combination of strength and resistance to high temperatures.

✓ ✓ Rigid White, Black

PA6GB40 The PA6GB40 material is a glass filled polyamide widely used in all those applications where the compo-nents are subject to wear or friction. Compared to PA12, it has superior mechanical properties. ✓ Semi-

RigidWhite

WhiteSinter Standard white nylon (PA12) with good characteristics of flexibility and elasticity. ✓ Semi- Rigid

White

DuraForm EX Black

DuraForm EX is an impact resistant rigid plastic that is ideal for applications where impact resistance is required and functional hinges. DuraForm EX combines the characteristics of ABS with extraordinary flexural strength and it is perfect for creating functional snaps and hinges.

✓ ✓ Rigid Black

Polypropylene (PP) Polypropylene (PP) for Selective Laser Sintering. With this material pre-series parts can thus be produced in the same basic material as large series parts. Decisive advantages of this material are the outstanding toughness and media resistance. ✓ ✓ Semi-

RigidWhite


MATERIAL DESCRIPTION

PROTOTYPES

Stiffness ColorFunctional Aesthetic

SLS

TPU Thermoplastic elastomer material with rubber-like flexibility and functionality for use with sPro 60 HD-HS. ✓ ✓ ElasticIvory, Yellow,Black, Red, Blue

CastformTM PS CastformTM PS is a Styrene-based, expendable pattern casting material, compatible with most standard foundry processes. For prototype metal castings and low to medium production runs without tooling. ✓ Red

FlexSinter- Infiltrated

Very tough elastomer, available in various colors; aesthetic quality lower than that of polyjet rubber. ✓ ElasticIvory, Yellow,Black, Red, Blue

Allusinter Nylon reinforced with aluminum. Structural material, rigid and with highmechanical strength. Excellent reproduction of details. ✓ ✓ Rigid Light Gray

FDM

ASA It’s similar to ABS M30, but is UV resistant. It’s ideal for end use parts. ✓ RigidIvory, Black, Light Gray, Dark Gray, White, Dark Blue, Green, Yellow, Orange, Red

ABS M30 Standard ABS created with FDM systems. Properties are identical to ABS injection molded. ✓ RigidIvory, Dark Gray, White, Black, Red, Blue

ABS-ESD7ABS thermoplastic with static dissipative properties: prevents static charges from damaging products, or impair their performance. ✓ Rigid Black

ABSi Components made from translucent Absi are penetrable by light. Monitoring of inside fluid movement is allowed. ✓ RigidTranslucent Natural-Amber-Red

PC Polycarbonate. Material with high mechanical resistance, it is suitable for the creation of very strong and definitive models. ✓ Rigid White

PC-ISO Polycarbonate ISO is an ideal material for the food, packaging and medical (certified for medical use) industry. ✓ Rigid Translucent Natural, White

PC-ABS ABS and polycarbonate. Material that combines mechanical and thermal properties of the PC and the flexibility of ABS. ✓ Rigid Black

NYLON 12 Nylon 12 has an elongation at break greater than 100-300%. It has high impact resistance and excellent chemical resistance. ✓ Rigid Black

NYLON 6Nylon 6 combines strength and toughness superior to other FDM Thermoplastics, for applications that require strong, customized parts and tooling that lasts longer and withstands rigorous functional testing. ✓ Rigid Black

NYLON 12CFFDM Nylon 12CFTM is a carbon-filled thermoplastic with excellent structural characteristics. The material is comprised of a blend of Nylon 12 resin and chopped carbon fiber, at a loading of 35% by weight. ✓ Rigid Black

PPSF Polyphenylensulphone. Material highly resistant to heat, it can be used in autoclave and it can be sterilized with various methods. ✓ Rigid Tan

ULTEM® 9085 Thermoplastic resin with high mechanical and thermal properties. Ideal for parts subject to high stress. Flame retardant. ✓ Rigid Tan, Black

ULTEM® 1010Offering excellent strength and thermal stability with food contact and bio-compatibility certifications; it’s ideal for food production tools, custom medical devices, aerospace and automotive applications. ✓ Rigid Tan

Antero 800NAAnteroTM 800NA is a PEKK-based FDM® thermoplastic. It combines FDM’s design freedom and ease of use with the excellent mechanical properties and low outgassing characteristics of the PEKK material. ✓ Rigid Tan

HP

HP 3D PA 12The HP 3D PA 12 material is a highly optimized 3D thermoplastic for high reusability. It allows you to get high-precision models with dimensional tolerances. ✓ ✓ Rigid Black

PA12 FDA (Food Grade)

The characteristics of PA12 FDA are: high resistance to fats, oils, water, saline solutions and solvents. It is a material suitable for the production of objects that need to come into contact with food (after certification of the process).

✓ ✓ Rigid Black

HP 3D PA11PA11 is a thermoplastic material which offers optimal mechanical properties and provides excellent cor-rosion resistance. Its ductility makes it suitable for the production of components with snap insertions. ✓ ✓ Rigid Gray

HP 3D PA12 Glass Beads

PA12 Glass Beads material is 40% glass filled and is ideal for applications requiring high stiffness like enclosures, housing and tooling. ✓ ✓ Rigid Black

PO

LYJE

T

Vero FamilyDurable and strong, this family of Rigid Opaque photopolymers provides excellent detail visualization and is available in a variety of colors: gray, black, white and blue. ✓ Rigid

Gray, Black, White, Blue

Vero Clear Transparent photopolymer, ideal for simulating PMMA, PC models or transparent methacrylate. ✓ Rigid Transparent, Opal

ABS-Like 2 Pigmented photopolymer particularly suitable for functional models (excellent stability), not suitable for walls <0.8 mm. ✓ Rigid Light Green

Helios RGD 525 HT Very rigid pigmented photopolymer, suitable for applications where thermal stability and extreme detail are required. ✓ ✓ Rigid Ivory

Full Cure 720 Translucent photopolymer with high accuracy and excellent surface smoothness (certified for medical use). ✓ Rigid Translucent Amber

Tango FamilyThe family of Rubber-like materials offers a variety of elastomer characteristics including Shore scale A hardness, elongation at break, tear resistance and tensile strength. ✓ Elastic

Traslucent Amber, Black, Light Gray

Endur RGD 450Endur RGD 450 is a tough and flexible photopolymer. It enables you to 3D print precision prototypes that look and behave like injection-molded polypropylene. ✓ Rigid Ivory

SLA

Accura® 25 Flexible plastic to simulate and replace CNC machined white polypropylene articles. ✓ Semi- Rigid

White

Somos® GP Plus 14122

Somos® GP Plus 14122 is a low-viscosity stereolithography resin with an opaque white appearance. This material mirrors production plastics like ABS and PBT and it is easily integrated in production cycles. Somos® GP Plus 14122 is a very versatile material.

✓ Rigid White

Accura® ClearVue™ High clarity plastic (transparent) for a multitude of applications. ✓ Rigid Transparent

Accura® Xtreme™ Ultra tough grey plastic to replace CNC-machined polypropylene and ABS articles. ✓ Rigid Gray

Somos® PerFORMSomos® PerFORM produces strong, stiff, high temperature resistant composite parts that are ideal for tooling and wind tunnel testing applications. ✓ Rigid White

Metal Laser Sintering DMLS/SLM - Zare€¦ · Metal Laser Sintering DMLS/SLM Metal End-Use Parts...

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