Alloys & Metals
With Global Distribution

special alloys

STAINLESS
STEELS

tungsten
alloys

complex nickel
alloys

Magnet
alloys

zirconium
alloys

nickel
alloys

high speed
steels

cobalt
alloys

TOOL
STEELS

nickel iron
alloys

titanium
alloys

STAINLESS STEELS

*Indicates maximum
The figures shown are nominal compositions of the various alloys.
Duplex 5.5 22.5 - 3 - BAL - - - - 0.17 N2
AISI 302 (EN58) 9 18 - - - BAL - - - - 0.15 C
AISI 304 9 18 - - - BAL - - - - 0.08* C
AISI 309 12.5 22.5 - - - BAL - - - - 0.20* C
AISI 316 10.5 17 - 2 - BAL - - - - 0.08* C
AISI 317 13 19 - 3.5 - BAL - - - - 0.08* C
AISI 321 (EN58B) 9 18 - - - BAL - 5xC - - 0.08* C
AISI 347/348 (EN58F,G) 10 18 - - - BAL - - - 8xC 0.08* C
AISI 409 0.7* 12 - - - BAL 0.5 0.5 - - 0.09* C
AISI 420 (EN56/S62) 1.0* 13 - 13 - BAL - - - 1.8 0.32* C
AISI 430 (FI 17) 0.5* 17 - - - BAL - - - - 0.12* C
AISI 431 (EN57/S80) 2 16 - - - BAL - - - - 0.20* C
Crown Min 12.5 22.5 - - 1 BAL - - - - 0.20* C
Crown Max 12.5 22.5 - - 2.75 BAL - - - - 0.20* C
17-4 PH 4 16.5 - - - BAL - - 3.5 0.3 0.03 C
17-7 PH 7 17 - - - BAL 1 1 - - 0.05 C
FV 520 (B) 5 14.5 - 1.6 1.6 BAL - - 1.8 0.4 0.05 C
FV 535 0.3 10.5 2.6* 0.75 0.75 BAL - - - 0.4 0.07* C
Rex 448 0.75 11.5 - 0.45 0.45 BAL - - - 0.45 0.15* C
Jethete M152 2.5 12 - 1.8 1.8 BAL - - - - 0.1 C
Jethete M190 2.7 12 1.55 1.8 1.8 BAL - - - - 0.13 C
G18B 13 13 10 1.7 2.5 BAL - - - 3 0.4 C
Ferralium 5.35 24.2 - 2.5 - BAL - - 1.6 -
Kanthal 22.5 2.0* - - BAL 5.5 5.5 - -

TUNGSTEN ALLOYS

*Indicates maximum
The figures shown are nominal compositions of the various alloys.
Mallory 1000 - - 6 BAL - - - - 4 -
Heavy Metal - - 3 BAL - - - - 7 -
Tungsten Carbide S2 6 - - BAL - 7 - - - 8.0 TiC
Tungsten Carbide S3 8.5 - - BAL - 5 - - - -
Tungsten Carbide D2 10 - - BAL - 5 - - - -
Tungsten Carbide 78B 9 - - BAL - 6 - - - 8.0 TiC
Tungsten Carbide 78 8 - - BAL - 6 - - - 4.0 TaC 12.0TiC
Tungsten Carbide 350 4.5 - - BAL - 6 - - - 12.2 TaC 12.2 TiC
Tungsten Carbide 370 8.5 - - BAL - 6 - - - 8.0 TaC 11.5 TiC
AISI 430 (FI 17) 0.5* 17 - - - BAL - - - - 0.12* C
AISI 431 (EN57/S80) 2 16 - - - BAL - - - - 0.20* C
Crown Min 12.5 22.5 - - 1 BAL - - - - 0.20* C
Crown Max 12.5 22.5 - - 2.75 BAL - - - - 0.20* C
17-4 PH 4 16.5 - - - BAL - - 3.5 0.3 0.03 C
17-7 PH 7 17 - - - BAL 1 1 - - 0.05 C
FV 520 (B) 5 14.5 - 1.6 1.6 BAL - - 1.8 0.4 0.05 C
FV 535 0.3 10.5 2.6* 0.75 0.75 BAL - - - 0.4 0.07* C
Rex 448 0.75 11.5 - 0.45 0.45 BAL - - - 0.45 0.15* C
Jethete M152 2.5 12 - 1.8 1.8 BAL - - - - 0.1 C
Jethete M190 2.7 12 1.55 1.8 1.8 BAL - - - - 0.13 C
G18B 13 13 10 1.7 2.5 BAL - - - 3 0.4 C
Ferralium 5.35 24.2 - 2.5 - BAL - - 1.6 -
Kanthal 22.5 2.0* - - BAL 5.5 5.5 - -

