HITEX 33 (Hitco) carbon fibre (6,000-filament tow) in an E7K8 (U.S. Polymeric) epoxy matrix, supplied as tape. Carbon/epoxy is the primary structural composite of modern aerospace: the highest stiffness-to-weight of the common systems, with well-characterised and predictable behaviour. It is used for wing and empennage skins, spars and ribs, fuselage panels and control surfaces — anywhere weight is the governing cost.
Compliance & Regulations
Fiber Direction
Ply Schedule
Laminate Code
[0/0/0/0/0/0/0/0/0/0]s
Fiber angles relative to the 0° reference direction (red arrow in 3D view). 0° = longitudinal, 90° = transverse, ±45° = shear paths.
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Compressive Modulus(Ec) | 103.4 – 129.6 | GPa | 8 entriesClick to expand | ||
Compressive Strength(σc) | 0.7446 – 1.751 | GPa | 8 entriesClick to expand | ||
Elongation at Break(εf)4 entries | 1.610 range 1.550–1.700 | - | -54°C · CTA · 1-axis · [0]:10 · as-measured · rec #405 | ||
| ↳ | 1.590 range 1.520–1.710 | - | 24°C · RTA · 1-axis · [0]:10 · as-measured · rec #401 | ||
| ↳ | 1.260 range 1.200–1.340 | - | 24°C · RTA · 1-axis · [0]:10 · as-measured · rec #421 | ||
| ↳ | 1.360 range 1.360–1.370 | - | -54°C · CTA · 1-axis · [0]:10 · as-measured · rec #425 | ||
Poisson's Ratio(ν)3 entries | 0.3100 n=5, 1 batches | - | 24°C · RTA · 12-axis · [0]:10 · as-measured | ||
| ↳ | 0.3100 n=5, 1 batches | - | 24°C · RTW · 12-axis · [0]:10 · as-measured | ||
| ↳ | 0.3000 n=5, 1 batches | - | 82°C · ETW · 12-axis · [0]:10 · as-measured | ||
Ultimate Shear Strength(Fsu)4 entries | 103.4 range 93.08–108.9n=20, 1 batches, CV 3.52% | MPa | 24°C · RTA · 12-axis · [(+-45):2/45]:s · as-measured | ||
| ↳ | 91.01 range 90.32–91.70n=5, 1 batches, CV 0.655% | MPa | 82°C · ETA · 12-axis · [(+-45):2/45]:s · as-measured | ||
| ↳ | 112.4 range 108.9–115.1n=5, 1 batches, CV 2.2% | MPa | 24°C · RTW · 12-axis · [(+-45):2/45]:s · as-measured | ||
| ↳ | 80.67 range 79.29–82.05n=5, 1 batches, CV 1.27% | MPa | 82°C · ETW · 12-axis · [(+-45):2/45]:s · as-measured | ||
Ultimate Tensile Strength(σUTS) | 0.03847 – 2.379 | GPa | 9 entriesClick to expand | ||
Young's Modulus(E) | 8.481 – 134.4 | GPa | 9 entriesClick to expand | ||