Style 3405 glass fabric (S1014 yarn) in an F-161 epoxy matrix. Glass/epoxy is the workhorse of secondary aircraft structure and tooling: far cheaper than carbon, electrically transparent, and tolerant of impact and handling damage. It is chosen where stiffness-per-pound is not the governing requirement — radomes and antenna windows, fairings and access panels, lay-up tooling, and marine and industrial laminates. The handbook characterises it from -65 °F to 450 °F, consistent with elevated-temperature service. MatWorld carries 65 tensile, compressive and shear curves for this system, digitised from MIL-HDBK-17-2F Volume 2 (US Government work, public domain).
Compliance & Regulations
Fiber Direction
Ply Schedule
Laminate Code
[0/0/0/0/0/0/0/0/0/0/0/0]s
Fiber angles relative to the 0° reference direction (red arrow in 3D view). 0° = longitudinal, 90° = transverse, ±45° = shear paths.
65 interactive curves 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 | |
|---|---|---|---|---|---|
Poisson's Ratio(ν)2 entries | Curve (14 pts) | - | 24°C · RTA · 12-axis · Balanced Laminate [0:12] · Balanced Laminate [0:12] | ||
| ↳ | Curve (10 pts) | - | 24°C · RTA · 21-axis · Balanced Laminate [0:12] · Balanced Laminate [0:12] | ||
Stress–Strain Curve(σ–ε) | — | ksi | 63 entriesClick to expand | ||