Complex Nickel Alloys

*Indicates maximum
The figures shown are nominal compositions of the various alloys.
C242 56 21.5 10 10.5 - 0.75* 0.2* 0.3* - - -
C263 50 20 20 5.9 - 0.75* 0.5 2.2 - - -
C1023 56 15.5 9.5 8 - 0.25 4.3 3.6 - - -
Incoloy 903 38 1.0* 15 - - BAL 0.7 1 - 3 -
Incoloy 907 38 1.0* 13 - - BAL 0.1 1.5 - 4.7 -
Incoloy 617 54 22 12.5 9 - - 1 - - - 0.07 C
Inconel 700 45 15 29 3 - 4 3.3 2.25 - - -
IN 100 (PK24) 60 10 15 3 - - 5.5 4.7 - - 1.0 V
IN-731 66 9.5 10 2.5 - 0.5 5.5 4.65 - - 0.95 V
IN-738 61 16 8.5 1.75 2.6 0.5 3.4 3.4 - 0.9 1.75 Ta
IN-792 61 12.7 9 2 3.9 - 3.2 4.2 - - 4.2 Ta
IN939 (Nimocast 739) 48 22.4 19 - 2 - 1.9 3.7 - 1 1.4 Ta
Incoloy 807 40 20 8 - 5 26 - - - 1 -
SRR99 65 8.6 5 - 9.5 0.1* 5.5 2.2 - - 2.8 Ta
Nimonic 90 57 20 16 - - 5.0* 1.5 2.5 - - -
Nimonic 91 47.5 28.5 20 - - - 1.2 2.3 - - -
Nimonic 105/108 53 15 20 5 - 1.0* 4.7 1.2 - - -
Nimonic 115/118 57 15 15 3.5 - 1.0* 5 4 - - -
Nimonic PK31 49 20 14 4.5 - 1 0.4 2.3 - 5 -
Nimonic PK33 56 19 14 7 - 0.5 2 2 - - -
GTD 111 59 14 9.5 1.5 3.8 0.5* 3 4.9 - - 2.8 Ta
GTD 222 50 22.5 19 - 2 0.25* 1.2 2.3 - 0.8 1.0 Ta
RA 333 45 25 3.5 3.5 3.5 18 - - 0.5 - -
Rene 41 52 19 11 10 - 5.0* 1.6 3.2 - - -
M252 54 19 10 10 - 5.0* 1 2.6 - - -
Thetalloy (PWA 651) 49 25 12.5 3 7 3 - - - - -
Waspaloy 56 19 14 4.2 - 1.5* 1.4 3 - - 0.1 Zr
Astraloy 56 15 15 5.25 - 0.2* 4.4 3.5 - - 0.03 B
Udimet 500 (PK25) 53 17.5 16.5 4 - 4.0* 2.9 3.9 - - 0.01 B
Udimet 520 56 19 12 6 1 1 2 3 - - -
Udimet 600 52 17.5 16.5 4 - 4.0* 4.2 2.9 - - 0.04* B
Udimet 700 (Rene 77) 52 15 15 4 - 0.5* 4.2 3.5 - - 0.02* B
Udimet 710 53 18 15 3 1.5 0.5* 2.5 5 - - 0.035 B
Udimet 720 53 18 15 3 1.4 0.5* 2.5 5 - - 0.045 B
MAR M-246 60 9 10 2.5 10 0.15 5.5 1.5 - - 1.5 Ta
Rene 80 60 14 9.5 4 4 - 3 5 - - -
Rene 88 55 16 13 4 4 0.25 2.1 3.75 - 0.7 0.02* B
B1900 (PWA 663) 64 8 10 6 - - 6 1 - - 1.0 Zr
B1914 66 10 10 3 - - 5.5 5.3 - - 0.1 B
B1925 61 12 8.5 1.8 4.5 - 3.5 4 - - 0.1 B
B1950 (MAR M-200) 60 9 10 - 12 - 5 2 - 1 0.12 B
B1964 59 9 10 1 8.5 - 3.5 5.3 - - 0.16 B
MAR M-002 59 10 10 - 10 1.0* 5 1.5 - - 2.5 Ta
MAR M-247 58 8.5 10 0.6 10 0.5* 5.5 1 - - 3.0 Ta
MARAGING 200 18 - 8.5 3.2 - BAL - 0.2 - - 0.03* C
MARAGING 250 18 - 8 5 - BAL - 0.4 - - 0.03* C
MARAGING 300 18.5 - 9 5 - BAL - 0.65 - - 0.03* C
MARAGING 350 18 - 11.5 5 - BAL - 1.35 - - 0.03* C

Magnet Alloys

*Indicates maximum
The figures shown are nominal compositions of the various alloys.
Alni 1 - - 24.5 BAL - - 6 12.5 - - -
Alnico 2 13 - 17 BAL - - 6 10 - 0.1 -
Alnico 5 24 - 14 BAL - - 3 8 - - -
Alnico 8 35 - 15 BAL - - 4 7.5 - - 5.0 Ti
Alcomax 2 21 - 11 BAL - - 4.25 8 - - -
Alcomax 3 24.5 - 13.5 BAL - - 3 8 - - 0.75 Nb
Alcomax 4 24.5 - 15 BAL - - 3 8 - - 2.0 Ti
Ticonal 25 - - BAL - - 3 8 - - 2.0 Ti
3% Co 3 9 - BAL 1.5 - - - - 1 -
6% Co 6 9 - BAL 1.5 - - - - 1 -
9% Co 9 9 - BAL 1.5 - - - - 1 -
15% Co 15 9 - BAL 1.5 - - - - 1 -
35% Co 35 6 - BAL - - - - 4 1 -

