Lanthanum hexaboride LaB6

LaB6 · CAS 12008-21-8

Lanthanum hexaboride (LaB6) is a boride ceramic used as a hot electron source.

10 sources · Updated 2026-10-26 · CC BY 4.0

Evidence level

2 of 5

Lab-measured

Melting

2528 K

Electron emission

2.6 eV

Hardness

20 GPa

Heat conduction

47 W/mK

Recipe, share of the weight

  • La not statedLanthanum
  • B not statedBoron

Best for

Hot electron sources in electron beam instruments and Hall thruster hollow cathodes, where a low work function matters more than oxidation resistance in air

Weakest at

Oxidation in air from 500 degC, and oxygen poisoning of the emitter in oxygen-rich plasma

Risk at a glance

  • People None found. Not classified in PubChem or Materion SDS
  • If it fails Moderate. Electron emission loss from oxygen poisoning
  • Corrosion Moderate. Oxidation starts at 500 degC and speeds up at 700 degC. At 900 degC a protective oxide layer formed and stayed continuous after 64 h in air.

Quick facts: LaB6

Key properties of LaB6
PropertyValueBasis
Density4.72 g/cm³1 sourced value
Thermal conductivity47 W/(m·K)1 sourced value
Thermal expansion (CTE)6.2 ppm/K1 sourced value
Melting point2,255 °C1 sourced value
Electrical resistivity1.5e-7 Ω·m1 sourced value

What is the density of Lanthanum hexaboride (LaB6)?

Lanthanum hexaboride (LaB6) has a density of 4.72 g/cm³. The source and test conditions are listed in the properties table on this page.

What is the thermal conductivity of Lanthanum hexaboride (LaB6)?

Lanthanum hexaboride (LaB6) has a thermal conductivity of 47 W/(m·K). The source and test conditions are listed in the properties table on this page.

What is the coefficient of thermal expansion of Lanthanum hexaboride (LaB6)?

Lanthanum hexaboride (LaB6) has a coefficient of thermal expansion of 6.2 ppm/K. The source and test conditions are listed in the properties table on this page.

What is the melting point of Lanthanum hexaboride (LaB6)?

Lanthanum hexaboride (LaB6) has a melting point of 2,255 °C. The source and test conditions are listed in the properties table on this page.

What is Lanthanum hexaboride (LaB6) used for?

Uses recorded in the sources include Thermionic electron source (hot cathode) for electron beam instruments; Hollow cathode electron source for a 6-kW Hall thruster; HERMeS 12.5-kW Hall thruster hollow cathode (NASA development).

Why it exists

LaB6 is a hard boride with a low work function. The vendor table gives 2.6 eV, and NASA's 2017 work uses the accepted 2.66 eV reference for polycrystalline LaB6, while its own measurements in gas discharge gave 2.1 to 2.44 eV. The vendor gives a melting point of 2528 K, so the material can stay solid at the heater temperatures used for hot cathodes. Its limits are oxidation from 500 degC in air and oxygen poisoning in oxygen-rich plasma.

Where it's used

Electron beam instruments

The vendor claims 10 times the brightness of tungsten cathodes and 50 times the service life, with no hours given.

Hall thruster hollow cathodes

NASA rated a compact LaB6 emitter cathode for 10 to 60 A on a 6-kW Hall thruster. The HERMeS cathode must provide 8 to 32 A for 34,000 hours.

Space applications

NASA development and ground tests only. No flight record was read in this run.

Recipe

LaB6

LaB6 is one lanthanum to six boron in the formula LaB6 (PubChem, CAS 12008-21-8, molar mass 203.8 g/mol). Sonber et al. found that pressureless sintering at 1950 degC reached 85.1 percent of theoretical density, while hot pressing at the same temperature gave near-theoretical density.

What LaB6 is made of
IngredientShare of the weightWhat it does
Lanthanum La not stated Rare-earth metal component. NASA's 2017 work says a lanthanum-rich emitting surface forms in gas discharge, with a lower work function than the bulk.
Boron B not stated Boron framework that pairs with the lanthanum in the formula LaB6 (PubChem).

