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The range of our standard metal powder Non Ferrous, Tool Steel, Stainless Steel and Light Alloys Discover the variety of Metal Powders

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Page 1: Discover the variety of Metal Powders - SLM Solutions · Discover the variety of Metal Powders. ... 8 ± 3 Surface roughness R z [μm] 36 ± 8 57 ± 11 42 ± 6 - 40

The range of our standard metal powderNon Ferrous, Tool Steel, Stainless Steel and Light Alloys

Discover the variety of Metal Powders

Page 2: Discover the variety of Metal Powders - SLM Solutions · Discover the variety of Metal Powders. ... 8 ± 3 Surface roughness R z [μm] 36 ± 8 57 ± 11 42 ± 6 - 40

Individual hip implantat in titanium

Memberships for Industry Development:

SLM Solutions, headquartered in Luebeck, Germany, is a leading provider of metal-based additive manufacturing technology (also commonly referred to as „3D printing“ ). The company‘s shares are traded on the Prime Standard of the Frankfurt Stock Exchange.

SLM Solutions focuses on the development, assembly and sales of machines and integrated system solutions in the field of selective laser melting. SLM Solutions currently employs over 300 members of staff in Germany, the USA, Singapore, Russia and China. The products are utilized worldwide by customers in particular from the aerospace, energy, healthcare and automotive industries.

SLM Solutions stands for technologically advanced, innovative and highly efficient integrated system solutions.

Headquarters

SLM Solutions Group AGRoggenhorster Strasse 9c23556 LübeckGermany

Fax +49-451-16082-250Phone +49-451-16082-0E-Mail [email protected]

SLM – The Industrial Manufacturing Revolution

PIONEERS in metal-based 3D printing

Page 3: Discover the variety of Metal Powders - SLM Solutions · Discover the variety of Metal Powders. ... 8 ± 3 Surface roughness R z [μm] 36 ± 8 57 ± 11 42 ± 6 - 40

Memberships for Industry Development:

Metal Variety:from dental prostheses to turbine blades

Customers from highly varied sectors utilise our machines to produce complex build parts for a large number of applications – from dental prostheses through to turbine blades. All of these products have one thing in common: they must meet the highest standards in terms of stability, surface structure or biocompatibility. And the number of utilisation scenarios is on the rise: almost all geometric forms are possible.

3D printing versus conventional manufacturingIn scenarios involving the production of smaller series of complex build parts, additive manufacturing is often

faster build time reduced by up to 90 percent

more efficient weight reduction of up to 60 percent, reduction in number of components of up to 95 percent

more cost-effective reduction of build part costs of up to 70 percent

more flexible „complexity comes for free“

in higher quality superior materials properties such as density, stability, temperature and corrosion resistance, surface structure and biocompatibility

AerospaceThis air duct made of titanium is produced in high precision without major rework.

Mechanical engineeringPump impellers made of aluminum and stainless steel with a streamlined shape geometry are made without molding costs.

AutomotiveOnly two days pass from the flexible design to the real-time test for this shaft flange.

Dental prosthesesIndividualized brackets and palatal plates are manufactured after a 3D scan no dental impression or casting is needed.

Medical technologyThe freedom of design for individual titanium implants allows for a better ingrowth for the benefit of the patients.

Energy sector

Small hydro stainless steel wheels are innovative build parts of a decentralized energy supply.

Universities and InstitutesModern engineers will find new solutions to the problems of traditional manufacturing on a daily basis.

SLM – The Industrial Manufacturing Revolution

PIONEERS in metal-based 3D printing

Page 4: Discover the variety of Metal Powders - SLM Solutions · Discover the variety of Metal Powders. ... 8 ± 3 Surface roughness R z [μm] 36 ± 8 57 ± 11 42 ± 6 - 40

Core Competencies

• Special metal powder selection for our 3D metal printing process• Extended Quality Assurance• Skilled Technical Staff for customer support • Deep Machine and Process understanding

Page 5: Discover the variety of Metal Powders - SLM Solutions · Discover the variety of Metal Powders. ... 8 ± 3 Surface roughness R z [μm] 36 ± 8 57 ± 11 42 ± 6 - 40

3D Metal Solutions

Al-Alloys Co-Alloys Ni-Alloys Ti-Alloys Tool Steel andStainless Steel

Light weight

Good alloying properties

Good processability (casting and pressing etc)