Zirconium Alloys

*Indicates maximum
The figures shown are nominal compositions of the various alloys.
Zr 10 (C.P.) - - - - - 100 - - - - -
Zr Nb - - - - - BAL - - - - 2.5 Nb
Zr 20 - - - 1.5 - BAL - - 0.1 - 0.05 Ni
Zr 30 - - - - - BAL 0.5 0.5 - - -
Zr 40 - - - 1.5 - BAL - - 0.1 - 0.12 Fe
Zr 42 - - - - - BAL 1.5 1.1 - - -
Alcomax 4 24.5 - 15 BAL - - 3 8 - - 2.0 Ti
Ticonal 25 - - BAL - - 3 8 - - 2.0 Ti
3% Co 3 9 - BAL 1.5 - - - - 1 -
6% Co 6 9 - BAL 1.5 - - - - 1 -
9% Co 9 9 - BAL 1.5 - - - - 1 -
15% Co 15 9 - BAL 1.5 - - - - 1 -
35% Co 35 6 - BAL - - - - 4 1 -

Nickel Alloys

*Indicates maximum
The figures shown are nominal compositions of the various alloys.
Hastelloy A 57 1.0* - - - 100 - - - - -
Hastelloy B 62 1.0* 2.5* - - BAL - - - - 2.5 Nb
Hastelloy B2 66 1.0* 0.75* 1.5 - BAL - - 0.1 - 0.05 Ni
Hastelloy C276 56 16 2.5* - - BAL 0.5 0.5 - - -
Hastelloy C22 54 21 2.5* 1.5 - BAL - - 0.1 - 0.12 Fe
Hastelloy C4 54 16 1.25* - - BAL 1.5 1.1 - - -
Hastelloy D 85 1.0* - BAL - - 3 8 - - 2.0 Ti
Hastelloy F 45 22 2.5* BAL - - 3 8 - - 2.0 Ti
Hastelloy G 44 22 - BAL 1.5 - - - - 1 -
Hastelloy N 72 7 0.2 BAL 1.5 - - - - 1 -
Hastelloy R 66 15.5 1.5* BAL 1.5 - - - - 1 -
Hastelloy S 68 15.5 - BAL 1.5 - - - - 1 -
Hastelloy W 63 5 2.5* BAL - - - - 4 1 -
Hastelloy X 47 22 1.5
Langalloy 4R 65 - -
Langalloy 5R 57 16 -
Langalloy 7R 58 23 -
PE 7 37 18 2
PE 10 64 20 -
PE 11 38 18 -
PE 13 48 22 1.5
PE 16 44 16.5 -
Illium G 57 22.5 -
Illium R 64 22 -
C130 62 22 -
Inconel 600 75.5 15.5 -
Inconel 601 60.5 23 -
Inconel 625 61 21.5 -
Inconel 690 61 29 -
Inconel 702 79 15.6 -
Inconel 706 41.5 16 1
Inconel 713C 72 13.4 -
Inconel 718 53 18.5 -
Inconel W(722) 75 15 -
Inconel X(X750) 73 15 1
GMR 235 63 15.5 -
IN-102 67 15 -
IN-162 74 10 -
IN-657 49 48 -
Incoloy 800 32 20 -
Incoloy 825 40 21 -
Incoloy 901 42 12.5 1.0*
Incoloy DS 37 18 -
R55 52 23 -
AISI 310(HK) 20 25 -
AISI 330(HT) 35 15 -
Nimonic 75 77 20 -
Nimonic 80 74 20 2.0*
Nimonic 81 65 30 -
Nimonic 86 64.5 25 -
Nimonic 942 48 12.5 1.0*
PD16 (PD21) 71 6 1.0*

High Speed Steels

*Indicates maximum
The figures shown are nominal compositions of the various alloys.
M1 - 4 - BAL 8.5 1 - - 1.5 0.8 -
M2 and M3 - 4 - BAL 5 2 - - 6 0.8 -
M4 - 4 - BAL 4.5 4 - - 5.5 1.3 -
M7 - 4 - BAL 8.75 2 - - 1.75 1 -
M10 - 4 - BAL 8 2 - - - 0.85 -
M15 5 4 - BAL 3.5 5 - - 6.5 1.5 -
M30 5 4 - BAL 8 1.25 - - 2 0.8 -
M33 8 3.75 - BAL 9.5 1.15 - - 1.5 0.9 -
M35 5 4 - BAL 5 2 - - 6 0.8 -
M42 8 3.75 - BAL 9.5 1.15 - - 1.5 01.05 -
M50 - 4 - BAL 5 2 - - - 0.8 -
T1 - 4 - BAL - 1 - - 18 0.7 -
T4 5 4 - BAL - 1.4 - - 18 0.75 -
T5 8 4 - BAL - 2 - - 18 0.8 -
T6 12 4.5 - BAL - 1.5 - - 21 0.8 -
T7 - 4 - BAL - 2 - - 14 0.75 -
T15 5 4 - BAL - 5 - - 12 1.5 -
T21 - 4 - BAL - 0.5 - - 14 0.65 -
T42 9.5 4.1 - BAL 3 3 - - 9 1.3 -

