Dental Metal Powders

Titanium alloy, commercially pure titanium, and cobalt-chrome — the raw material behind every Space Ti® build, supplied direct from the manufacturer.

We make the powder, not just sell it

Most dental suppliers resell metal powder they never see produced. HiZir is a raw metal powder manufacturer and supplier — titanium and cobalt-chrome powders come to your lab through one chain of custody, with the composition and particle size certified batch by batch.

That vertical integration is why our print parameters are reliable. The powder, the Space Ti-160 printer, and the Space Ti-200 heat treatment furnace are developed against each other — not bolted together from three vendors who never spoke.

New to HiZir? Request a free evaluation sample — tell us your alloy and your printer, and we'll ship enough powder to run a real test build.

Request a Free Sample Request a Quote
Dental restorations printed from Space Ti TC4 titanium powder on a single build plate

Three alloys, one workflow

Every grade runs on the same printer and the same furnace. Choose by indication, not by equipment.

Commercially Pure
Pure Titanium TA1
Unalloyed titanium · Ti > 90
500±50
MPa yield strength (0.2% offset)

Unalloyed titanium with the highest ductility in the range — 20% elongation before fracture. Specified where maximum biocompatibility and formability outrank raw strength.

  • Titanium > 90%, no aluminium or vanadium
  • Density 4.5 g/cm³
  • Young's modulus 110 ± 10 GPa
  • Elongation after fracture 20 ± 5%
Traditional
Cobalt-Chrome
Co-Cr alloy · base metal
600±50
MPa yield strength (0.2% offset)

The stiffest option at 200 GPa — the familiar choice for rigid RPD frameworks and metal-ceramic crown and bridge work. Available in two grades tuned for different indications.

  • Co 62 · Cr 28 · W 8.5
  • Density 8.5 g/cm³
  • Young's modulus 200 ± 20 GPa
  • Elongation after fracture 15 ± 5%

Full material comparison

Standard values are the minimum required by specification. Test values are measured on printed and heat-treated specimens.

Category Titanium Alloy TC4
Space Ti® Aerospace Titanium
Pure Titanium TA1 Cobalt-Chromium Alloy
Chemical Composition (%) Titanium (Ti): Balance
Aluminium (Al): 5.50–6.50%
Vanadium (V): 3.50–4.50%
Titanium (Ti): > 90 Cobalt (Co): 62
Chrome (Cr): 28
Tungsten (W): 8.5
Processing Equipment Space Ti-160
SLM Metal 3D Printer
Space Ti-160
SLM Metal 3D Printer
Space Ti-160
SLM Metal 3D Printer
Heat Treatment Space Ti-200
Rapid Heat Treatment Furnace
Space Ti-200
Rapid Heat Treatment Furnace
Space Ti-200
Rapid Heat Treatment Furnace
0.2% Offset Yield Strength (MPa) Standard ≥ 360
Test Value 950 ± 50 500 ± 50 600 ± 50
Elongation After Fracture (%) Standard ≥ 2
Test Value 13 ± 2 20 ± 5 15 ± 5
Young's Modulus (GPa) Standard
Test Value 110 ± 10 110 ± 10 200 ± 20
Metal-Ceramic Bond Strength (MPa) Standard > 25
Test Value > 30 > 30 > 30
Density (g/cm³) 4.5 4.5 8.5

Test values are measured on SLM-printed specimens after heat treatment in the Space Ti-200 furnace. Full datasheets are available on request — see Downloads.

Two grades, two indications

Not all cobalt-chrome is interchangeable. Crown and bridge work and removable frameworks pull the alloy in opposite directions.

Crown & Bridge

Cobalt SLM Powder

A molybdenum- and tungsten-bearing Co-Cr for metal-ceramic restorations. Classified as an IdentAlloy® base metal, with the alloy certificate supplied for every batch you receive.

CompositionCo 61.5% · Cr 28.1% · Mo 5.3% · W 5% · Si 1% · Fe, Mn < 1% each
Density8.6 g/cm³
Yield strength600 MPa
Elongation8%
Hardness365 HV10
Removable Prosthetics

Cobalt H

Formulated for removable partial denture frameworks produced by laser sintering. The higher tungsten and silicon content targets clasp resilience and casting-free flexural behaviour.