Good electrical conductivity

High toughness

High strength

Good bio- compatibility

Good corrosion resistance

High corrosion resistance

Excellent mech. strength

High creep rupture strength up to 700°C

Outstanding weldability

High strength, low weight

High corrosion resistance

Good bio- compatibility

Low thermal expansion

Good machinability

High hardness and toughness

High corrosion resistance

Good machinability

Aerospace

Automotive

General industrial applications

Dental

Medical implants

High temperature

SLM MediDent

Aerospace

Gas turbines

Rocket motors

Nuclear reactors

Pumps

Turbo pump seals

Tooling

Bio-material for implants

Aerospace

F1 motor sport

Maritime applications

Plastic injection and pressure diecasting moulds

Medical implants

Cutlery and kitchenware

Maritime

Spindles and screws

AlSi12

AlSi10Mg

AlSi7Mg

AlSi9Cu3

AlMg4.5Mn0,4

Other materialson request

CoCr28Mo6 acc to ASTM F75

SLM MediDent

IN625

IN718

IN939

HX (2.4665)

Pure Titanium

Ti6Al7Nb

Ti6Al4V

1.2709

1.4404 (316L)

1.2344 (H 13)

1.4540 (15-5PH)

1.4542 (17-4PH)

Other materials on request

Mat

eria

l Pr

oper

ties

App

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Allo

ys

Page 6: Discover the variety of Metal Powders - SLM Solutions · Discover the variety of Metal Powders. ... 8 ± 3 Surface roughness R z [μm] 36 ± 8 57 ± 11 42 ± 6 - 40

Al-Alloys

General

With a density of 2.7 g/cm³, aluminium is classified as a light metal. It is highly suited to processing and is used, for example, in thin-walled components with complex geometries. Aluminium also displays good electrical conductivity. Due to its low strength, it is used above all in alloys; currently the most common alloy is AlSi10Mg. Typical alloying additions are silicon, magnesium, copper or manganese. In alloyed forms, aluminium is used to produce components with high strength and high dynamic loadability. The components are optimal for use in areas such as aerospace engineering and the automotive industry.

Mechanical Data5

Formula Symbol and Unit

AlSi10Mg2,3 AlSi122,3 AlSi7Mg2,3 AlSi9Cu32,3

Tensile strength Rm [MPa] 397 ± 11 409 ± 20 294 ± 17 415 ± 15

Offset yield stress Rp0,2 [MPa] 227 ± 11 211 ± 20 147 ± 15 236 ± 8

Break strain A [%] 6 ± 1 5 ± 3 3 5 ± 1

Reduction of area Z [%] 8 ± 1 - - 11 ± 1

E-Modul E [GPa] 64 ± 10 - - 57 ± 5

Hardness by Vickers [HV10] 117 ± 1 110 112 ± 3 129 ± 1

Surface roughness Ra [μm] 7 ± 1 - 6 ± 1 7 ± 1

Surface roughness Rz [μm] 46 ± 8 34 ± 4 45 ± 5 46 ± 7

1 Layer thickness 30 μm 2 Layer thickness 50 μm 3 As built 4 Heat treated5 Process conditions and parameters according to SLM Solutions standards

Chemical Composition (nominal), %

Element / Material Al Si Mg Cu Fe Mn Zn Ti Ni Pb Sn Cr Others Total Others

AlSi10Mg 20-63 µm Bal. 9.00 - 11.00

0.20 - 0.45 0.05 0.55 0.45 0.10 0.15 0.05 0.05 0.05 0.05 0.15

AlSi12 20-63 µm Bal. 10.50 - 13.50 0.05 0.55 0.35 0.10 0.15 0.05 0.15

AlSi7Mg0.6 20-63 µm Bal. 6.50 - 7.50

0.45 - 0.70 0.05 0.19 0.10 0.07 0.25 0.03 0.10

AlSi9Cu3 20-63 µm Bal. 8.00 - 11.00

0.05 - 0.55

2.00 - 4.00 1.30 0.55 1.20 0.25 0.55 0.35 0.25 0.15 0.05 0.15

Page 7: Discover the variety of Metal Powders - SLM Solutions · Discover the variety of Metal Powders. ... 8 ± 3 Surface roughness R z [μm] 36 ± 8 57 ± 11 42 ± 6 - 40