COBALT ALLOYS

*Indicates maximum
The figures shown are nominal compositions of the various alloys.
Stellite® 1 50 33 - 13 - 2.5 - - - - -
Stellite® 3 52 30 - 13 - 2.4 - 0.1 - - -
Stellite® 4 53 31 3.0* 14 - 1.0* 3.0* - - - -
Stellite® 6 66 26 3.0* 5 - 1 3.0* - - - -
Stellite® 7 66 26 - 5 - 0.4 - - - - -
Stellite® 8 (F75) 63 30 - - 6 0.2 - - - - -
Stellite® 12 59 29 3.0* 9 - 1.8 2.0* - - - -
Stellite® 19 52 31 3.0* 10.5 - 1.7 3.0* - - - -
Stellite® 20 45 33 - 18 - 2.5 - - - - -
Stellite® 21 60 27 2.5* - 5.5 0.25 3.0* 0.005 - - -
Stellite® 23 65 25 1.5 5 - 0.4 2.0* - - - -
Stellite® 25 (L605) 52 20 10 15 - 0.15* 2.0* - - - -
Stellite® 30 50 26 15 - 6 0.45* 2.0* - - - -
Stellite® 31 (X40) 56 25 10 7 - 0.3 - - - - -
Stellite® (X45) 56 25 10.5 7.5 0.5* 0.3* 2.0* - - - 0.015* B
Stellite® 100 43 34 - 19 - 2 - - - - -
Stellite® 151 65 20 1.0* 13 - 0.5 2.0* 0.05 - - -
Stellite® 188 37 22 22 14 - 0.1 3.0* - - - 1.25* Mn
WI-52 (PWA 653) 63 21 1.0* 11 - 0.45* 1.5 - - - 2.0 Nb
S 816 44 20 20 4 4 0.35 5.0* - - - 4.0 Nb
Elgiloy 40 20 15 - 7 0.15 17 - - - 0.04 Be
Umco 50 50 28 - - - 0.12 20 - - - 0.75 Si, 0.5 Mn
Umco 51 48 28 - - - - 20 - - - 2.0 Nb, 0.7Si
HS Star J 41 32.5 2.5* 17.5 - 2.4 3 - - - -
MAR M-302 57 21.5 - 10 - - - - - 9 0.2 Zr
MAR M-322 60 21.5 - 9 - 1 - - - 4.5 2.25 Zr, 0.75 Ti
MAR M-509 50 21.5 10 7 - - 1 - - 3.5 0.5 Zr, 0.2 Ti
MAR M-918 50 30 20 - - 0.05 0.5 - - 7.5 0.1 Zr
FSX 414 48 20 10.5 7 - 0.30* 1.5* - - - 0.015* B
MP35N 35 4.1 35 - 10 - - - - - -

TOOL STEELS

*Indicates maximum
The figures shown are nominal compositions of the various alloys.
Hastelloy A 57 1.0* - 21 - 19 - - - - -
Hastelloy B 62 1.0* 2.5* 28 - 5.5 - - - - 0.4 V
Hastelloy B2 66 1.0* 0.75* 28 - 2.0* 0.4* - - - -
Hastelloy C276 56 16 2.5* 17 4 5.5 0.4* - - - 0.35* V
Hastelloy C22 54 21 2.5* 14 3 5.0* 0.4* - - - 0.35* V
Hastelloy C4 54 16 1.25* 16 - 2.0* 0.4* 0.5* - - -
Hastelloy D 85 1.0* - - - 1.0* - - 4.0* - 9 Si
Hastelloy F 45 22 2.5* 6 1.0* 18 - - - 2 -
Hastelloy G 44 22 - 6.5 1.0* 20 - - 2 2 -
Hastelloy N 72 7 0.2 16.5 0.5 5.0* 0.25 0.25 - - 0.01 B
Hastelloy R 66 15.5 1.5* 5 - 7.0* 2.2 2.5 - - -
Hastelloy S 68 15.5 - 14.5 - 1 - - - - 0.5 Mn
Hastelloy W 63 5 2.5* 24.5 - 5.5 - - - - 0.6 V
Hastelloy X 47 22 1.5 9 0.6 18.5 - - - - -
Langalloy 4R 65 - - 30 - 5 - - - - -
Langalloy 5R 57 16 - 17 5 5 - - - - -
Langalloy 7R 58 23 - 6 2 5 - - 6 - -
PE 7 37 18 2 5 - 35 1.2 1.2 - - -
PE 10 64 20 - 6 2.5 - - - - 6.5 -
PE 11 38 18 - 5.2 - 34 0.8 2.3 - - -
PE 13 48 22 1.5 9 0.6 18.5 - - - - -
PE 16 44 16.5 - 3.5 - 33 1.2 1.2 - - -
Illium G 57 22.5 - 6.4 - 6.5 - - 6.5 - -
Illium R 64 22 - 5 - 6 - - 2.5 - -
C130 62 22 - 10 - 0.5 1 2.7 - - -
Inconel 600 75.5 15.5 - - - 7 - - - - -
Inconel 601 60.5 23 - - - 14.1 1.35 - - - -
Inconel 625 61 21.5 - 9 - 3 - - - 3 -
Inconel 690 61 29 - - - 9 - - - - -
Inconel 702 79 15.6 - - - 0.4 3.4 0.7 - - -
Inconel 706 41.5 16 1 - - 36 - 1.75 - 2.9 -
Inconel 713C 72 13.4 - 4.5 - 1.5* 6.2 1.0* - 2.3 -
Inconel 718 53 18.5 - 3 - 18 - 0.8 - 5 -
Inconel W(722) 75 15 - - - 6.5 0.6 2.4 - - -
Inconel X(X750) 73 15 1 - - 7 0.9 2.5 - 0.9 -
GMR 235 63 15.5 - 5.2 - 10 3.7 2 - - 0.06 B
IN-102 67 15 - 2.9 3 7 0.5 - - 2.9 -
IN-162 74 10 - 4 2 0.5 6.5 1 - 1 2.0 Ta
IN-657 49 48 - - - - - - - 1.5 -
Incoloy 800 32 20 - - - 47 - - - - -
Incoloy 825 40 21 - 3 - 32 - 1 2 - -
Incoloy 901 42 12.5 1.0* 5.7 - 35 0.35* 2.9 - - -
Incoloy DS 37 18 - - - 42 - - - - 2.3 Si
R55 52 23 - 4 2 8 - - 6 - 4.0 Si
AISI 310(HK) 20 25 - - - BAL - - - - 2 Mn
AISI 330(HT) 35 15 - - - BAL - - - - 2.5 Si
Nimonic 75 77 20 - - - 5.0* 0.15 0.4 - - -
Nimonic 80 74 20 2.0* - - 1.5* 13 2.2 - - -
Nimonic 81 65 30 - - - 1.0* 1 1.75 - - -
Nimonic 86 64.5 25 - 10 - - - - - - 0.15 Mn
Nimonic 942 48 12.5 1.0* 5.5 - 25 4 3.7 - - 0.015 B
PD16 (PD21) 71 6 1.0* 2 11 - 6 0.2 - 1.5 0.02 B

