Class of Material
Flame retardant carbon fiber filled material UL 94 V-0 and FAR 25.853 compliant
Technology
Selective Laser Sintering
FEATURES
FAR 25.853 compliantNon-halogenated formulationSmoke density test passedTough, stiff and lightweightV-0, carbon fiber filled flame retardant
KEY VALUES
Density (20° C) 1,21 g/ccHDT (1.82 Mpa) 162,9° CMelting point 181,30° CTensile strength – X axis 65,20 MPaTensile modulus – X axis 6981 MPaHardness Shore D 82
APPLICATIONS
Aeronautic and Aerospace interior partsAutomotive and Transportation related partsConsumer goods and ElectronicsParts requiring flame retardancy
FEATURES
FAR 25.853 compliantNon-halogenated formulationSmoke density test passedTough, stiff and lightweightV-0, carbon fiber filled flame retardant
Which characteristics
are you searching for?
KEY VALUES
Density (20° C) 1,21 g/ccHDT (1.82 Mpa) 162,9° CMelting point 181,30° CTensile strength – X axis 65,20 MPaTensile modulus – X axis 6981 MPaHardness Shore D 82
Technical data sheet
DownloadAPPLICATIONS
Aeronautic and Aerospace interior partsAutomotive and Transportation related partsConsumer goods and ElectronicsParts requiring flame retardancy
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Get inspiredTechnical Properties
Density: 1,21 g/cc
Colour:
DARK GREY
Thermal Properties | Test Method | SI Unit | US Unit |
---|---|---|---|
Melting point | ISO 11357 | 181,30° C | 358.34° F |
HDT, 1.82 Mpa | ISO 75 Method A | 162,90° C | 325.22° F |
Vicat 10N | ISO 306 Method A50 | 179,00° C | 354.20° F |
Flammability Properties | Test Method | SI Unit | US Unit |
---|---|---|---|
Burning Test - HB 1mm | UL 94 | HB | HB |
Burning Test - HB 3mm | UL 94 | HB | HB |
Burning Test - V 2mm | UL 94 | V-0 | V-0 |
Burning Test - V 3mm | UL 94 | V-0 | V-0 |
Flammability - 15 seconds - Horizontal | FAR/CS 25.853 (a), Appendix F, Part I (b)(5) | pass | pass |
Flammability - 12 seconds - Vertical | FAR/CS 25.853 (a), Appendix F, Part I (a)(1) | pass | pass |
Flammability - 30 seconds - 45 degree | FAR/CS 25.853 (a), Appendix F, Part I (b)(6) | pass | pass |
Smoke Density, Flaming Mode - 4 min/240 sec | FAR/CS 25.853, Appendix F, Part V | pass | pass |
Mechanical Properties | Test Method | SI Unit | US Unit |
---|---|---|---|
Tensile Strength - X axis | UNI EN ISO 527-1 | 65,20 Mpa | 9456.46 psi |
Tensile Strength - Y axis | UNI EN ISO 527-1 | 47,40 Mpa | 6874.79 psi |
Tensile Strength - Z axis | UNI EN ISO 527-1 | 41,70 Mpa | 6048.07 psi |
Tensile Modulus - X axis | UNI EN ISO 527-1 | 6981,00 Mpa | 1012.50 ksi |
Tensile Modulus - Y axis | UNI EN ISO 527-1 | 4633,00 Mpa | 671.96 ksi |
Tensile Modulus - Z axis | UNI EN ISO 527-1 | 3315,00 Mpa | 480.80 ksi |
Elongation at Break - X axis | UNI EN ISO 527-1 | 3,18 % | 3,18 % |
Elongation at Break - Y axis | UNI EN ISO 527-1 | 3,38 % | 3,38 % |
Elongation at Break - Z axis | UNI EN ISO 527-1 | 3,06 % | 3,06 % |
Flexural Strength | UNI EN ISO 14125 | 115,24 Mpa | 16714.15 psi |
Flexural Modulus | UNI EN ISO 14125 | 6536,00 Mpa | 947.97 ksi |
Impact Strength Unnotched (Charpy 23 °C/73.4 °F) | UNI EN ISO 179-1 | 19,70 KJ/m² | 9.37 ft-lb/in² |
Impact Strength Unnotched (Charpy -40 °C/-40 °F) | UNI EN ISO 179-1 | 18,30 KJ/m² | 8.71 ft-lb/in² |
Impact Strength Notched (Charpy 23 °C/73.4 °F) | UNI EN ISO 179-1 | 5,60 KJ/m² | 2.66 ft-lb/in² |
Impact Strength Notched (Charpy -40 °C/-40 °F) | UNI EN ISO 179-1 | 4,50 KJ/m² | 2.14 ft-lb/in² |
Hardness Shore D | UNI EN ISO 868 | 82 | 82 |
Poisson Ratio - X axis | ASTM D638-14 | 0,39 μ | 0.39 μ |
