Rene 41® Nickel Superalloy, Heat Treatment: 1079°C (1975°F) + Age
Subcategory: Superalloy; Nickel Base
Key Words: Allvac, an Allegheny Teledyne Company, UNS N07041; AMS 5712, 5713; René 41 Nickel
Material Notes: Nickel content calculated as remainder. Data provided by Allvac. Applications: Jet and rocket engines, torque rings, afterburners, and hardware; space shuttle turbo pumps seals.
Available Properties |
- Density
- Hardness, Brinell
- Hardness, Knoop
- Hardness, Rockwell C
- Hardness, Vickers
- Tensile Strength, Ultimate
- Tensile Strength, Yield
- Elongation at Break
- Reduction of Area
|
|
|
|
Property Data |
This page displays only the text
of a material data sheet.
To see MatWeb's complete data
sheet for this material (including
material property data, metal
compositions, material suppliers,
etc), please click the button below. |
|
|
|
|