Co-Alloys

Mechanical Data5

Formula Symbol and Unit

AlSi10Mg2,3 AlSi122,3 AlSi7Mg2,3 AlSi9Cu32,3

Tensile strength Rm [MPa] 397 ± 11 409 ± 20 294 ± 17 415 ± 15

Offset yield stress Rp0,2 [MPa] 227 ± 11 211 ± 20 147 ± 15 236 ± 8

Break strain A [%] 6 ± 1 5 ± 3 3 5 ± 1

Reduction of area Z [%] 8 ± 1 - - 11 ± 1

E-Modul E [GPa] 64 ± 10 - - 57 ± 5

Hardness by Vickers [HV10] 117 ± 1 110 112 ± 3 129 ± 1

Surface roughness Ra [μm] 7 ± 1 - 6 ± 1 7 ± 1

Surface roughness Rz [μm] 46 ± 8 34 ± 4 45 ± 5 46 ± 7

1 Layer thickness 30 μm 2 Layer thickness 50 μm 3 As built 4 Heat treated5 Process conditions and parameters according to SLM Solutions standards

General

Cobalt-chrome alloys are distinguished by their especially high hardness as well as high ductility. Additionally they are corrosion resistant. Due to their high bio-compatibility, cobalt-chrome alloys are among the standard alloys used in medical and dental technologies. They are used to produce dental as well as knee and hip prostheses.

Their resistance to heat makes them well-suited for use in high-temperature areas, such as in jet engines. Since cobalt-chrome components are very hard, there are limitations when it comes to exposing them to cutting processes. The SLM-process provides a low-effective option to quickly produce cobalt-chrome components.

Mechanical Data5

Formula Symbol and Unit

CoCr1, 3 CoCr2, 3 SLM MediDent

Tensile strength Rm [MPa] 1101 ± 78 1039 ± 91 1062 ± 46

Offset yield stress Re [MPa] 720 ± 18 705 ± 73 319* ± 18

Break strain A [%] 10 ± 4 10 ± 4 -

Reduction of area Z [%] 11 ± 4 11 ± 3 -

E-Modul E [GPa] 194 ± 9 191 ± 10 114 ± 5

Hardness byVickers [HV10] 375 ± 2 372 ± 7 -

Surface roughness Ra [μm] 10 ± 1 10 ± 2 7 ± 1

Surface roughness Rz [μm] 64 ± 6 65 ± 12 43 ± 2

1 Layer thickness 30 μm 2 Layer thickness50 μm 3 As built 4 Heat treated* Yield strength Rp0,25 Process conditions and parameters according to SLM Solutions standards

Chemical Composition (nominal), %

Element / Material Co Cr Mo W Al Si Fe Mn Ti Ni Pb C B N P S Be Cd Others Total Others

CoCr28Mo6 10-45 µm 1 Bal. 27.00 -

30.005.00 - 7.00 0.20 0.10 1.00 0.75 1.00 0.10 0.50 0.35 0.010 0.25 0.02 0.01

SLM MediDent 10-45 µm Bal. 22.7 -

26.74.0 - 6.0

4.4 - 6.4 2.0 0.50 0.10 0.10 0.02 0.02 0.10 0.10 0.10 0.02 0.02 0.50 0.50

1 Chemistry acc. to F75

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Ni-Alloys

General

Materials like IN or HX are examples of highly heat-resistant and corrosion resistant nickel-based alloys. In most cases, these alloys contain chrome, iron, niobium and molybdenum and other alloy components and they are often known as superalloys. Nickel-based alloys withstand higher temperatures than steels and they are also highly weldable. Their resistance to temperature is achieved through a mixture of dispersion hardening, precipitation hardening and solid solution strengthening.

Nickel-based alloys exhibit good mechanical characteristic values such as high tensile strength and good endurance strength. IN can be used at temperatures of up to 700 °C. HX can even be used at temperatures of up to 1200 °C. This makes these alloys ideally suited for aerospace technologies and for turbine production.

Another area where nickel-based alloys are used is toolmaking. These alloys are also suitable for sustained heat treatment and mechanical post treatment.

Mechanical Data5

Formula Symbol and Unit

IN7182,3 IN6251,3 IN9391,3 IN9391,4 HX1,3

Tensile strength Rm [MPa] 994 ± 40 961 ± 41 1009 ± 35 1348 ± 57 772 ± 24

Offset yield stress Rp0,2 [MPa] 702 ± 65 707 ± 41 735* ± 41 957* ± 18 595 ± 28

Break strain A [%] 24 ± 1 33 ± 2 30 ± 4 11 ± 2 20 ± 6

Reduction of area Z [%] 40 ± 7 51 ± 5 45 ± 7 12 ± 2 21 ± 7

E-Modul E [GPa] 166 ± 12 182 ± 9 177 ± 8 195 ± 6 162 ± 11

Hardness by Vickers [HV10] 293 ± 3 285 ± 3 302 ± 3 - 248 ± 4

Surface roughness Ra [μm] 7 ± 2 8 ± 1 6 ± 1 - 8 ± 3

Surface roughness Rz [μm] 36 ± 8 57 ± 11 42 ± 6 - 40 ± 14

1 Layer thickness 30 μm 2 Layer thickness 50 μm 3 As built 4 Heat treated and hipped* Yield strength Re 5 Process conditions and parameters according to SLM Solutions standards