NICKEL IRON ALLOYS

*Indicates maximum
The figures shown are nominal compositions of the various alloys.
IMI 115-160 (C.P.) Grade 1 BAL - - - - - - - - - 0.18 O2
IMI 115-160 (C.P.) Grade 2 BAL - - - - - - - - - 0.25 O2
IMI 115-160 (C.P.) Grade 3 BAL - - - - - - - - - 0.35 O2
IMI 115-160 (C.P.) Grade 4 BAL - - - - - - - - - 0.50 O2
IMI 230 BAL - - - - - - 2.5 - - -
IMI 260 BAL - - - - - - - - - 0.2 Pd
IMI 314 BAL 4 - - 4 - - - - - -
IMI 315 BAL 2 - - 2 - - - - - -
IMI 317 BAL 5 - 2.5 - - - - - - -
IMI 318 BAL 6 4 - - - - - - - -
IMI 443 BAL - 11 - - - - - 15 - -
IMI 550 BAL 4 - 2 - - 4 - - 0.5 -
IMI 551 BAL 4 - 4 - - 4 - - 0.5 -
IMI 679 BAL 2.25 - 11 - 5 1 - - 0.2 -
IMI 680 BAL 2.25 - 11 - - 4 - - 0.2 -
IMI 684 BAL 6 - - - 5 - - - 0.3 1.0 W
IMI 685 BAL 6 - - - 5 0.5 - - 0.25 -
IMI 700 BAL 6 - - - 5 4 1 - 0.25 -
IMI 829 BAL 5.5 - 3.5 - 3 0.3 - - 0.3 1.0 Nb
06/06/2002 BAL 6 6 2 - - - - - - -
6-2-4-2 BAL 6 - 2 - 4 2 - - - -
6-2-4-6 BAL 6 - 2 - 4 6 - - - -
8 Mn BAL - - - 8 - - - - - -
08/01/2001 BAL 8 1 - - - 1 - - - -
3-2.5 BAL 3 2.5 - - - - - - - -
Inconel 600 75.5 15.5 - - - 7 - - - - -
Inconel 601 60.5 23 - - - 14.1 1.35 - - - -
Inconel 625 61 21.5 - 9 - 3 - - - 3 -
Inconel 690 61 29 - - - 9 - - - - -
Inconel 702 79 15.6 - - - 0.4 3.4 0.7 - - -
Inconel 706 41.5 16 1 - - 36 - 1.75 - 2.9 -
Inconel 713C 72 13.4 - 4.5 - 1.5* 6.2 1.0* - 2.3 -
Inconel 718 53 18.5 - 3 - 18 - 0.8 - 5 -
Inconel W(722) 75 15 - - - 6.5 0.6 2.4 - - -
Inconel X(X750) 73 15 1 - - 7 0.9 2.5 - 0.9 -
GMR 235 63 15.5 - 5.2 - 10 3.7 2 - - 0.06 B
IN-102 67 15 - 2.9 3 7 0.5 - - 2.9 -
IN-162 74 10 - 4 2 0.5 6.5 1 - 1 2.0 Ta
IN-657 49 48 - - - - - - - 1.5 -
Incoloy 800 32 20 - - - 47 - - - - -
Incoloy 825 40 21 - 3 - 32 - 1 2 - -
Incoloy 901 42 12.5 1.0* 5.7 - 35 0.35* 2.9 - - -
Incoloy DS 37 18 - - - 42 - - - - 2.3 Si
R55 52 23 - 4 2 8 - - 6 - 4.0 Si
AISI 310(HK) 20 25 - - - BAL - - - - 2 Mn
AISI 330(HT) 35 15 - - - BAL - - - - 2.5 Si
Nimonic 75 77 20 - - - 5.0* 0.15 0.4 - - -
Nimonic 80 74 20 2.0* - - 1.5* 13 2.2 - - -
Nimonic 81 65 30 - - - 1.0* 1 1.75 - - -
Nimonic 86 64.5 25 - 10 - - - - - - 0.15 Mn
Nimonic 942 48 12.5 1.0* 5.5 - 25 4 3.7 - - 0.015 B
PD16 (PD21) 71 6 1.0* 2 11 - 6 0.2 - 1.5 0.02 B