CompositionCo 61.5% · Cr 27.8% · W 8.5% · Si 1.5% · Mn, Fe < 1% each
Particle size10–60 µm
ProcessSelective laser melting / sintering
IndicationRPD frameworks, clasps, major connectors
CertificateIdentAlloy® supplied per batch

Titanium or
cobalt-chrome?

The honest answer is that both still have a place. Cobalt-chrome is nearly twice as stiff and remains the reference material for rigid RPD frameworks — technicians have decades of muscle memory with it.

Titanium wins on everything the patient feels. At 4.5 g/cm³ against 8.5, a full-arch framework comes out close to half the weight. Its 110 GPa modulus sits far closer to bone than cobalt-chrome's 200 GPa, so load transfers more naturally around implants. And it contains no nickel, no beryllium, and no cobalt — the three metals behind most reported dental alloy sensitivities.

Where TC4 gives nothing away is strength: at 950 ± 50 MPa yield it is over 50% stronger than the cobalt-chrome grade, while still elongating 13% before fracture.

lighter than cobalt-chrome

4.5 g/cm³ vs 8.5 g/cm³ — the difference a patient notices on a full-arch case.

110
GPa Young's modulus

Nearer to natural bone than cobalt-chrome's 200 GPa, easing stress shielding.

0%
nickel & beryllium

Neither element appears in TC4 or TA1 — a straightforward answer for sensitive patients.

>95%
powder recovery

Unfused powder is sieved and returned to the feed — near-zero material waste per build.

Certified batch by batch

Every shipment carries its own paperwork. Nothing leaves without a composition certificate tied to the lot number.

ISO 13485 & CE 0197

Manufactured under a medical-device quality management system, with CE marking under notified body 0197.

ISO 22074 Composition

Dental alloy composition and marking to ISO 22074, so what is on the certificate is what is in the drum.

IdentAlloy® Certificate

Each alloy ships with its IdentAlloy® certificate — the disclosure form your dentist and patient records expect.

Where the powder goes

The same four stages regardless of alloy — every stage on equipment we supply and support.

1

Load & Sieve

Powder is sieved and loaded under inert atmosphere. Ultrasonic sieve and glove box keep the lot clean and the operator safe.

2

Print

The Space Ti-160 or Mini-100 fuses each 20–60 µm layer with a fiber laser.

3

Heat Treat

The Space Ti-200 furnace relieves stress and brings the printed alloy to its final mechanical properties.

4

Finish

Supports removed, then plasma polishing takes the surface to a mirror finish without hand labour.

Handling it safely, using all of it

Fine reactive metal powder needs to be treated with respect. It also represents real money sitting in the build chamber — over 95% of what you do not fuse can go straight back into the next build if you sieve it properly.

We supply the full handling chain alongside the powder itself, and cover all of it during on-site training.

See Powder Handling Equipment
  • Ultrasonic sieve & recycler — reclaims unfused powder and removes spatter before it reaches the recoater.
  • Powder vacuum cleaner — industrial units rated specifically for combustible metal powder.
  • Nitrogen generator — on-site inert gas for both printing and powder transfer.
  • Glove box — sealed loading so titanium never meets open air during transfer.
  • Sealed storage — powder returns to a sealed, labelled container tied back to its lot certificate.

Common questions

Which powders does HiZir supply?

Three families: Space Ti® TC4 titanium alloy (Ti-6Al-4V), commercially pure titanium TA1, and cobalt-chrome — the latter in a Co-Cr-Mo-W grade for crown and bridge work and a tungsten-bearing Cobalt H grade for removable frameworks.

Which printers are they qualified on?

All three run on the Space Ti-160 and heat treat in the Space Ti-200. The compact Mini-100 takes the same material set at a smaller build volume.

Can I get a free sample first?

Yes. Tell us the alloy and the printer you run and we will ship enough powder for a genuine test build. Email info@HiZir3D.com or call +1 (314) 403-5175.

How is pricing handled?

Powder is quoted per order — alloy, quantity, and delivery schedule all move the number. Submit the materials order form and we will come back with a quote.

Ready to test a batch?

Free evaluation samples for new labs. Quote-based pricing on production quantities of titanium and cobalt-chrome.