Engineered laminate of 5505, stacked [(0/90):2]S. Properties here are laminate-level effective values in the laminate's own axes — not the lamina constants, which live on the parent prepreg (5505 — boron fibre / epoxy). From MIL-HDBK-17-2F Volume 2 (US Government work, public domain).
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20 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)3 entries | Curve (5 pts) | - | -55°C · CTA · 12-axis · Laminate [(0/90):2]S (0 deg - 90 deg Crossply, 6 plies total) · Laminate [(0/90):2]S (0 deg - 90 deg Crossply, 6 plies total) | ||
| ↳ | Curve (3 pts) | - | 24°C · RTA · 12-axis · Laminate [(0/90):2]S (0 deg - 90 deg Crossply, 6 plies total) · Laminate [(0/90):2]S (0 deg - 90 deg Crossply, 6 plies total) | ||
| ↳ | Curve (4 pts) | - | 127°C · ETA · 12-axis · Laminate [(0/90):2]S (0 deg - 90 deg Crossply, 6 plies total) · Laminate [(0/90):2]S (0 deg - 90 deg Crossply, 6 plies total) | ||
Stress–Strain Curve(σ–ε) | — | ksi | 17 entriesClick to expand | ||