Chemical Composition (nominal), %

Element / Material

Ni Cr Co Mo Al Fe Ti W Nb Ta Nb + Ta

C B Zr Cu Mn P S Si

HX 10-45 µm

Bal. 20.50 - 23.00

0.50 - 2.50

8.00 - 10.00

17.00 - 20.00

0.20 -1.00

0.05-0.15

1.00 0.04 0.03 1.00

IN625 10-45 µm

Bal. 20 - 23 0.1 8 -10 0.4 5 0.4 3.15 - 4.15

0.1 0.5 0.015 0.015 0.5

IN718 10-45 µm

50.00 - 55.00

17.00 - 21.00

1.0 2.80 - 3.30

0.20 - 0.80

Bal. 0.65 - 1.15

4.75 - 5.50

0.08 0.006 0.30 0.35 0.015 0.015 0.35

IN939 10-45 µm

Bal. 22.00 - 23.00

18.00 - 20.00

1.00 - 3.00

3.00 - 4.50

1.00 - 2.00

0.50 - 1.50

1.00 - 3.00

0.15 0.10 0.50 0,50

Page 9: Discover the variety of Metal Powders - SLM Solutions · Discover the variety of Metal Powders. ... 8 ± 3 Surface roughness R z [μm] 36 ± 8 57 ± 11 42 ± 6 - 40

Mechanical Data5

Formula Symbol and Unit

IN7182,3 IN6251,3 IN9391,3 IN9391,4 HX1,3

Tensile strength Rm [MPa] 994 ± 40 961 ± 41 1009 ± 35 1348 ± 57 772 ± 24

Offset yield stress Rp0,2 [MPa] 702 ± 65 707 ± 41 735* ± 41 957* ± 18 595 ± 28

Break strain A [%] 24 ± 1 33 ± 2 30 ± 4 11 ± 2 20 ± 6

Reduction of area Z [%] 40 ± 7 51 ± 5 45 ± 7 12 ± 2 21 ± 7

E-Modul E [GPa] 166 ± 12 182 ± 9 177 ± 8 195 ± 6 162 ± 11

Hardness by Vickers [HV10] 293 ± 3 285 ± 3 302 ± 3 - 248 ± 4

Surface roughness Ra [μm] 7 ± 2 8 ± 1 6 ± 1 - 8 ± 3

Surface roughness Rz [μm] 36 ± 8 57 ± 11 42 ± 6 - 40 ± 14

1 Layer thickness 30 μm 2 Layer thickness 50 μm 3 As built 4 Heat treated and hipped* Yield strength Re 5 Process conditions and parameters according to SLM Solutions standards

Mechanical Data5

Formula Symbol and Unit

Ti6Al4V1,3 Ti6Al7Nb1,3 Ti Gd II1,3

Tensile strength Rm [MPa] 1286 ± 57 1308 ± 76 > 290

Offset yield stress Rp0,2 [MPa] 1116 ± 61 1147* ± 35 > 180

Break strain A [%] 8 ± 2 5 ± 1 > 20

Reduction of area Z [%] 30 ± 10 12 ± 4 -

E-Modul E [GPa] 111 ± 4 108 ± 1 105

Hardness by Vickers [HV10] 384 ± 5 348 ± 4 130 - 210

Surface roughness Ra [μm] 12 ± 1 12 ± 1 -

Surface roughness Rz [μm] 70 ± 3 69 ± 8 36 ± 4

1 Layer thickness 30 μm 2 Layer thickness 50 μm 3 As built 4 Heat treated* Yield strength Re5 Process conditions and parameters according to SLM Solutions standards

General

Thanks to their high strength and relatively low density, as well as excellent corrosion resistance, titanium components are found across a broad spectrum of applications. Titanium and its alloys have already been successfully put to use, for example, in the automotive industry and in aerospace engineering, since around 1950.

