|
NICKEL
600
|
|
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
|
|
Alloy
625
|
|
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
|
|
Alloy
718
|
|
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
|
|
Alloy
X750
|
|
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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[TOP]
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