Engineered laminate of AW193P plain weave, stacked [0:f/90:f/+-45:f]:s. Properties here are laminate-level effective values in the laminate's own axes — not the lamina constants, which live on the parent prepreg (AW193P plain weave — AS4 carbon/3501-6). From MIL-HDBK-17-2F Volume 2 (US Government work, public domain).
Compliance & Regulations
Fiber Direction
Ply Schedule
Laminate Code
[0/90/45/-45/-45/45/90/0]s
Fiber angles relative to the 0° reference direction (red arrow in 3D view). 0° = longitudinal, 90° = transverse, ±45° = shear paths.
1 interactive curve for this material
Stress-strain, S-N fatigue and environmental knockdown curves are free with an account.
Create free account| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Compressive Modulus(Ec) | 9,200 range 8,500–9,800n=15, 3 batches, CV 3.4% | ksi | 24°C · RTA · 1-axis · [0:f]:14 · norm. thk+Vf | ||
Compressive Strength(σc) | 130 range 115–140n=15, 3 batches, CV 6.45% | ksi | 24°C · RTA · 1-axis · [0:f]:14 · norm. thk+Vf | ||
Interlaminar Shear Strength(ILSS) | 10.90 range 9.700–11.90n=15, 3 batches, CV 6.09% | ksi | 24°C · RTA · 13-axis · [0:f]:14 · as-measured | ||
Ultimate Tensile Strength(σUTS) | 68.50 range 62.00–75.10n=9, 3 batches, CV 7.6% | ksi | 24°C · RTA · x-axis · [0:f/90:f/+-45:f]:s · as-measured | ||
Young's Modulus(E) | Curve (3 pts) | ksi | CTA · 1-axis · [0:f]:8 · norm. thk+Vf |