Pure titanium is used primarily in chemical industries, process engineering or in medical technologies, wherever good corrosion resistance is especially required. An added advantage here is titanium’s low thermal expansion. Its bio-compatibility also makes titanium suitable for use in medical technologies. Therefore, dental implants or prosthetic hips, for example, can be made from titanium.

The alloy Ti6Al4V is by far the most common titanium alloy worldwide. The main reason for this is its well-balanced mechanical properties and the many years of industrial experience with this material.

Chemical Composition (nominal), %

Element / Material Ti Al V Nb Fe C N Ta O H Others Total Others

Ti6Al7Nb 20-63 µm Bal. 5.50 - 6.50

6.50 - 7.50

0.25 0.08 0.05 0.5 0.20 0,009

Ti6Al4V ELI (grade 23) 20-63 µm 1

Bal. 5.50 - 6.50

3.50 - 4.50

0.25 0.08 0.03 0.13 0.0125 0.10 0.40

Ti Gd I 20-63 µm Bal. 0.2 0.08 0.03 0.18 0.015 0.1 0.4

Ti Gd II 20-63 µm 2 Bal. 0.30 0.08 0.03 0.25 0.015 0.10 0.40

1 Chemistry acc. to F1362 Chemistry acc. to F67

Ti-Alloys

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General

Components made from tool or stainless steels are known for great hardness with a high ductility. Through selective application of alloying components, the material properties can be precisely adjusted. This means that even corrosion-resistant steel alloys like 1.4404 (316L) can be treated using the SLM-process. Applications for corrosion-resistant alloys are found in medical technologies, the automotive industry as well as in aerospace engineering. Tool steel is used above all to produce tools and moulds, and its layered structure enables components to be fitted with integrated cooling canals.

The good mechanical characteristic values of tool and stainless steel make it suitable for use in places that are exposed to heavy strain, because its high resistance to wear and tear or surface hardening keep abrasion to a minimum. Steel can also be used at high operating temperatures which reduces the amount of wear and tear on the tools.

Mechanical Data5

Formula Symbol and Unit

1.4404 / 316L2,3 1.27092,3 1.4540 / 15-5PH1,3 17-4PH2,3

Tensile strength Rm [MPa] 633 ± 28 1011 ± 39 1100 ± 50 832 ± 87

Offset yield stress RP0,2 [MPa] 519 ± 25 837 ± 76 1025 ± 25 572 ± 25

Break strain A [%] 30 ± 5 7 ± 2 16 ± 4 31 ± 3

Reduction of area Z [%] 49 ± 11 20 ± 6 - 55 ± 4

E-Modul E [GPa] 184 ± 20 167 ± 24 - 155 ± 22

Hardness by Vickers [HV10] 209 ± 2 321 ± 7 - 221 ± 4

Surface roughness Ra [μm] 10 ± 2 8 ± 4 - 9 ± 2

Surface roughness Rz [μm] 50 ± 12 41 ± 9 14 ± 2 54 ± 15

1 Layer thickness 30 μm 2 Layer thickness 50 μm 3 As built 4 Heat treated5 Process conditions and parameters according to SLM Solutions standards

Chemical Composition (nominal), %

Element / Material Fe Cr Ni Mo Cu Ti Co Al Nb + Ta

Si Mn C N P S O

15-5PH (1.4540) 10-45 µm

Bal. 14.50 - 15.50

3.50 - 5.50

2.50 - 4.50

0.15 - 0.45

1.00 1.00 0.07 0.10 0.04 0.03 0.10

17-4 PH (1.4542) 10-45 µm

Bal. 15.50 - 17.50

3.00 - 5.00

3.00 - 5.00

0.15 - 0.45

1.00 1.00 0.07 0.10 0.04 0.03 0.10

316L (1.4404) 10-45 µm

Bal. 16.00 - 18.00

10.00 - 14.00

2.00 - 3.00

1.00 2.00 0.030 0.10 0.045 0.030 0.10

304 (1.4301) 10-45µm

Bal. 17.50 - 19.50

8.00 - 12.00

1.00 2.00 0.030 0.1 0.045 0.03 0.10

1.2709 10-45 µm

Bal. 18.00 - 19.00

4.70 - 5.20

0.50 - 0.80

8.5 - 9.5

0.05 - 0.15

0.10 0.03 0.01 0.01

Tool and Stainless Steels

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SLM Machines

SLM 280 2.0

the top seller:

The Selective Laser Melting Machine SLM 280 2.0 provides a 280 x 280 x 365 mm³ build envelope and a patented multibeam technology. The SLM 280 2.0 is equipped with one or two fiber lasers with 3D scanning optics. The machine is available in several configurations providing single optics (1x 400W or 1x 700W), twin optics (2x 400W or 2x 700W) and dual optics (1x 700W and 1x 1000W). Depending on how the build parts are arranged, a 80% higher build rate can be achieved.