TITANIUM ALLOYS

*Indicates maximum
The figures shown are nominal compositions of the various alloys.
F Nickel 92 - - 2 - - - - - - 5.5 Si
Z Nickel (Duranickel) 94 - - 0.2 4.5 0.5 - - - - -
Mumetal (British) 77 - 5 13 - - - - - - 3.7 Mo
Mumetal (U.S.A.) 77 1.5 4.5 17 - - - - - - -
Hy-Mu 80 - - 16 - - - - - - 4.0 Mo
Nilo 36 (Invar) 36 - - 63 - - - - - - -
Nilo 42 42 - - 57 - - - - - - -
Radiometal 46 - - 53 - - - - - - -
Nilo 48 48 - - 51 - - - - - - -
Nilo 50 50 - - 49 - - - - - - -
Nilo 475 47 5 - 47 - - - - - - -
A286 26 15 - 53 0.35 2.15 - - - - 1.25 Mo
Discalloy 26 13.5 - 54 0.35 1.6 - - - - 3.0 Mo
Timken 16-25-6 25 16 - 51 - - - - - - 6.5 Mo
Tinidur 26 15 - 55 0.15 2.3 - - - - -
Carpenter 20 27 20 3.5 45 - - - - - - 2.5 Mo
Carpenter 20Cb/Langalloy 20V 27 20 3.5 44 - - - - - - 2.5 Mo
0.6 Nb
Multimet (N-I55) 20 21 - 30 - - - - - - 20.0 Co
3.0 Mo
2.5 W
1.0 Nb
0.15 N
Kovar (Nilo K) 29 - - 54 - - - - - - 17.0 Co
C130 62 22 - 10 - 0.5 1 2.7 - - -
Inconel 600 75.5 15.5 - - - 7 - - - - -
Inconel 601 60.5 23 - - - 14.1 1.35 - - - -
Inconel 625 61 21.5 - 9 - 3 - - - 3 -
Inconel 690 61 29 - - - 9 - - - - -
Inconel 702 79 15.6 - - - 0.4 3.4 0.7 - - -
Inconel 706 41.5 16 1 - - 36 - 1.75 - 2.9 -
Inconel 713C 72 13.4 - 4.5 - 1.5* 6.2 1.0* - 2.3 -
Inconel 718 53 18.5 - 3 - 18 - 0.8 - 5 -
Inconel W(722) 75 15 - - - 6.5 0.6 2.4 - - -
Inconel X(X750) 73 15 1 - - 7 0.9 2.5 - 0.9 -
GMR 235 63 15.5 - 5.2 - 10 3.7 2 - - 0.06 B
IN-102 67 15 - 2.9 3 7 0.5 - - 2.9 -
IN-162 74 10 - 4 2 0.5 6.5 1 - 1 2.0 Ta
IN-657 49 48 - - - - - - - 1.5 -
Incoloy 800 32 20 - - - 47 - - - - -
Incoloy 825 40 21 - 3 - 32 - 1 2 - -
Incoloy 901 42 12.5 1.0* 5.7 - 35 0.35* 2.9 - - -
Incoloy DS 37 18 - - - 42 - - - - 2.3 Si
R55 52 23 - 4 2 8 - - 6 - 4.0 Si
AISI 310(HK) 20 25 - - - BAL - - - - 2 Mn
AISI 330(HT) 35 15 - - - BAL - - - - 2.5 Si
Nimonic 75 77 20 - - - 5.0* 0.15 0.4 - - -
Nimonic 80 74 20 2.0* - - 1.5* 13 2.2 - - -
Nimonic 81 65 30 - - - 1.0* 1 1.75 - - -
Nimonic 86 64.5 25 - 10 - - - - - - 0.15 Mn
Nimonic 942 48 12.5 1.0* 5.5 - 25 4 3.7 - - 0.015 B
PD16 (PD21) 71 6 1.0* 2 11 - 6 0.2 - 1.5 0.02 B

Flakes

Manganese

Manganese is too brittle to be of much use as a pure metal. It is used mainly in alloys, such as steel.
Steel contains about 1% manganese to increase strength and improve workability and wear resistance.
Manganese(IV)oxide is used as a catalyst, as a rubber additive and to decolorize glass, which is colored green by iron impurities. Manganese sulfate is used to make a fungicide.
Manganese(II)oxide is a strong oxidizing agent and is used in quantitative analysis. It is also used in the manufacture of fertilizers and ceramics.

Ingots

AlBe

Berillium

Beryllium increases strength, hardness, and resistance to corrosion steel properties. The use of beryllium to copper alloys is particularly effective. Beryllium bronzes can be produced by adding 3 to 6% of the metal. They are essential for the industrial production of stable and spark-free springs. These materials are also in demand for the production of parts of the outer skin of spacecraft.

