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ALLOY 625
| ALLOY 718 | ALLOY X750 | SHEET
| COIL/FOIL | ROD | PRODUCTS
NOMINAL DATA SHEET
|
|
| C - .15max |
Ti - .50max |
Furnace Muffles |
| Mn - 1.00max |
Cb+Ta - 1.0max |
Electronic and Electrical
Components |
| S - .015max |
Co - 1.0max |
Jet Engine Parts |
| Si - .50max |
|
Springs |
| Cr - 14/17 |
|
Chemical and Food |
| Ni - 72.0 |
|
Processing Equipment |
| Cu - .50max |
|
Bellows |
| Fe - 6/10 |
|
|
| Al - .35max |
|
|
| |
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| 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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NOMINAL DATA SHEET
|
|
| Cu - .10max |
Al - .40max |
Ducting Systems |
| Mn - .50max |
Ti - .40max |
Springs |
| P - 0.15max |
Cb+Ta - 3.15/4.15 |
Fuel Nozzles |
| S - 0.15max |
Co - 1.0max |
Jet Engine Parts |
| Si - .50max |
|
Honeycomb |
| Cr - 20/23 |
|
|
| Ni - Balance |
|
|
| Mo - 8/10 |
|
|
| Fe - 5.0max |
|
|
| |
| PHYSICAL
PROPERTIES (ANNEALED CONDITION) |
| Modulus of Elasticity, Tension
10(******)psi - 30.0 |
| Magnetic permeability at
200H(At 70 F) - 1.001 |
| Electrical Resistivity,
Microhm-cm (At 70 F) - 129 |
| Density, lb/cu.in. - .305 |
| Coefficient of Thermal
Expansion, in./in./ F x 10(-******) |
| 70 - 200 F ............................
7.1 |
| 70 - 400 F ............................
7.3 |
| 70 - 800 F ............................
7.6 |
| 70 - 1000 F ...........................
7.8 |
| |
| |
| 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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NOMINAL DATA SHEET
|
|
| C - .08max |
Fe - Balance |
Jet Engine Parts |
| Mn - .35max |
Al - .20/.80 |
Pump Parts |
| P - .015max |
Ti - .65/1.15 |
Rocket Motors Casings |
| S - .015max |
Cb+Ta - 4.75/5.50 |
Aerospace Components |
| Si - .35max |
Co - 1.0max |
Nuclear Reactor Fuel |
| Cr - 17/21 |
B - .006max |
Support Grids |
| Ni - 50/55 |
|
|
| Mo - 2.8/3.3 |
|
|
| Cu - .30 |
|
|
| |
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| 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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NOMINAL DATA SHEET
|
|
| C - .08max |
Al - .4/1.0max |
Vacuum Envelopes |
| Mn - .35max |
Ti - 2.25/2.75max |
Bellows |
| P - .015max |
Cb+Ta - .7/1.2 |
Aircraft Sheet |
| S - .015max |
Co - 1.0max |
Steam Service |
| Si - .35max |
|
Springs |
| Cr - 14/17 |
|
|
| Ni - 70.0 |
|
|
| Cu - .50max |
|
|
| 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) |
| |
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| 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 |
| |
|
NICKELS 600/601/625/718/750 |
| SHEET |
COIL/FOIL |
ROD |
.050
.062
.078
.109
.125
.140
.250
.375
.500
.750
1.00 |
.003
.004
.005
.010
.015
.020
.030
.040
.050
.062 |
.125
.250
.312
.437
.500
.625
.750
.875
1.00
1.25
1.50
1.75
2.00
2.25
2.50
3.00
3.50
4.00
5.00
5.50
6.00 |
*NOTE: Other sizes available upon request.
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Disclaimer
Every
effort is made to ensure that technical specifications are accurate.
However, technical specifications included herein should be used as a
guideline only. All specifications are subject to change without notice.
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