5456 Aluminum O
Verifiedmetal5456-O is an aluminum-magnesium alloy (nominally 5% Mg) in the fully annealed condition, providing excellent corrosion resistance in marine and seawater environments with moderate strength suitable for welded structures and pressure vessels. The O temper offers maximum ductility and elongation at break, making it ideal for applications requiring formability and weldability over strength, with availability in extruded and rolled forms per aerospace specifications AMS-QQ-A-200/7 and AMS-QQ-A-250/9.
aerospacestructural
Compliance & Regulations
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Specification
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Ultimate Bearing Strength(Fbru)2 entries | — | ksi | 22°C · Sheet/Plate · O · AMS-QQ-A-250/9 · t=0.051-1.500 in · e/D=1.5 | — | |
| ↳ | — | ksi | 22°C · Sheet/Plate · O · AMS-QQ-A-250/9 · t=0.051-1.500 in · e/D=2 | — | |
Bearing Yield Strength(Fbry) | — | ksi | 22°C · Sheet/Plate · O · AMS-QQ-A-250/9 · t=0.051-1.500 in · e/D=1.5 | — | |
Compressive Modulus(Ec) | Curve (19 pts) | ksi | — | — | |
Compressive Tangent Modulus vs Stress(Etn(σ))4 entries | Curve (11 pts) | ksi | 21°C · L | — | |
| ↳ | Curve (11 pts) | ksi | 21°C · LT | — | |
| ↳ | Curve (13 pts) | ksi | 21°C · L | — | |
| ↳ | Curve (13 pts) | ksi | 21°C · LT | — | |
Compressive Yield Strength(Fcy)4 entries | — | ksi | 22°C · Sheet/Plate · O · AMS-QQ-A-250/9 · L · t=0.051-1.500 in | — | |
| ↳ | — | ksi | 22°C · Sheet/Plate · O · AMS-QQ-A-250/9 · LT · t=0.051-1.500 in | — | |
| ↳ | — | ksi | 22°C · Sheet/Plate · O · AMS-QQ-A-250/9 · ST · t=0.051-1.500 in | — | |
| ↳ | — | ksi | 22°C · Bar/Extrusion/Rod · O · AMS-QQ-A-200/7 · L · t=≤5.000 in | — | |
Elongation at Break(εf) | — | - | 6 entriesClick to expand | ||
Poisson's Ratio(ν) | — | - | 22°C | — | |
Shear Modulus(G) | — | ksi | 22°C · Sheet/Plate | — | |
Ultimate Shear Strength(Fsu) | — | ksi | 22°C · Sheet/Plate · O · AMS-QQ-A-250/9 · t=0.051-1.500 in | — | |
Stress–Strain Curve (buckling region, ≤ 2% strain)(σ–ε (low-strain)) | — | ksi | 8 entriesClick to expand | ||
Ultimate Tensile Strength(σUTS) | — | ksi | 7 entriesClick to expand | ||
Yield Strength (0.2% offset)(σy) | — | ksi | 7 entriesClick to expand | ||
Young's Modulus(E) | — | ksi | 22°C · Sheet/Plate | — | |
N entriesMultiple entries per property — large groups are collapsed; click a summary row to expand. Use filters above to narrow by form / heat treatment / basis.
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
CTE vs Temperature(α(T))2 entries | Curve (10 pts) | µin/in·°F | — | — | |
| ↳ | Curve (10 pts) | µin/in·°F | — | — | |
Thermal Conductivity vs Temperature(k(T)) | Curve (20 pts) | BTU/(hr·ft·°F) | — | — |
N entriesMultiple entries per property — large groups are collapsed; click a summary row to expand. Use filters above to narrow by form / heat treatment / basis.
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | — | lb/in³ | 22°C | — |
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
Regulatory Screening
Environmental
Safety & Biocompatibility
Quality & Standards
RoHS, REACH, and Prop 65 statuses are validated against official substance lists (ECHA SVHC Candidate List, OEHHA Prop 65, RoHS Annex II). Other regulations are estimated from composition and material classification. All screening is a starting point for due diligence — always verify with your supplier before making compliance decisions.