Cat No:SSM-0129
Description
Advanced ceramic-matrix support for space-grade applications; survives launch-simulation environments and vacuum baking.
| Base Material | Ceramic-Matrix Resin |
| Solubility Method | Thermal |
| Solvent Type | Pyrolysis |
| Heat Deflection Temp (0.45MPa) | 500+ |
| Glass Transition Temp (Tg) | - |
| Melting Point (°C) | - |
| Density (g/cm³) | 2.05 |
| Water Absorption (%) | 0.01 |
| Tensile Strength (MPa) | 45 |
| Tensile Modulus (MPa) | 9500 |
| Elongation at Break (%) | 0.5 |
| Flexural Strength (MPa) | 90 |
| Flexural Modulus (MPa) | 9000 |
| Printing Temp (°C) | 350-400 |
| Bed Temp (°C) | 140-180 |
| Chamber Temp (°C) | 120-160 |
| Nozzle Type | Hardened Steel |
| Layer Height (mm) | 0.15 |
| Shrinkage Rate (%) | 0.01 |
| Continuous Use Temp (°C) | 450 |
| Impact Strength (kJ/m²) | 3 |
| Flame Retardancy (UL94) | V-0 |
| Surface Resistivity (Ω) | 10^16 |
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For Research or Industrial Raw Materials, Not For Personal Medical Use!
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