Poisson Ratio - Y axis | ASTM D638-14 | 0,26 μ | 0.26 μ |
Poisson Ratio - Z axis | ASTM D638-14 | 0,22 μ | 0.22 μ |
Compression Strength - XY axis | ASTM D695 Rev 15 | 90,6 Mpa | 13140.42 psi |
Compression Strength - YX axis | ASTM D695 Rev 15 | 80,2 Mpa | 11632.03 psi |
Compression Strength - ZX axis | ASTM D695 Rev 15 | 57,4 Mpa | 8325.17 psi |
Compression Elastic Modulus - XY axis | ASTM D695 Rev 15 | 4,83 Gpa | 700.53 ksi |
Compression Elastic Modulus - YX axis | ASTM D695 Rev 15 | 2,86 Gpa | 414.81 ksi |
Compression Elastic Modulus - ZX axis | ASTM D695 Rev 15 | 2,00 Gpa | 290.07 ksi |
Electrical Properties | Test Method | SI Unit | US Unit |
---|---|---|---|
Resistivity, Volume | ASTM D257-14 | 2,1 x 10^16 ohm*cm | 2,1 x 10^16 ohm*cm |
Resistivity, Surface | ASTM D257-14 | 2,1 x 10^16 ohm | 2,1 x 10^16 ohm |
CTI Comparative Tracking Index | IEC 60112 Solution A | < 175 Volt | < 175 Volt |
Surface Finish | SI Unit | US Unit |
---|---|---|
After SLS Process | 6,78 Ra μm | 6.78 Ra μm |
After manual finishing | 1,68 Ra μm | 1.68 Ra μm |
After CNC machining | 0,73 Ra μm | 0.73 Ra μm |
Properties per Density Unit | SI Unit | US Unit |
---|---|---|
UTS per density unit | 53,74 Mpa/(g/cc) | 7794.98 psi/(g/cc) |
Tensile Modulus per density unit | 5754,45 Mpa/(g/cc) | 834.61 ksi/(g/cc) |
Flexural Strength per density unit | 94,99 Mpa/(g/cc) | 13777.51 psi/(g/cc) |
Flexural Modulus per density unit | 5387,64 Mpa/(g/cc) | 781.41 ksi/(g/cc) |
Note: The material properties provided herein are for reference purposes only. Data was generated from the testing of parts produced with Windform FR1 material under optimal processing conditions. Actual values may vary significantly as they are affected by part geometry and process parameters. Material specifications are subject to change without notice.
Standard Technical Details for Accuracy versus Tolerance:
For parts up to 1 mm (0.039″), the standard tolerance is ± 0,070 mm (0.003″)
For parts up to 3 mm (0.118″), the standard tolerance is ± 0,125 mm (0.005″)
For parts up to 6 mm (0.236″), the standard tolerance is ± 0,150 mm (0.006″)
For parts over 6 mm (0.236″), refer to UNI EN ISO 286-2 JS14 class (linear tolerances).
Technical specifications
Windform® FR1 is the newborn material from the TOP-LINE family of sls composite materials created by CRP Technology.
This revolutionary Windform® FR1 is the unique Flame Retardant (V-0 rated) material for Additive Manufacturing carbon fiber reinforced.
It passed the FAR 25.853 12-second vertical and 15-second horizontal flammability tests as well as the 45° Bunsen burner test successfully
It is halogen free polyamide based material, that combines superior mechanical properties with excellent stiffness and lightweight.
Applications
Owing to its flame-retardant quality, this high-performance composite material is suitable for Aircrafts and Aerospace applications (for example interior parts, cockpit, cabin components, air conditioning piping, air ducts, air outlet valves); Automotive and Transportation parts (vehicle interiors, housing and enclosure assemblies, air ducts, air outlet valves), Consumer goods and Electronics (lighting, appliances) and in general for any parts requiring flame retardancy.
Windform® FR1 is ideal for high feature detail applications requiring FAR 25.853 fire retardant compliancy.
It is also suitable for the manufacturing of components with detailed surface resolution.
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