APR
(basic grade)

APR
(catalyst grade)

rhenium

Rhenium is used as an additive for tungsten- and molybdenum-based alloys to obtain useful properties. These alloys are used for furnace filaments and X-ray equipment. It is also used as an electrical contact material because it is wear resistant and resists arc corrosion.
Rhenium catalysts are extremely resistant to poisoning (deactivation) and are used for the hydrogenation of fine chemicals. Some rhenium is used in nickel alloys to make single crystal turbine blades.

Ingots

Sponge

zirconium

Zirconium(IV) oxide is used in ultra-strong ceramics. It is used to make heat-resistant crucibles, furnace linings, cast stones, abrasives, and in the glass and ceramics industries. It is so strong that even scissors and knives can be made from it. It is also used in cosmetics, antiperspirants, food packaging, and to make microwave filters.
Zirconium metal is protected by a thin oxide layer that makes it exceptionally corrosion resistant to acids, alkalis and seawater. For this reason, it is used extensively by the chemical industry.
Together with niobium, zirconium is superconductive at low temperatures and is used to make superconducting magnets.

Metal

Carbide powder

Ingots

Oxide

APT

Concentrate

Catalyst

tungsten

Tungsten has the highest melting point of all metals and is alloyed with other metals to strengthen them. Tungsten and its alloys are used in many high-temperature applications, such as electrodes for arc welding electrodes and as heating elements in high-temperature furnaces.
Tungsten carbide is extremely hard and very important to the metalworking, mining and petroleum industries. It is produced by mixing tungsten powder and carbon powder and heating to 2200°C. It is excellent for cutting and drilling, including a new ‘painless’ dental drill that spins at extremely high speeds.

Ingots

tantalum

One of the most important uses of tantalum is in the manufacture of electronic components. An oxide layer that forms on the surface of tantalum can serve as an insulating (dielectric) layer.
It is highly resistant to corrosion and is therefore used in equipment for handling corrosive materials. It is also used as electrodes for neon tubes, AC /DC rectifiers and in glass for special lenses.
Tantalum alloys can be extremely strong and have been used for turbine blades, rocket nozzles, and nose caps for supersonic aircraft.

Ingots

hafnium

Hafnium has a very high melting point and is therefore used in plasma welding torches. Hafnium has been successfully alloyed with various metals, including iron, titanium, and niobium.
Hafnium oxide is used as an electrical insulator in microchips, while hafnium catalysts are used in polymerization reactions.

Ingots

tin

Tin has many uses. It can be highly polished and is used to coat other metals to prevent corrosion, such as tin cans made from tin-plated steel. Tin alloys are important, such as soft solder, tin, bronze and phosphor bronze. A niobium-tin alloy is used for superconducting magnets.

Concentrate (unroasted)

Oxide

FeMo

Concentrate (roasted)

Catalyst

Metal

molybdenum

Most molybdenum is used to make alloys. It is used in steel alloys to increase strength, hardness, electrical conductivity, and resistance to corrosion and wear. These ‘moly steel’ alloys are used in parts of engines. Other alloys are used in heating elements, drills and saw blades.
Molybdenum disulfide is used as a lubricant additive. Other uses for molybdenum include catalysts for the petroleum industry, printing inks for printed circuit boards, pigments and electrodes.

FeNb60

NiNb

AlNb

Ingots

Powder

Bar

niobium

Niobium is used in alloys, including stainless steel. It improves the strength of alloys, especially at low temperatures. Alloys containing niobium are used in jet engines and rockets, supports for buildings and oil platforms, and oil and gas pipelines.

Ingots

yttrium

Yttrium is often used as an additive in alloys. It increases the strength of aluminum and magnesium alloys. It is also used in the manufacture of microwave filters for radar equipment and serves as a catalyst in the polymerization of ethene. Yttrium aluminum garnet (YAG) is used in lasers that can cut through metals. It is also used in white LED lamps. Yttrium oxide is added to the glass used to make camera lenses to make it heat and shock resistant. It is also used to make superconductors. Yttrium oxysulfide was once widely used to make red phosphor for old color television tubes.

Ingots

zinc

Most zinc is used to galvanize other metals, such as iron, to prevent rust. Galvanized steel is used for car bodies, streetlights, safety barriers, and suspension bridges.
Large quantities of zinc are used to make die castings, which are important in the automotive, electrical and hardware industries. Zinc is also used in alloys such as brass, nickel silver and aluminum solder.
Zinc oxide is used in the manufacture of many products such as paints, rubber, cosmetics, pharmaceuticals, plastics, inks, soaps, batteries, textiles and electrical equipment. Zinc sulfide is used in the manufacture of fluorescent paints, fluorescent tubes and X-ray screens.

Cathode uncuts (A-grade)

Cathode crowns

nickel

Nickel is corrosion resistant and is used to protect other metals as a coating. However, it is mainly used to make alloys such as stainless steel. Nichrome is an alloy of nickel and chromium with small amounts of silicon, manganese and iron. It resists corrosion even when red-hot, and is therefore used in toasters and electric ovens. A copper-nickel alloy is often used in desalination plants that convert seawater into fresh water. Nickel steel is used for armor plating. Other nickel alloys are used for ship propeller shafts and turbine blades.
Nickel is used in batteries, including rechargeable nickel-cadmium batteries and nickel-metal hydride batteries used in hybrid vehicles.

