Cat No:SSM-0022
Description
Sacrificial system designed for super-alloy sintering, providing structural support before disintegrating at extreme temperatures.
| Base Material | Carbon-Ceramic Matrix |
| Solubility Method | Pyrolysis |
| Solvent Type | High Temp |
| Heat Deflection Temp (0.45MPa) | 320+ |
| Glass Transition Temp (Tg) | 350 |
| Melting Point (°C) | - |
| Density (g/cm³) | 0.98 |
| Water Absorption (%) | 0.01 |
| Tensile Strength (MPa) | 28 |
| Tensile Modulus (MPa) | 5200 |
| Elongation at Break (%) | 1 |
| Flexural Strength (MPa) | 45 |
| Flexural Modulus (MPa) | 4800 |
| Printing Temp (°C) | 340-380 |
| Bed Temp (°C) | 140-160 |
| Chamber Temp (°C) | 120-150 |
| Nozzle Type | Hardened Steel |
| Layer Height (mm) | 0.2 |
| Shrinkage Rate (%) | 0.01 |
| Continuous Use Temp (°C) | 300 |
| Impact Strength (kJ/m²) | 3 |
| Flame Retardancy (UL94) | V-0 |
| Surface Resistivity (Ω) | 10^4 |
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For Research or Industrial Raw Materials, Not For Personal Medical Use!
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