Weight shares are as printed in the sources.

What it can do

Melting

2528 K

measured

The vendor gives a melting point of 2528 K.

Electron emission

2.6 eV

measured

The vendor table gives 2.6 eV. NASA measured 2.1 to 2.44 eV in hollow cathodes run in gas discharge.

Hardness

20 GPa

measured

Dense LaB6 is about 20 GPa hard (Sonber 2014, test load not stated).

Heat conduction

47 W/mK

measured

The vendor gives 47 W/mK at 20 degC.

How it compares

Within this profile, LaB6 has a density of 4.72 g/cm3, a melting point of 2528 K and a work function of 2.6 eV. The sources read do not name a second material for a direct ranking. The vendor claims about 10 times the brightness of tungsten cathodes, which is a vendor claim and not an independent test.

The same measurements for each material, so you can compare them. Each row names the key condition under the value; the full conditions and methods are in the numbered notes under Technical details. Other materials are shown beside it; each was measured under its own conditions, so open its page before comparing closely. Compare every grade in the family.

Benchmarks
MeasurementLaB6CrB2TM boridesMoSi2TiB2MSi2
Thermal behavior and safety
Melting point, LaB6 (vendor specification)2528 K11850 °C3245 °Cno data3225 °C2160 °C
Thermal conductivity, LaB6 (vendor specification)47 W/mK4no data60 W/(m·K)30 W/m·K96 W/m·Kno data
Oxidation onset temperature in air, LaB6 (thermogravimetry)500 °C12no datano datano datano datano data
Physical and electrical
Density, LaB6 (vendor specification)Density row of the vendor specification table4.72 g/cm³5.15 g/cc6.119 g/cm³5.6 g/cm³4.5 g/cm³9.3 g/cm³
Electrical resistance, LaB6 (vendor specification)15 uOhm·cm6no datano data23 to 27 uOhm·cm9 to 15 uOhm·cm12 to 24 uOhm·cm
Emission current density, LaB6 cathode (vendor specification)150 A/cm²7no datano datano datano datano data
Hardness, LaB6 (vendor specification, Rockwell A)87.5 RA8no datano datano datano datano data
Hardness, dense LaB6 (Sonber 2014)Quoted in the paper summary for dense LaB620 GPa9.72 GPa23 GPa9 GPa25 GPano data
Relative density after pressureless sintering (Sonber 2014)85.1 %11no data97.7 %no datano datano data
Other measurements
Electron emissivity (work function), LaB6 cathode (vendor table)2.6 eV2no datano datano datano datano data
Work function, LaB6 hollow cathode emitter (measured in gas discharge)Estimated range printed in the abstract2.1 to 2.44 eVno datano datano datano datano data
Accepted work function, polycrystalline LaB6 (as quoted by the NASA authors)2.66 eV3no datano datano datano datano data
Mean coefficient of thermal expansion, LaB6 (vendor specification)6.2 10-6/K511.1 10-6/K5.9 10-6/K7 to 8 10-6/K7.4 10-6/Kno data
Flexure strength, LaB6 (vendor specification)200 MPa9no datano data450 MPa400 MPano data
Fracture toughness, dense LaB6 (Sonber 2014)3.02 MPa m1/210no data4 MPa·m1/23 to 4 MPa·m1/26.2 MPa·m1/2no data

Why choose it, and why not

Good for

  • Hot-cathode electron sources: vendor work function 2.6 eV, and NASA's 2.66 eV reference for polycrystalline LaB6.
  • Hall thruster hollow cathodes that need less stringent xenon purity than barium oxide cathodes (NASA 2010).

Watch out for

  • Oxidation: starts at 500 degC in air and speeds up at 700 degC (Sonber 2014).
  • Oxygen: LaB6 resists poisoning better than dispenser cathodes, but oxygen still cuts emission (Michigan Tech thesis).
  • Work function: measured 2.1 to 2.44 eV in gas discharge, against 2.6 and 2.66 eV in the vendor table and the accepted value.
  • No lifetime in hours for a LaB6 cathode was found in a source read.

