Alloy/UNS
Density(g/cm3) |
DESCRIPTION
|
Ni+
|
C
|
Mn |
Fe
|
Si
|
OTHER
|
AMS*
|
ASTM*
|
NICKEL 200
N02200
8.89 |
Commercially pure
nickel. High corrosion resistance. Used
in food handling and electronics. |
99.5 |
.08 |
.18 |
.20 |
.18 |
Cu .13 |
-- |
B-162 |
NICKEL 201
N02201
8.89 |
Similar to nickel
200 except with a lower carbon content
for better formability.Most applications
in chemicals. |
99.5 |
.01 |
.18 |
.20 |
.18 |
Cu .13 |
5553 |
B-162 |
HASTELLOYC-22
N06022
8.69 |
A versatile nickel
chromium molybdenum tungstenAlloy with
resistance to a variety of industrial
chemicals. Superior weldability. |
56 |
.010
MAX |
.50
MAX |
3 |
.08
MAX |
Co 2.5MAX
W 3
Cr 22
V .35MAX
Mo 13 |
-- |
B-275 |
HASTELLOYG-30
N06030
8.22 |
High chromium nickel
base alloy with superior corrosion resistance
to phosphoric acids and environments
with highly oxidizing acids. |
40 |
.03 |
1.5
MAX |
13-17 |
.8
MAX |
Co 5 MAX
W 1.5-4
Cr 28-31.5
V 1-2.4
Mo 4-6
Cb+Ta .3-1.5
|
-- |
B-582 |
HAYNES?
2142
N07214
8.05 |
Nickel based precipitation
strengthened alloy with oxidation resistance
to 2200°F. For furnaceparts exposed
to carburizing, chlorine contaminatedand
oxidizing atmospheres; gas turbine parts.
|
76.5 |
-- |
-- |
3 |
-- |
Co 16.0
Al 4.5 |
-- |
-- |
HAYNES?
230TM
N06230
8.83 |
Nickel-chromium-tungsten-molybdenum
alloy with outstanding resistance to
oxidizing environments up to 2100°F
for prolonged periods. |
53.5 |
.10 |
.5 |
3 MAX |
.4 |
Cr 22
Al 3
W 14
La 1-2.4
Mo 2
B .015 MAX
Co 5 MAX |
5878 |
B-435 |
HAYNES?
2422
(None)
9.05 |
Age hardenable,
nickel alloy for use up to 1300°F. Low
thermal expansion, good oxidation resistance
and excellent aged ductility. Suited
for gas turbine engines and chemical
process plants. |
62.5 |
0.03 |
0.80 |
2 |
0.80 |
Al 0.50
Cr 7-9
Cu 0.50
Co 2-5
Mo 24-26 |
-- |
-- |
MONEL?
4001
N04400
8.83 |
A solid solution
alloy with high strength andtoughness
over wide temp. ranges. Used in electronic
components, springs. Corrosion resistant
and oxidation resistance to 1000°F.
|
66.5 |
.15 |
1.0 |
1.25 |
.50 |
Cu 31.50
S .01 |
4544 |
B-127 |
MONEL?
K-5001
N05500
8.46 |
Similar to Monel?
4001 but with higher tensile strength;a
precipitation hardening alloy. Used
in oil well drilling collars, doctor
blades. Good strength and ductility
423°F to 1200°F. |
66.5 |
.13 |
.75
MAX |
1.0 |
.50 |
Cu 29.5
Ti .63
Al 2.73 |
4676 |
|
INCONEL?
6001
N06600
8.43 |
Has high corrosion
and heat resistance combined with excellent
strength and workability. Mainly used
in corrosive atmospheres. Oxidation
resistance to 2150°F. |
76.0 |
.08 |
.50
MAX |
8.0 |
.25 |
Cu .25
Cr 15.50 |
5540 |
B-168 |
INCONEL?
6251
N06625
8.44 |
Outstanding corrosion
resistance with excellent fabricability.
Good for cryogenic to high temp.applications
up to 2000°F.< |
61.0 |
.08 |
.25 |
2.5 |
.25 |
Cr 21.50
Mo 9.0
Al .20
Cb+Ta 3.65
Ti .20
Nb 3.65 |
5599 |
B-443 |
INCONEL?
