2.4858

Data sheet material 2.4858 / Alloy 825

NiCr21Mo

Fully austenitic titanium-stabilised nickel-iron-chromium alloy

Brief description

The material 2.4858 or Alloy 825 or Incoloy® 825 is a titanium-stabilised, fully austenitic nickel-iron-chromium alloy with additions of copper and molybdenum with excellent resistance to a wide range of corrosive media. This material is resistant to corrosion in acids and alkalis as well as in oxidising and reducing environments.

Standards and nomenclature

EN
DIN NiCr21Mo
AISI Alloy 825, Incoloy® 825
US N08825
EN
DIN NiCr21Mo
AISI Alloy 825, Incoloy® 825
US N08825

Chemical composition according to DIN 17744

Ni (nickel) 38,0 46,0
Cr (chromium) 19,5 23,5
Fe (iron) 20,0 38,0
C (carbon) - 0,025
Mn (manganese) - 1,0
Si (silicon) - 0,5
Co (Cobalt) - 1,0
Al (aluminium) - 0,2
Ti (titanium) 0,6 1,2
P (phosphorus) - 0,02
S (sulphur) - 0,015
Mo (molybdenum) 2,5 3,5
Cu (copper) 1,5 3,0

-
-

min.

max.

Ni
(nickel)

38,0

46,0

Cr
(chrome)

19,5

23,5

Fe
(iron)

20,0

38,0

C
(carbon)

-

0,025

Mn
(Manganese)

-

1,0

Si
(Silicon)

-

0,5

Co
(Cobalt)

-

1,0

-
-

min.

max.

Al
(aluminium)

-

0,2

Ti
(Titanium)

0,6

1,2

P
(phosphorus)

-

0,02

S
(sulphur)

-

0,015

Mo
(Molybdenum)

2,5

3,5

Cu
(copper)

1,5

3,0

-
-

-

-

General properties

Corrosion resistance
Mechanical properties good
Weldability good

Special properties

Good toughness at continuous temperatures up to approx. 550°C

Corrosion resistance

Due to its high nickel content, the material 2.4858 is practically insensitive to stress corrosion cracking. It is also resistant to chloride-induced pitting and crevice corrosion. Alloy 825 also has good resistance to mineral acids (nitric, phosphoric, sulphuric and hydrochloric acid), organic acids, alkalis, ammonia and chloride alkalis. Its versatility is due to the fact that Alloy 825 is used in dissolution tanks for nuclear fuel elements, in which a variety of corrosive media act alternately. This material is resistant to seawater.

Mechanical properties
at 20°C

Yield point
Rp0,2
N / mm²

≥ 220

Tensile strength
Rm
N / mm²

≥ 550

Elongation
A5,65

≥ 30%

Weldability

The material 2.4858 can be welded using standard welding processes (TIG, MIG/MAG, plasma, electron beam welding and manual metal arc welding). The workpiece should be free of dirt and scale. The heat input should be kept low and the line bead technique should be used. Annealing colours should be removed immediately after welding, i.e. while still warm, using a stainless steel brush.

Machinability

Machining should be carried out in the annealed condition. Alloy 825 tends to work harden. Therefore, a low feed rate and a low cutting speed should be selected. In order to undercut the previously created work-hardened zone, the tool should be in constant engagement with a sufficient cutting depth.

Processing

Cold forming
Chip-removing processing Yes
Cold forming
Chip-removing processing Yes

Thermal treatment

Soft or stable annealing
Hot forming 1150 - 900°C
Cooling down Fast in water; rapid air cooling for thicknesses under 3 mm
Soft or stable annealing
Hot forming 1150 - 900°C
Cooling down Fast in water; rapid air cooling for thicknesses under 3 mm

Physical properties

Density
at 20°C
kg/dm³

8,05

Electrical
Resistance at 20°C
(ohm) mm²/m

1,12


Melting range
 

1370 - 1400°C

Thermal conductivity
at 20°C
W/m K

10,8

Specific
Heat capacity
at 20°C
J/kg K

440

Markets & Applications

Plant engineering
Chemistry
Oil and Gas
Offshore
Compensators / recuperators
Nuclear technology
Flue gas desulphurisation systems

Frequently asked questions

Important note

TEAM EDELSTAHL operates purely as a trading company without technical staff. Consequently, we are not authorised to provide material consulting services.

The above values and information on the properties and/or usability of the material are purely informative. This information is based on the experience of the manufacturer and TEAM EDELSTAHL. All information is without guarantee. Misprints, errors and changes excepted.