Ti-6Al-4V (Grade 5)
The most used titanium alloy: annealed Rm 895 MPa, Rp0.2 828 MPa at 4.4 g/cm³ — steel-like strength at 56 % of its weight.
Alpha-beta alloy for aircraft structures, engine parts, fasteners, pressure vessels and implants. Can be solution treated and aged for more strength in thin sections. Retains its properties up to about 350 °C.
- 0.2 % proof strength Rp0.2
- ≥ 828 MPa1guaranteed minimum · annealed, sheet and plate 0.025–1.000 in; also ASTM B348 bars < 3 in
- Tensile strength Rm
- ≥ 895 MPa1guaranteed minimum · annealed, sheet and plate 0.025–1.000 in; also ASTM B348 bars < 3 in
- Elongation after fracture A
- ≥ 10 %1guaranteed minimum · annealed
- Modulus of elasticity E
- 107 000–122 000 MPa1guaranteed range
How we know these values · 19 values from 2 sources
- Single source
- 19
- Disagreements explained
- 3
- Click any value under “All values” to see the sources that state it, with dates.
- 3 disagreements between sources, each explained under its value.
- How we rate evidence
What to watch
- Sources disagree on density; the reason is given under the value.
- Not yet sourced: Solution treated and aged minimums (Mil-T-9047) as separate values.
All values
- Identity and composition 7
- Mechanical 7
- Physical 1
- Thermal 3
- Electrical and magnetic 1
- Chemical and durability not yet
Mechanical
Elastic
Modulus of elasticity E
Young's modulus for design.
| Condition | Value | Evidence |
|---|---|---|
| 107 000–122 000MPa | Single source |
Shear modulus G
G = E / 2(1 + ν).
| Condition | Value | Evidence |
|---|---|---|
| 41 000–45 000MPa | Single source |
Poisson's ratio ν
In the elastic range.
| Condition | Value | Evidence |
|---|---|---|
| ≈ 0.31typical | Single source |
Strength
0.2 % proof strength Rp0.2
Minimum 0.2 % proof strength.
| Condition | Value | Evidence |
|---|---|---|
| ≥ 828MPa | Single source |
Tensile strength Rm
Ultimate tensile strength. Product standards give a range or a minimum.
| Condition | Value | Evidence |
|---|---|---|
| ≥ 895MPa | Single source |
Ductility
Elongation after fracture A
Minimum elongation; depends on gauge length and test direction.
| Condition | Value | Evidence |
|---|---|---|
| ≥ 10% | Single source |
Reduction of area Z
Minimum necking at fracture of a tensile test piece, relative to its cross-section.
| Condition | Value | Evidence |
|---|---|---|
| ≥ 25% | Single source |
Physical
Density ρ
Mass per unit volume.
| Condition | Value | Evidence |
|---|---|---|
| 4 420kg/m³ | Single source1 |
Thermal
Coefficient of thermal expansion α
Linear, near room temperature.
| Condition | Value | Evidence |
|---|---|---|
| ≈ 9×10⁻⁶ /Ktypical | Single source |
Specific heat capacity cp
Heat needed to warm 1 kg by 1 K.
| Condition | Value | Evidence |
|---|---|---|
| ≈ 580J/(kg·K)typical | Single source1 |
Thermal conductivity λ
Heat flow through 1 m of material per kelvin of temperature difference.
| Condition | Value | Evidence |
|---|---|---|
| ≈ 6.6W/(m·K)typical | Single source |
Electrical and magnetic
Electrical resistivity ρe
Resistance of a 1 m cube between opposite faces.
| Condition | Value | Evidence |
|---|---|---|
| ≈ 1.68 × 10⁻⁶Ω·mtypical | Single source1 |
Chemical composition
Show on the periodic tableASTM Grade 5, %
| Element | Applies to | Range % | Evidence |
|---|---|---|---|
| Al | all thicknesses | 5.5–6.75 | Single source |
| V | all thicknesses | 3.5–4.5 | Single source |
| Fe | all thicknesses | 0.40 | Single source |
| O | all thicknesses | 0.20 | Single source |
| C | all thicknesses | 0.080 | Single source |
| N | all thicknesses | 0.050 | Single source |
| H | all thicknesses | 0.015 | Single source |
Zapp lists Fe ≤ 0.30 % (DIN 3.7165). ELI (Grade 23) has O ≤ 0.13 %.
Compare side by side
With any other gradeSources here are public pages that reproduce ASTM B265. For design and acceptance, the standard edition named in your specification and the inspection certificate (EN 10204 3.1) of the delivered product take precedence. Design factors are recommended values; your National Annex may set others.