This model comprised almost 70% of our new order intake in 2014. The SLM 280 is equipped with high-performance multi-laser technology, and manufactures 68% faster than the SLM 125. The SLM 280 is especially suitable for the industrial series manufacturing of medium-sized build parts.

SLM 500the flagship:

The Selective Laser Melting Machine SLM 500 provides a build envelope of 500 x 280 x 365 mm³ and the patented multi-beam technology. In the high-performance SLM 500 machine, four quad fiber lasers (4x 400W or 4x 700W) are in action simultaneously, increasing the build-up rate by up to 90% compared with the twin configuration (2x 400W or 2x 700W).

The SLM 500 has ranked as the premium product in our product range since its market launch of the end of 2013. The unit can be equipped with up to four lasers, thereby boosting the build rate by more than 250% compared with the singlelaser machine. The SLM 500 is thereby the most productive laser melting machine on the market currently. It accounted for 18% of our new order intake in 2014.

SLM 125 the compact model:

The Selective Laser Melting Machine SLM 125 offers a build envelope of 125 x 125 x 125 mm³. The flexibly applicable machine with high productivity has been designed for quick results in the research and development sector, as well as for the production of smaller build parts. In addition, the SLM 125 provides a build volume reduction of 50 x 50 x 50 mm³ thus decreasing the amount of powder by 80%.

SLM Solutions‘ most compact machine is equipped with single-laser technology, and is particularly suitable for the production of small workpieces, as in medical applications and technology, or in research and development.

Mechanical Data5

Formula Symbol and Unit

1.4404 / 316L2,3 1.27092,3 1.4540 / 15-5PH1,3 17-4PH2,3

Tensile strength Rm [MPa] 633 ± 28 1011 ± 39 1100 ± 50 832 ± 87

Offset yield stress RP0,2 [MPa] 519 ± 25 837 ± 76 1025 ± 25 572 ± 25

Break strain A [%] 30 ± 5 7 ± 2 16 ± 4 31 ± 3

Reduction of area Z [%] 49 ± 11 20 ± 6 - 55 ± 4

E-Modul E [GPa] 184 ± 20 167 ± 24 - 155 ± 22

Hardness by Vickers [HV10] 209 ± 2 321 ± 7 - 221 ± 4

Surface roughness Ra [μm] 10 ± 2 8 ± 4 - 9 ± 2

Surface roughness Rz [μm] 50 ± 12 41 ± 9 14 ± 2 54 ± 15

1 Layer thickness 30 μm 2 Layer thickness 50 μm 3 As built 4 Heat treated5 Process conditions and parameters according to SLM Solutions standards

Chemical Composition (nominal), %

Element / Material Fe Cr Ni Mo Cu Ti Co Al Nb + Ta

Si Mn C N P S O

15-5PH (1.4540) 10-45 µm

Bal. 14.50 - 15.50

3.50 - 5.50

2.50 - 4.50

0.15 - 0.45

1.00 1.00 0.07 0.10 0.04 0.03 0.10

17-4 PH (1.4542) 10-45 µm

Bal. 15.50 - 17.50

3.00 - 5.00

3.00 - 5.00

0.15 - 0.45

1.00 1.00 0.07 0.10 0.04 0.03 0.10

316L (1.4404) 10-45 µm

Bal. 16.00 - 18.00

10.00 - 14.00

2.00 - 3.00

1.00 2.00 0.030 0.10 0.045 0.030 0.10

304 (1.4301) 10-45µm

Bal. 17.50 - 19.50

8.00 - 12.00

1.00 2.00 0.030 0.1 0.045 0.03 0.10

1.2709 10-45 µm

Bal. 18.00 - 19.00

4.70 - 5.20

0.50 - 0.80

8.5 - 9.5

0.05 - 0.15

0.10 0.03 0.01 0.01

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© SL

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You need special metal powder?Please feel free to contact us.

SLM Solutions Group AG | Roggenhorster Straße 9c | 23556 Lübeck | Germany Fon +49 451 16082-0 | Fax +49 451 16082-250 | www.slm-solutions.com

SLM and SLM Solutions are registered trademarks by SLM Solutions Group AG, Germany.