CF
Thornel T-650/35 3K 3K
Cytec ? Aerospace Standard
Manufacturer page / TDSDescription
High strength PAN-based fiber, surface treated
Comparative overview
Carbon fiber — High-strength standard-modulus carbon
Strengths: Higher tensile strength and strain than baseline carbon while retaining mature standard-modulus processing.
When to use: Select for pressure vessels, pultrusion, industrial structures and sporting goods requiring strength with controlled cost.
Key tradeoffs: Less stiff than IM/HM grades; conductive and more expensive than baseline large-tow carbon.
Qualitative ratings (1–10 scale)
| Relative cost | 8/10 — High — aerospace/high-performance PAN carbon with controlled precursor, surface treatment and sizing. |
|---|---|
| EM transparency | 1/10 — Very poor — electrically conductive; causes reflection/attenuation rather than RF transparency. |
| Temperature / fire resistance | 6/10 — Good — non-melting but oxidation in air and the matrix system cap fire/hot-service performance. |
| Impact / penetration resistance | 6/10 — Good — higher strain and tensile strength than HM/UHM carbon improve impact response, but delamination and brittle fiber fracture remain. Stored TDS elongation: 1.75%. |
| Electrical / thermal conductivity | 7/10 — High — electrically conductive with moderate axial thermal conductivity typical of PAN carbon. Stored axial thermal conductivity: 14 W/m·K. |
| Specific tensile strength | 8/10 — 8/10 | 2570.6 kN·m/kg | Product TDS |
| Atmospheric durability | 9/10 — Excellent — carbon fiber is intrinsically resistant to UV, moisture and salt exposure; long-term laminate durability is usually governed by sizing, matrix, galvanic coupling and interfaces rather than the fiber. |
| Sustainability (CO₂e) | 5/10 — 19.85 kg CO₂e/kg fiber — High emissions — data quality: High |
Technical properties
| Tensile strength | 4550.0 MPa |
|---|---|
| Tensile modulus | 241.0 GPa |
| Density | 1.77 g/cm³ |
| Filament diameter | 6.8 µm |
Applications and processing
Aerospaceindustrial composites