Buy Nickel 600 & Alloys 625, 718 & X750

NICKEL 600ALLOY 625ALLOY 718ALLOY X750

High Temperature and Corrosion Resistant Nickel Alloys

Are you looking for a metal alloy supplier that offers quality products with fast turn around times at competitive prices? If so, you’ve come to the right place. Our products, including Nickel 600 and Alloys 625, 718, and X750 are stored and pulled directly from warehouses on the east and west coasts. All the alloys featured below are high temperature/corrosion resistant alloys that are often used in the aerospace industry. Nickel 600 is corrosion and heat resistant. Some of its applications include: vegetable vessels, phenol condensers, mufflers, and furnace trays. Aside from being used in the aerospace industry, it’s used extensively in the chemical industry. Nickel 600 is reliable in standing up to chlorine ion stress corrosion cracking and ammonia, just to name two characteristics.



NOMINAL DATA SHEET


CHEMICAL COMPOSITION
TYPICAL APPLICATIONS
C - .15 max
Furnace Muffles
Mn - 1.00 max
Electronic & Electrical
S - .015 max
Components
Si - .50 max
Jet Engine Parts
Cr - 14/17
Springs
Ni - 72.0
Chemical & Food
Cu - .50 max
Processing Equipment
Fe - 6/10
Bellows
Al - .35 max
Ti - .50 max
Cb+Ta - 1.0 max
Co - 1.0 max


PHYSICAL PROPERTIES(ANNEALED CONDITION)
Modulus of Elasticity, Tension 10(******)psi - 31.0
Magnetic permeability at 200H(At 70 F) - 1.010
Electrical Resistivity, Microhm-cm(At 70 F) - 103
Density,lb/cu.in. - .304
Coefficient of Thermal Expansion, in./in./ F x 10(-******)
70 - 200 F ............................ 7.4
70 - 400 F ............................ 7.7
70 - 800 F ............................ 8.1
70 - 1000 F ........................... 8.4


NOMINAL MECHANICAL PROPERTIES(ANNEALED CONDITION)
Ultimate Tensile Strength,psi - 90,000
0.2% Offset Yield Strength,psi - 31,000
Elongation in 2 inches percent - 40
Hardness, Rockwell - B65
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Alloy 625 is strong at high and low temperatures. Unlike some of its nickel-based counterparts, it has good weldability. In addition to being used in the aerospace industry, it’s used in the marine industry. Because of the properties it contains, it’s useful in seawater applications, thus being applied to exhaust ducts for Navy utility boats, submarine auxiliary propulsion motors, undersea communication cables, and much more.

NOMINAL DATA SHEET

CHEMICAL COMPOSITION
TYPICAL APPLICATIONS
Cu - .10 max Al - .40 max
Ducting Systems
Mn - .50 max Ti - .40 max
Springs
P - 0.15 max Cb+Ta - 3.15/4.15
Fuel Nozzles
S - 0.15 max Co - 1.0 max
Jet Engine Parts
Si - .50 max
Honeycomb
Cr - 20/23
 
Ni - Balance  
Mo - 8/10  
Fe - 5.0 max  



NOMINAL MECHANICAL PROPERTIES(ANNEALED CONDITION)
Ultimate Tensile Strength,psi - 130,000
0.2% Offset Yield Strength,psi - 68,000
Elongation in 2 inches percent - 42
Hardness, Rockwell - B65
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Aircraft engineers depend on strong, temperature-capable alloys, and that’s why many of them depend on Alloy 718 for use in aircraft engines. It’s an alloy that has good weldability (like Alloy 625). Other applications include but are not limited to: high strength bolts, cryogenic storage tanks, and land-based turbines.

NOMINAL DATA SHEET

CHEMICAL COMPOSITION
TYPICAL APPLICATIONS
C - .08 max Fe - Balance
Jet Engine Parts
Mn - .35 max Al - .20/.80
Pump Parts
P - .015 max Ti - .65/1.15
Rocket Motors Casings
S - .015 max Cb+Ta - 4.75/5.50
Aerospace Components
Si - .35 max Co - 1.0 max
Nuclear Reactor Fuel
Cr - 17/21 B - .006max
Support Grids
Ni - 50/55  
Mo - 2.8/3.3  
Cu - .30  


PHYSICAL PROPERTIES(ANNEALED CONDITION) **
Modulus of Elasitcity, Tension 10(******)psi - 29.0
Magnetic permeability at 200H(At 70 F) - 1.001
Electrical Resistivity, Microhm-cm(At 70 F) - 121
Density,lb/cu.in. - .296
Coefficient of Thermal Expansion, in./in./ F x 10(-******)
70 - 200 F ............................ 7.2
70 - 400 F ............................ 7.8
70 - 800 F ............................ 8.1
70 - 1000 F ........................... 8.2
** (Aged)


NOMINAL MECHANICAL PROPERTIES(ANNEALED CONDITION)
Ultimate Tensile Strength,psi - 130,000
0.2% Offset Yield Strength,psi - 67,000
Elongation in 2 inches percent - 41
Hardness, Rockwell - B90
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Alloy X750 is similar to Nickel 600 but contains aluminum (less than 1%) and titanium (2.5%), thus, it’s made precipitation hardenable. In addition, it’s non-magnetic and can be worked both hot and cold. Alloy X750 is applied to rocket engines, aircraft structures, nuclear reactors, and others.

NOMINAL DATA SHEET

CHEMICAL COMPOSITION
TYPICAL APPLICATIONS
C - .08 max Al - .4/1.0 max
Vacuum Envelopes
Mn - .35 max Ti - 2.25/2.75 max
Bellows
P - .015 max Cb+ta - .7/1.2
Aircraft Sheet
S - .015 max Co - 1.0 max
Steam Service
Si - .35 max  
Springs
Cr - 14/17  
Ni - 70.0  
Cu - .50 max  
Fe - 5/9  


PHYSICAL PROPERTIES(ANNEALED CONDITION) **
Modulus of Elasitcity, Tension 10(******)psi - 31.0
Magnetic permeability at 200H(At 70 F) - 1.0035
Electrical Resistivity, Microhm-cm(At 70 F) - 122
Density,lb/cu.in. - .298
Coefficient of Thermal Expansion, in./in./ F x 10(-******)
70 - 200 F ............................ 7.0
70 - 400 F ............................ 7.1
70 - 800 F ............................ 7.8
70 - 1000 F ........................... 8.1
** (Aged)


NOMINAL MECHANICAL PROPERTIES(ANNEALED CONDITION)
Ultimate Tensile Strength,psi - 112,000
0.2% Offset Yield Strength,psi -46,000
Elongation in 2 inches percent - 45
Hardness, Rockwell - B80
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