Cupro - Nickel

HYMU 80

Kovar

Molybdenum 

Mumetal

Nickel 200 and  201

Nickel 400

Nickel 500

Nickel 600, 601, 625

Nickel 718 and X 750

Nickel Chrome

Nickel Silver 

Stainless 300 Series

Tantalum

Titanium 

Tungsten

Alloy 42 - F30

Invar 36

Alloy 45

Alloy 46

Alloy 47/50

Alloy 48 

Alloy 49

Alloy 52 

OFHC Copper

Nickel 600

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

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

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

Alloy 718

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

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

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)

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