7181
N07718
8.19 |
High strength and
corrosion resistance for use in temp.
ranges from -423°F to 1300°F.
Nuclear applications. |
52.5 |
.04 |
.18 |
17.5 |
.18 |
Cu .15
S .008
Al .50
Mo 3.05
Ti .90
Cb+Ta 5.13
Cr 19.0
Nb 5.13 |
5596
5597 |
B-670 |
INCONEL?
X-7501
N07750
8.25 |
A precipitation
hardening nickel-chromium alloy with
useful strength to 1500°F. Good corrosion
and oxidation resistance. |
73.0 |
.04 |
.50 |
7.0 |
.25 |
Cu .25
Cr 15.50
Al .70
Mo .005
Ti 2.50
Cb+Ta .95 |
5542
5598 |
|
INCOLOY?
8001
N08800
7.95 |
Nickel-iron-chromium
alloy that is carburization resistant
at elevated temp. |
32.5 |
.05 |
.75 |
46.0 |
.50 |
Cu .38
Cr 21.00
Al .38
Ti.38 |
5871 |
B-409 |
INCOLOY?
8251
N08825
8.14 |
An alloy that is
highly resistant to aggressively corrosive
environments such as sulfuric,phosphoric
acids and seawater. |
42.0 |
.03 |
.50 |
29.0 |
.25 |
Cu 2.25
Cr 21.50
Al .10
S.015
Ti.90
Mo 3.00 |
|
B-424 |
Ni-SpanC?
9021
N09902 |
A nickel-iron-chromium
alloy used in precision spring applications
subject to severe temperature fluctuations.
|
42.25 |
.03 |
.40 |
48.5 |
.50 |
Al .55
Cr 5.33
Ti 2.58
S .02 |
5521
5223
5225 |
|
HASTELLOY?
B-2
N10665
9.22 |
Used in chemical
industry for resistance to hydrochloric
acid, sulfuric acid, phosphoric acid.
Oxidation atmosphere resistant to 1400?F.
|
69 |
.02
MAX |
1.00
MAX |
2.0
MAX |
.10
MAX |
Mo 26.0-30.0
Co 1.00 MAX
Cr 2.50 MAX |
|
B-333 |
HASTELLOY?
C-2762
N10276
8.89 |
Used in chemical
industry for resistance to oxidizing
agents. Replaces Hastelloy? C2
with better fabricability. |
66 |
.02
MAX |
1.00
MAX |
4.0-
7.0 |
.08
MAX |
Cr 14.5-16.5
W 3.0-4.5
Mo 15.0-17.0
Co 2.50MAX |
|
B-575< |
HASTELLOY? X2
N06002
8.22 |
Jet engine components
for afterburner sections, blades, tailpipes,
furnace applications, honey-comb, bellows,
ducting. Good strength and oxidation
resistance to 2200°F. |
48 |
.05- .15 |
1.00
MAX |
17.0-
20.0 |
1.00
MAX |
Cr 20.5-23.0
W .20-1.0
Mo 8.0-10.0
Co .50-2.5 |
5536 |
B-435 |
HAYNES?
1882
R30188
8.98 |
A cobalt-based alloy
with excellent high temperature Strength
and oxidation resistance to 2000°F,
combined with outstanding post-standing
ductility. |
20.0-
24.0 |
.05-
.15 |
1.25
MAX |
3.0
MAX |
.20-
.50 |
Co 38.0
W 13.0-16.0
Cr 20.0-24.0
La .03-.15
| 5608 |
|
HAYNES?
252
L-605
R30605
9.13 |
Jet engine components,
combustion chambers,afterburner parts.
Oxidation and carburization resistant
to 1900°F. Good high temperature strength.
|
9.0-
11.0 |
.05-
.15 |
1.25
MAX |
3.0
MAX |
.40
MAX |
Co 51.0
Cr 19.0-21.0
W 14.0-16.8 |
5537 |
|
WASPALOYTM6
N07001
8.20
| Jet engine turbine
wheels, buckets, spacers, shafts. Good
for high temperature applications. |
56.0 |
.02-
.10 |
.10
MAX |
2.0
MAX |
.15
MAX |
Co 13.5
Al 1.3
Cr 19.5
Cu 10
Mo 4.25
Ti 3.0 |
5544 |
|
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