| Standard-modulus PAN-based | Approximately 230–250 GPa | Approximately 3.5–5.0 GPa | Approximately 1.75–1.82 g/cm³ | A widely used balance of stiffness, strength, damage tolerance, and cost. PAN refers to the polyacrylonitrile precursor commonly used to make structural carbon fiber. | General-purpose composite parts, sporting goods, automotive components, and structures where a balanced property set is preferred. |
| Intermediate-modulus PAN-based | Approximately 280–320 GPa | Approximately 4.0–6.0 GPa | Approximately 1.78–1.84 g/cm³ | Higher axial stiffness than standard-modulus fiber while retaining useful tensile strength. Actual strength and strain-to-failure vary by specific fiber grade and processing. | Stiff, lightweight structural components and applications where deflection control matters. |
| High-modulus PAN-based | Approximately 350–450 GPa | Approximately 3.0–5.0 GPa | Approximately 1.80–1.90 g/cm³ | High stiffness along the fiber direction. Greater modulus does not automatically mean greater tensile strength; these fibers can have lower strain-to-failure and require careful design. | Precision structures, aerospace components, and parts that need high stiffness with low mass. |
| High- or ultra-high-modulus pitch-based | Often approximately 400–900+ GPa, depending on grade | Highly grade-dependent; often approximately 2.0–4.0 GPa | Approximately 1.90–2.20 g/cm³ | Pitch-based fibers can achieve exceptionally high axial modulus and, in some grades, high thermal conductivity. They are generally more specialized and can be more brittle or less tolerant of handling damage. | High-stiffness components, thermal-management structures, and applications requiring high thermal conductivity along the fiber direction. |
| Woven carbon-fiber fabric | Depends on the fiber grade and weave; properties are lower at laminate level than straight-fiber values | Depends on fiber grade, weave, resin, and laminate design | Finished composite density depends on fiber, resin, and fiber volume fraction | Weave improves handling and provides fibers in multiple directions, but crimp in the yarns can reduce stiffness and strength compared with straight, aligned fibers. | Panels and shaped parts where handling, drape, and multidirectional reinforcement are useful. |
| Unidirectional carbon-fiber reinforcement | Depends on the fiber grade; highest laminate stiffness is generally along the aligned fiber direction | Depends on fiber grade, resin, fiber volume fraction, and loading direction | Finished composite density depends on the full laminate system | Fibers are aligned mainly in one direction, giving efficient directional strength and stiffness. Additional plies may be needed to support loads in other directions. | Engineered structures with known load paths, such as beams, spars, and selectively reinforced panels. |