
The plasma chamber (discharge chamber) is its core component, where propellant ionization occurs and which must withstand intense thermal energy and energy impact from plasma. Hexagonal boron nitride (h-BN) is the ideal material for this component. Boasting excellent high-temperature resistance, bombardment resistance and secondary electron emission properties, it not only ensures the structural integrity of the chamber under extreme conditions, but also improves ionization efficiency, reduces chamber erosion and plasma contamination, serving as a key material for the efficient and stable operation of the thruster.
Properties:
– High Thermal Stability and Resistance
– Electrical Insulation
– Chemical Inertness
– Surface Smoothness and Machinability
Use high-purity raw materials and advanced sintering processes to ensure uniform microstructure and consistent performance of the materials. Each batch of products undergoes rigorous thermal, electrical and plasma compatibility tests to meet the reliability requirements of aerospace grade. We support customers in customizing dimensions and shapes, and provide professional technical support to assist in the design and performance improvement of thrusters.
Boron Nitride Material Properties
| Properties | Unit | UHB | HB | BC | BMS | BMA | BSC | BMZ | BAN | BSN |
| Main Composition | BN>99.7% | BN>99% | BN>97.5% | BN+SiO₂ | BN+A₂O₃ | BN+SiC | BN+ZrO₂ | BN+AIN | BN+Si₃N₄ | |
| Color | White | White | White | _White Graphite |
White Graphite |
Greyish- Green |
White Graphite |
Greyish- Green |
Gray Black |
|
| Density | g/cm³ | 1.6 | 2 | 2.0~2.1 | 2.2~2.3 | 2.25~2.35 | 2.4~2.5 | 2.8~2.9 | 2.8~2.9 | 2.2~2.3 |
| Three-Point Bending Strength |
MPa | 18 | 35 | 35 | 65 | 65 | 80 | 90 | 90 | / |
| Compressive Strength |
MPa | 45 | 85 | 70 | 145 | 145 | 175 | 220 | 220 | 400~500 |
| Thermal Conductivity |
W/(m·K) | 35 | 40 | 32 | 35 | 35 | 45 | 30 | 85 | 20~22 |
| Thermal Expansion Coefficient (20~1000°C) |
10-6/K | 1.5 | 1.8 | 1.6 | 2 | 2 | 2.8 | 3.5 | 2.8 | / |
| Max Using Temperature In Atmosphere In Inactive Gas In High Vacuum (Long Time) |
℃ | 900 2100 1800 |
900 2100 1800 |
900 2100 1900 |
900 1750 1750 |
900 1750 1750 |
900 1800 1800 |
900 1800 1800 |
900 1750 1750 |
900 1750 1700 |
| Room Temperature Electric Resistivity |
Ωcm | >1014 | >1014 | >1013 | >10³ | >10³ | >10² | >10¹² | >10³ | / |
| Typical Application | Nitrides Sintering |
High Temperature Furance |
High Temperature Furance |
Powder Metallurgy |
Powder Metallurgy |
Powder Metallurgy |
Metal Casting |
Powder Metallurgy |
Metal Casting |





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