Cat No:CRSM-0063
Description
Aerospace-grade PEEK composite with high carbon fiber loading for extreme specific strength and modulus in structural space research components.
| Base Material | PEEK |
| Reinforcement Type | Chopped Carbon Fiber |
| Reinforcement Volume (%) | 0.2 |
| Density (g/cm³) | 1.38 |
| Tensile Strength (MPa) | 155 |
| Tensile Modulus (MPa) | 13500 |
| Elongation at Break (%) | 2 |
| Flexural Strength (MPa) | 230 |
| Flexural Modulus (MPa) | 12200 |
| Heat Deflection Temp (0.45MPa) | 310 |
| Glass Transition Temp (Tg) | 143 |
| Melting Point (°C) | 343 |
| Thermal Conductivity (W/mK) | 0.45 |
| Flame Retardancy (UL94) | V-0 |
| Surface Resistivity (Ω) | 10^6 - 10^8 |
| Water Absorption (%) | 0.12 |
| Printing Temp (°C) | 400-445 |
| Bed Temp (°C) | 125-155 |
| Chamber Temp (°C) | 110-150 |
| Nozzle Type | Hardened Steel |
| Layer Height (mm) | 0.1 |
| Shrinkage Rate (%) | 0.2 |
| Continuous Use Temp (°C) | 260 |
| Impact Strength (kJ/m²) | 11 |
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For Research or Industrial Raw Materials, Not For Personal Medical Use!
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