LaB6 is a dense, high-melting boride used as a hot electron source in electron beam instruments and Hall thruster cathodes. Its limits are oxidation from 500 degC in air and oxygen poisoning in oxygen-rich plasma. PubChem and the Materion SDS show no hazard classification, but the SDS reports no toxicology data.

Technical details

For scientists and researchers. Everything above comes from the record below: every number with its method, its conditions and its source.

Notes

The method, full conditions and any caveat for the numbered rows above.

Notes for the numbered rows
#MeasurementMethodConditionsCaveat
1Melting point, LaB6 (vendor specification)Melting Point row of the vendor specification table, printed in kelvinbasis vendor specification table; the same figure is in the page body—
2Electron emissivity (work function), LaB6 cathode (vendor table)Electron Emissivity row of the vendor specification table. The page body gives near 2.70 eV for the work function, and the page does not reconcile the two values.basis vendor specification table; crystal face and temperature not stated—
3Accepted work function, polycrystalline LaB6 (as quoted by the NASA authors)Quoted in the abstract as the accepted value that does not describe hollow cathode emission in gas dischargebasis polycrystalline LaB6, described by the authors as the accepted value—
4Thermal conductivity, LaB6 (vendor specification)Thermal Conductive row of the vendor specification table, printed as 47 W/mK at 20 degCtemperature 20 °C—
5Mean coefficient of thermal expansion, LaB6 (vendor specification)Thermal Expansion row of the vendor specification table, printed as 6.2 10-6 K-1 over 20 to 900 degCtemperature 20 to 900 °C—
6Electrical resistance, LaB6 (vendor specification)Electrical Resistance row of the vendor specification table, printed as ca.15 uOhm cm at 20 degC. The label says resistance, and the unit is a resistivity.temperature 20 °Cnote on value printed as ca.15 (approximate)—
7Emission current density, LaB6 cathode (vendor specification)Currency Density row of the vendor specification table (the page's own spelling), printed as 150 A/cm2 at 1950 degCtemperature 1950 °C—
8Hardness, LaB6 (vendor specification, Rockwell A)Hardness row of the vendor specification table, printed as 87.5 RAbasis vendor specification table; test method printed as RA—
9Flexure strength, LaB6 (vendor specification)Flexure Strength row of the vendor specification table, printed as 200 Mpabasis vendor specification table; temperature, form and grade not stated—
10Fracture toughness, dense LaB6 (Sonber 2014)Quoted in the paper summary with the hardness of dense LaB6basis dense LaB6 as stated in the paper; test method not stated in the summary—
11Relative density after pressureless sintering (Sonber 2014)Printed as a percentage of theoretical density after pressureless sinteringtemperature 1950 °Cprocess pressureless sintering of LaB6 powder—
12Oxidation onset temperature in air, LaB6 (thermogravimetry)Thermogravimetry result quoted in the paper summary. Oxidation starts slowly at this temperature and accelerates at 700 degC.atmosphere airbasis onset of slow oxidation, not a service limit; the time of the thermogravimetry run is not givenCustom property name. It marks the start of oxidation, not a safe limit.

Corrosion and compatibility

What happens when it meets other materials and environments.

Corrosion and compatibility
EnvironmentConcernWhat happens
Air at 500 to 900 degC (thermogravimetry and isothermal oxidation of dense LaB6) moderate Oxidation starts at 500 degC and speeds up at 700 degC. At 900 degC a protective oxide layer formed and stayed continuous after 64 h in air.1
Very low Earth orbit air-breathing electric propulsion, where oxygen and nitrogen are the main constituents moderate Oxygen poisons Hall thruster cathodes. LaB6 resists this better than dispenser cathodes, and the thesis seeks rare-earth alloys that do better than LaB6.2
Corrosion details
#EnvironmentDetailsTest conditions
1 Air at 500 to 900 degC (thermogravimetry and isothermal oxidation of dense LaB6) Sonber et al. report that thermogravimetric oxidation starts slowly at 500 degC and accelerates at 700 degC. An isothermal test at 900 degC gave a protective continuous oxide layer that was still present after 64 h exposure in air. The summary does not give the thermogravimetry run time or the oxide phases. temperature 500 to 900 °Ctime 64 hatmosphere air
2 Very low Earth orbit air-breathing electric propulsion, where oxygen and nitrogen are the main constituents The thesis abstract says oxygen causes a Hall-effect thruster cathode to poison, which sharply decreases electron emission and reduces thrust. It names LaB6 and dispenser cathodes as the two thermionic options, and says LaB6 has better resistance to oxygen poisoning. The project explores alloys of LaB6 and other rare-earth hexaborides that tolerate oxygen better. Its test results were not read. environment Very low Earth orbit, atomic oxygen and nitrogen as the main constituentstest not stated in the abstract

