Category: | Nylon, Unspecified , Polyamide |
Manufacturer: | CRP Technology s.r.l. |
Trademark: | WINDFORM® |
Fillers: | - |
Ports: | Qinzhou, Shekou, Shanghai, Ningbo |
Delivery Terms | FOB, CIF, DAP, DAT, DDP |
PDF: | gMukYQ_WINDFORM-XT-2-0.pdf ![]() |
PRICE: | Order Products email sales@su-jiao.com |
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Technology: Selective Laser Sintering Windform® XT 2.0 is the evolution of the ground breaking high performance Windform® XT, the carbon fiber reinforced composite material, known for its mechanical properties, which made it particularly suitable in demanding applications such as motorsport sector, aerospace and UAV's. Windform® XT 2.0 is an innovative material, and will replace the Windform® XT, as the "Top Level" of the current Windform® range. Windform® XT 2.0 improves mechanical properties compared to "traditional" Windform® XT, while maintaining the same workability for Laser Sintering machines in order to better fulfill the needs of Additive Manufacturing required to produce end use parts and prototypes. Windform® XT 2.0 retains the matte black colour of the previous version and features improvements in mechanical properties: +8% in tensile strength, +22% in tensile modulus and +46% increase in elongation at break. Windform XT® 2.0 allows for the creation of accurate, reliable and durable prototypes and is perfect for functional applications. Applications: Windform® XT 2.0 is the high-tech material for Additive Manufacturing chosen by those working in the Motorsport, Automotive (suitable for example for components under the hood, such as intake manifolds and functional cooling ducts), Air (for components UAV, Unmanned Aerial Vehicle) Aerospace (useful also to create prototype satellite, such as the CubeSat) and Design, as it allows applications that are fully functional, as well as bench testing, or testing and racing on the track. Surface Finish: After SLS Process 6.0 Ra µm After finishing 1.8 Ra µm |
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Physical | Nominal Value | Unit | |
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Density (20°C) | 1.10 | g/cm³ |
Mechanical | Nominal Value | Unit | Test Method |
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Tensile Modulus | 8930 | MPa | ISO 527-2 |
Tensile Stress | 83.8 | MPa | ISO 527-2 |
Tensile Strain (Break) | 3.8 | % | ISO 527-2 |
Flexural Modulus | 7340 | MPa | ISO 178 |
Flexural Stress | 133 | MPa | ISO 178 |
Flexural Modulus - per density unit | 6690 | MPa/g/cm³ | |
Flexural Strength - per density unit | 121 | MPa/g/cm³ | |
Tensile Modulus - per density unit | 8140 | MPa/g/cm³ | |
Ultimate Tensile Strength - per density unit | 76.4 | MPa/g/cm³ |
Impact | Nominal Value | Unit | Test Method |
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Charpy Notched Impact Strength (23°C) | 4.7 | kJ/m² | ISO 179 |
Charpy Unnotched Impact Strength (23°C) | 22 | kJ/m² | ISO 179 |
Notched Izod Impact Strength (23°C) | 5.3 | kJ/m² | ISO 180 |
Unnotched Izod Impact Strength (23°C) | 19 | kJ/m² | ISO 180 |
Thermal | Nominal Value | Unit | Test Method |
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Heat Deflection Temperature (1.8 MPa, Unannealed) | 173 | °C | ISO 75-2/A |
Vicat Softening Temperature | 176 | °C | ISO 306/A50 |
Melting Temperature | 179 | °C | ISO 11357 |
Electrical | Nominal Value | Unit | Test Method |
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Surface Resistivity | < 1.0E+8 | ohms | ASTM D257 |
Volume Resistivity | < 1.0E+8 | ohms·cm | ASTM D257 |
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NEFTEKHIM PP 7445LM | Nizhnekamskneftekhim Inc. | PP Copolymer | NEFTEKHIM PP |
Desmopan® DP 9392A | Covestro - PUR | TPU, Unspecified | Desmopan® |
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