Thornel T-300 (Amoco) carbon fibre (3,000-filament tow) in an F652 (Hexcel) bismaleimide matrix, supplied as 8-harness satin weave. Carbon/BMI extends carbon/epoxy to sustained service around 350-450 °F, well beyond epoxy's limit, while processing in broadly similar tooling. It is used for engine nacelles and nozzles, structure near exhaust, and supersonic-aircraft skins subject to aerodynamic heating.
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 | |
|---|---|---|---|---|---|
Interlaminar Shear Strength(ILSS)2 entries | 41.16 range 35.37–45.78n=15, 1 batches, CV 8.17% | MPa | 21°C · RTA · 13-axis · [0:f]:10 · as-measured | ||
| ↳ | 31.65 range 29.58–33.23n=15, 1 batches, CV 3.6% | MPa | 316°C · ETA · 13-axis · [0:f]:10 · as-measured | ||
Ultimate Tensile Strength(σUTS)2 entries | 507.5 range 405.4–581.2n=15, 1 batches, CV 10.1% | MPa | 21°C · RTA · 1-axis · [0:f]:10 · batch_fiber_volume | ||
| ↳ | 579.2 range 462.6–662.6n=15, 1 batches, CV 10% | MPa | 21°C · RTA · 1-axis · [0:f]:10 · as-measured | ||
Young's Modulus(E)2 entries | 66.95 range 61.64–70.33n=15, 1 batches, CV 4.36% | GPa | 21°C · RTA · 1-axis · [0:f]:10 · batch_fiber_volume | ||
| ↳ | 76.53 range 70.33–79.98n=15, 1 batches, CV 4.28% | GPa | 21°C · RTA · 1-axis · [0:f]:10 · as-measured |