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Nickel coating

Aeronautics

Base

Material

Chemical

composition

in %

Density

g/cm3

lb/in3

Resistivity

@ 20°C µΩ.cm

Ω cmil/ft

Tensile Strength

Solid wire

mm

awg

Stranded

mm²

awg

Bobbins

hard

daN/mm²

psi

soft

daN/mm²

psi

ETP Copper Cu 99.9 %

8,93

.323

class2 :

1,796 / 10.803

class4 :

1,834 / 11.033

class7 :

1,894 / 11.397

45

65,000

24

35,000

0,040-2,050

12 to 46

0,005-13,24

6 to 40

 
OF Copper Cu 99.95 % O2 15ppm

8,93

.323

45

65,000

24

35,000

12 to 46

0,005-13,24

6 to 40

 
Cuprofor® (Cd free) P 0.08% Co 0.28 % Cu Reste

8,93

.323

2,300 / 13.836

65

94,000

40

58,000

0,050-0,800

20 to 44

0,005-13,24

6 to 40

 
Green6 TM (RoHS) Cu 99% Mg 1%

8,93

.323

2,155 / 12.964

65

94,000

40

58,000

0,030-0,800

20 to 48

0,005-13,24

6 to 40

 
Copper Clad Aluminum (CCA) Cu 15% of the total weight depends on Ni Thickness 2,676 / 16.096

20

29,000

14

20,000

0,100-2,450

10 to 38

0,20 - 21

4 to 24

-
Copper Clad Steel 40% IACS Cu thickness 10% of the wire radius

8,13

.294

4,397 / 26.470

75,8

110,000

34,5

50,000

0,080-0,800

20 to 40

0,020-13,24

6 to 34

-
Bronze 6 Sn 6 % P 0.15 % Cu Balance

8,85

.320

11,90 / 71.586

100

145,000

44

64,000

0,080-0,800

20 to 40

- -


All data given in these tables should be considered as typical or average. Variations in properties can occur.