Product Details, Specifications, and Technical Information
Alloy 625 is a nickel-chromium-molybdenum alloy known for its excellent strength, corrosion resistance, and high-temperature performance. It is highly resistant to oxidation, pitting, and crevice corrosion, making it ideal for use in extreme environments like aerospace, marine, and chemical processing industries. The alloy maintains its mechanical properties in both high and low temperatures, providing exceptional fatigue and thermal resistance. Alloy 625 is commonly used in components like turbine engines, exhaust systems, and pressure vessels due to its durability and reliability under harsh conditions.
Dimension Name | Specification |
Alloy | 625 |
DFAR | true |
Brand | Arbor Metals |
Material | Nickel |
Shape | Sheet/Plate |
Domestic | false |
Weight/Lineal Foot | ||
17.28 pounds |
Please note that this data is to be used ONLY FOR REFERENCE, NOT FOR DESIGN, and by using it,you agree that any decisions you make regarding materials for your project are at your own discretion.
Mechanical Properties | |
Property | Value |
Yield Tensile Strength KSI | 67 |
Ultimate Tensile Strength KSI | 128 |
Brinell Hardness 500 kg load | 102 |
Density g/cm^3 | 8 |
Elongation % in 2 in. | 33 |
Rockwell Hardness B Scale | 65 |
Melting Point °F | 2350 - 2460 |
Machinability % | 22 |
Electrical Conductivity % IACS | 1 |
Shear Strength KSI | 87 |
Chemistry Information: 625 Nickel | |
Element | Percentage |
C | 0.1 max |
Mn | 0.5 max |
P | 0.015 max |
S | 0.015 max |
Si | 0.05 max |
Cr | 20 - 23 |
Ni | - |
Mo | 8 - 10 |
Nb | 3.15 - 4.15 |
Ti | 0.4 max |
Al | 0.4 max |
Fe | 5 max |
Ta | 0.05 max |