Cat No:CRSM-0075
Description
Extreme performance continuous fiber system achieving aerospace-grade structural strength for satellite frames and engine components.
| Base Material | PEEK |
| Reinforcement Type | Continuous Carbon Fiber |
| Reinforcement Volume (%) | 0.45 |
| Density (g/cm³) | 1.55 |
| Tensile Strength (MPa) | 1800 |
| Tensile Modulus (MPa) | 145000 |
| Elongation at Break (%) | 1.2 |
| Flexural Strength (MPa) | 1100 |
| Flexural Modulus (MPa) | 125000 |
| Heat Deflection Temp (0.45MPa) | 315 |
| Glass Transition Temp (Tg) | 143 |
| Melting Point (°C) | 343 |
| Thermal Conductivity (W/mK) | 1.1 |
| Flame Retardancy (UL94) | V-0 |
| Surface Resistivity (Ω) | 10^1 |
| Water Absorption (%) | 0.05 |
| Printing Temp (°C) | 400-450 |
| Bed Temp (°C) | 130-160 |
| Chamber Temp (°C) | 120-150 |
| Nozzle Type | Hardened Steel |
| Layer Height (mm) | 0.125 |
| Shrinkage Rate (%) | 0.02 |
| Continuous Use Temp (°C) | 260 |
| Impact Strength (kJ/m²) | 145 |
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For Research or Industrial Raw Materials, Not For Personal Medical Use!
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