Materials
Compare Materials
Compare candidate materials with unit-aware values and condition metadata.
| Property |
Titanium 6Al-4V annealed sheet (NASA historical reference)
Ti-6Al-4V annealed 0.060 in sheet; historical room-temperature observation | sheet
|
|---|---|
| Density |
4424 kg/m^3
Density
Nominal
Room temperature.
|
| Thermal conductivity |
Not listed
Not listed for this material record, condition, or selected unit system.
|
| Specific heat capacity |
Not listed
Not listed for this material record, condition, or selected unit system.
|
| Young's modulus |
110.316 GPa
Young's modulus
Historical Design Reference
Handbook design value for all forms; converted from 16.0 x 10^3 ksi.
|
| Shear modulus |
42.747 GPa
Shear modulus
Historical Design Reference
Handbook design value for all forms; converted from 6.2 x 10^3 ksi.
|
| Poisson's ratio |
0.342 -
Poisson's ratio
Nominal
Handbook alloy reference.
|
| Yield strength |
972.161 MPa
Tensile yield strength
Historical Test Value
Annealed 0.060 in sheet at 21 degC; converted from 141 ksi.
|
| Tensile strength |
1041.108 MPa
Ultimate tensile strength
Historical Test Value
Annealed 0.060 in sheet at 21 degC; converted from 151 ksi.
|
| Elongation at break |
Not listed
Not listed for this material record, condition, or selected unit system.
|
| Maximum service temperature |
Not listed
Not listed for this material record, condition, or selected unit system.
|