Metal
INCONEL alloy 718 annealed and aged sheet (NASA historical reference)
Historical AMS minimum tensile requirements for annealed-and-aged alloy 718 sheet, strip, and plate plus selected handbook physical data.
Properties
Physical
| Property | Value | Unit |
|---|---|---|
| Density | 8210 | kg/m^3 |
Thermal
| Property | Value | Unit |
|---|---|---|
| Specific heat capacity | 435.136 | J/kg/K |
Mechanical
| Property | Value | Unit |
|---|---|---|
| Ultimate tensile strength | 1241.056 | MPa |
| Tensile yield strength | 1034.214 | MPa |
| Elongation | 12 | % |
| Rockwell hardness | 36 | HRC |
Units
Condition
- Condition
- Alloy 718 after 1750 degF (954 degC) anneal plus aging; historical AMS minimums
- Temper
- annealed and aged
- Heat treatment
- 1750 degF (954 degC) anneal plus aging; detailed aging schedule is in the cited handbook specification context
- Product form
- sheet, strip, and plate
- Thickness / diameter range
- room-temperature column applies to the listed sheet, strip, and plate product
- Test direction
- not stated in the cited table
- Processing route
- wrought nickel-base alloy sheet, strip, or plate
- Temperature range
- 21 ... 21 degC
- Notes
- Historical reference data transcribed with the stated property semantics and SI conversions. Confirm against the official PDF, a current procurement specification, the actual product form and thickness, and a material test report before engineering use.
Standards
No material standards linked.
Record status
- Category
- Metal
- Unit system
- Common SI