Materials
Compare Materials
Compare candidate materials with unit-aware values and condition metadata.
| Property |
Aluminum 2219-T6 die forging (NASA historical reference)
2219-T6 die forging; NASA historical minimums | die forging or separately forged test bar
|
|---|---|
| Density |
2824 kg/m^3
Density
Nominal
Room-temperature value converted from 0.102 lb/in^3.
|
| 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 |
Not listed
Not listed for this material record, condition, or selected unit system.
|
| Shear modulus |
Not listed
Not listed for this material record, condition, or selected unit system.
|
| Poisson's ratio |
Not listed
Not listed for this material record, condition, or selected unit system.
|
| Yield strength |
262.001 MPa
Tensile yield strength
Historical Specified Minimum
T6 die forging, orientation A, maximum 4 in section; converted from 38.0 ksi.
|
| Tensile strength |
399.896 MPa
Ultimate tensile strength
Historical Specified Minimum
T6 die forging, orientation A, maximum 4 in section; converted from 58.0 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.
|