Metal

Cake

Powder

cobalt

Cobalt is alloyed with aluminum and nickel to make particularly strong magnets.
Other cobalt alloys are used in jet turbines and gas turbine generators, where high temperature resistance is important.

Metal

FeCr HC/LC

Chromium

Chromium is used to harden steel, to produce stainless steel and to produce various alloys.
Chromium plating can be used to give steel a polished mirror finish.
Chrome-plated car and truck parts, such as bumpers, used to be very common. It is also possible to chrome plastics, which are often used in bathroom fixtures.
Chromium compounds are used as industrial catalysts and pigments. Rubies get their red color from chrome, and glass treated with chrome has an emerald green color.

FeV80

Catalyst

Vanadium

About 80% of the vanadium produced is used as a steel additive. Vanadium steel alloys are very tough and are used for armor plates, axles, tools, piston rods, and crankshafts. Less than 1% vanadium and as little chromium make the steel shock and vibration resistant. Vanadium alloys are used in nuclear reactors because vanadium hardly absorbs neutrons. Vanadium(V) oxide is used as a pigment for ceramics and glass, as a catalyst and in the manufacture of superconducting magnets.

Metal

Powder

Sponge

FeTi70

Magnesium

Magnesium has a density one-third lower than aluminum. As an alloying agent, it improves the mechanical, processing and welding properties of aluminum. These alloys are useful in aircraft and automotive construction. Magnesium is used in products that benefit from its light weight, such as car seats, luggage, laptops, cameras and power tools. It is also added to molten iron and steel to remove sulfur.

Magnesium sulfate is sometimes used as a mordant for dyes. Magnesium hydroxide is added to plastics to make them fire retardant. Magnesium oxide is used to make heat-resistant bricks for fireplaces and stoves. It is also added to livestock feed and fertilizers. Magnesium hydroxide (milk of magnesia), sulfate (Epsom salt), chloride and citrate are used in medicine.

Metal

Powder

Sponge

FeTi70

Titanium

Titanium is as strong as steel, but has a much lower density. Therefore, it is an important alloying agent for many metals such as aluminum, molybdenum, and iron. These alloys are used primarily in aircraft, spacecraft and missiles because of their low density and ability to withstand extreme temperatures. They are also used in golf clubs, laptops, bicycles and crutches. Most titanium is used in the form of titanium(IV)oxide. It is used extensively as a pigment in house paints, artists’ paints, plastics, enamels and paper.

Flakes
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Ingots
AlBe
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APR (basic grade)
APR (catalyst grade)
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Ingots
Sponge
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Metal
Carbide powder
Ingots
Oxide
APT
Concentrate
Catalyst
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Ingots
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Ingots
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Ingots
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Concentrate
(unroasted)
Oxide
FeMo
Concentrate (roasted)
Catalyst
Metal
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FeNb60
NiNb
AlNb
Ingots
Powder
Bar
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Ingots
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Ingots
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Cathode uncuts
(A-grade)
Cathode crowns
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Metal
Cake
Powder
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Metal
FeCr HC/LC
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FeV80
Catalyst
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Ingots
Oxide
Flakes
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STAINLESS STEELS

*Indicates maximum
The figures shown are nominal compositions of the various alloys.
Duplex 5.5 22.5 - 3 - BAL - - - - 0.17 N2
AISI 302 (EN58) 9 18 - - - BAL - - - - 0.15 C
AISI 304 9 18 - - - BAL - - - - 0.08* C
AISI 309 12.5 22.5 - - - BAL - - - - 0.20* C
AISI 316 10.5 17 - 2 - BAL - - - - 0.08* C
AISI 317 13 19 - 3.5 - BAL - - - - 0.08* C
AISI 321 (EN58B) 9 18 - - - BAL - 5xC - - 0.08* C
AISI 347/348 (EN58F,G) 10 18 - - - BAL - - - 8xC 0.08* C
AISI 409 0.7* 12 - - - BAL 0.5 0.5 - - 0.09* C
AISI 420 (EN56/S62) 1.0* 13 - 13 - BAL - - - 1.8 0.32* C
AISI 430 (FI 17) 0.5* 17 - - - BAL - - - - 0.12* C
AISI 431 (EN57/S80) 2 16 - - - BAL - - - - 0.20* C
Crown Min 12.5 22.5 - - 1 BAL - - - - 0.20* C
Crown Max 12.5 22.5 - - 2.75 BAL - - - - 0.20* C
17-4 PH 4 16.5 - - - BAL - - 3.5 0.3 0.03 C
17-7 PH 7 17 - - - BAL 1 1 - - 0.05 C
FV 520 (B) 5 14.5 - 1.6 1.6 BAL - - 1.8 0.4 0.05 C
FV 535 0.3 10.5 2.6* 0.75 0.75 BAL - - - 0.4 0.07* C
Rex 448 0.75 11.5 - 0.45 0.45 BAL - - - 0.45 0.15* C
Jethete M152 2.5 12 - 1.8 1.8 BAL - - - - 0.1 C
Jethete M190 2.7 12 1.55 1.8 1.8 BAL - - - - 0.13 C
G18B 13 13 10 1.7 2.5 BAL - - - 3 0.4 C
Ferralium 5.35 24.2 - 2.5 - BAL - - 1.6 -
Kanthal 22.5 2.0* - - BAL 5.5 5.5 - -
Metal
Powder
Sponge
FeTi70
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