Risks and side effects

Hazards to people, what happens when a cell overheats, and how the material is handled and stored.

For people

PubChem and the Materion SDS both show no hazard classification, but the SDS reports no toxicology data. Treat the powder as an unknown inhalation hazard and control dust.

Dust
Materion says to observe good industrial hygiene practices and to wear respiratory protection if ventilation is insufficient.
Data gap
Materion's toxicology section says classification is not possible due to lack of data for every route.

If an emitter fails

These figures come from NASA hollow cathode work and Sonber 2014.

Oxygen
Oxygen poisons Hall thruster cathodes and sharply reduces emission. LaB6 resists this better than dispenser cathodes (Michigan Tech thesis abstract).
Brittleness
Dense LaB6 has a fracture toughness of 3.02 MPa m1/2 and a hardness of 20 GPa (Sonber 2014).

Test details
The original wording and numbers from the sources, for readers who want them.

Failure risks

Failure risks
FailureTrigger and consequence
Electron emission loss from oxygen poisoningmoderate severityOxygen in the propellant or plasma of an air-breathing or oxygen-rich Hall thrusterThe thesis abstract says oxygen poisoning sharply decreases electron emission and so reduces thrust. LaB6 resists it better than dispenser cathodes.
Brittle fracture of dense ceramicmoderate severityTensile or bending load on a flawDense LaB6 has a fracture toughness of 3.02 MPa m1/2 (Sonber 2014), so a flaw can grow under load. The paper summary gives no flexural strength.
Heater or cathode life limitmoderate severityLong-duration operation of a heated LaB6 hollow cathodeNASA planned LaB6 heater life testing to validate heater reliability for the HERMeS cathode. No result is given in the slides read.

Handling and storage

  • Materion SDS: observe good industrial hygiene practices, wash hands after handling, and store in the original tightly closed container away from incompatible materials.
  • Materion SDS: in a fire, use water spray to cool unopened containers. Gases hazardous to health may form during a fire. After a spill, stop the flow if safe and flush the area with water.
  • Oxidation starts at 500 degC in air (Sonber 2014). The sources read give no handling rule for it.

Supply and geography

How common the raw materials are and where they come from.

Rare earths (lanthanum is one of the rare earths; the USGS chapter read gives no lanthanum-only production figure)

USGS 2026: about 390,000 t of rare-earth oxide was mined worldwide in 2025 (rounded). World reserves of 44,000,000 t are reported for China alone. U.S. imports of rare-earth compounds and metals were 71 percent from China (2021 to 2024). The USGS lists 1,100 t of lanthanum as potential government stockpile acquisitions for FY 2025.

Top producers (2025)
China 69.2%, United States 13.1%, Australia 7.4%
Recycling
USGS: limited quantities of rare earths were recovered from batteries, permanent magnets and fluorescent lamps.

Boron (the boron half of LaB6)

USGS 2026: the 2025 world total is withheld (XX), so shares are not calculated. 2025 production as printed: Turkey 1,500 t of refined borates, Bolivia 380 t of ulexite, Peru 220 t of crude borates and China 230 t as boric oxide equivalent. U.S. imports of all forms came from Turkey (90 percent, 2021 to 2024).

Critical mineral lists
US: listed
Recycling
USGS: insignificant.