Incoloy 825 Alloy 825 (UNS N08825)

Nickel-iron-chromium-molybdenum-copper austenitic alloy, limiting composition (wt %): Ni 38.0 to 46.0, Fe 22.0 min, Cr 19.5 to 23.5, Mo 2.5 to 3.5, Cu 1.5 to 3.0, Ti 0.6 to 1.2, C 0.05 max, Mn 1.0 max, S 0.03 max, Si 0.5 max, Al 0.2 max

Also known as UNS N08825, EN 2.4858, EN name NiCr21Mo, DIN 17750, DIN 17752, AFNOR NC21FeDU · 8 more

Incoloy 825 (UNS N08825, W.Nr.

8 sources · Updated 2026-10-26 · CC BY 4.0

Evidence level

2 of 5

Lab-measured

Resist acids

Sulfuric and phosphoric acid resistance

Carry strength when annealed

338 MPa yield (plate)

Gain strength by cold work

889 MPa yield (cold drawn tubing)

Weight

8.14 g/cm3

Melt

1370 to 1400 C

Recipe, share of the weight

  • Ni 38 to 46%Nickel
  • Fe minimum (matrix)Iron
  • Cr 19.5 to 23.5%Chromium
  • Mo 2.5 to 3.5%Molybdenum
  • Cu 1.5 to 3%Copper
  • Ti 0.6 to 1.2%Titanium
  • C 0.05 max, Mn 1.0 max, S 0.03 max, Si 0.5 max, Al 0.2 max (wt %)Minor elements

Best for

Corrosion service in sulfuric and phosphoric acid, sour gas and seawater, in sheet, plate, bar, tube and pipe that must be welded and formed

Weakest at

Strength against chloride pitting: Jacquet judges it only an improvement over Type 316 for pitting, and rates Alloy 625 and AL-6XN higher

Risk at a glance

  • People Moderate. Solid is an article, dust and fume are not
  • If it fails Moderate. Chloride stress cracking in boiling magnesium chloride
  • Corrosion Moderate. Alloy 825 resists chloride pitting only moderately and is judged an improvement, not a dramatic one, over Type 316.

Quick facts: Alloy 825 (UNS N08825)

Key properties of Alloy 825 (UNS N08825)
PropertyValueBasis
Density8.14 g/cm³1 sourced value
Yield strength240 to 889 MPa3 sourced values across conditions
Tensile strength585 to 1,000 MPa3 sourced values across conditions
Young's modulus196 GPa1 sourced value
Thermal conductivity11.1 W/(m·K)1 sourced value
Thermal expansion (CTE)13.9 ppm/K1 sourced value
Melting point1,370 to 1,400 °C1 sourced value
Specific heat440 J/(kg·K)1 sourced value
Electrical resistivity0.0000011 Ω·m1 sourced value

What is the density of Incoloy 825?

Incoloy 825 has a density of 8.14 g/cm³. The source and test conditions are listed in the properties table on this page.

What is the thermal conductivity of Incoloy 825?

Incoloy 825 has a thermal conductivity of 11.1 W/(m·K). The source and test conditions are listed in the properties table on this page.

What is the coefficient of thermal expansion of Incoloy 825?

Incoloy 825 has a coefficient of thermal expansion of 13.9 ppm/K. The source and test conditions are listed in the properties table on this page.

What is the melting point of Incoloy 825?

Incoloy 825 has a melting point of 1,370 to 1,400 °C. The source and test conditions are listed in the properties table on this page.

What is the yield strength of Incoloy 825?

Incoloy 825 has a yield strength of 240 to 889 MPa. The range covers 3 sourced values across the tempers, forms and test conditions the sources report; room-temperature values are used where a source states a temperature.

What are the other names and codes for Incoloy 825?

Incoloy 825 is also written as UNS N08825, EN 2.4858, EN name NiCr21Mo, DIN 17750, DIN 17752, AFNOR NC21FeDU. Each code is printed in the source listed beside it in the designations table.

What is Incoloy 825 used for?

Uses recorded in the sources include Process pressure vessels and heat exchangers in chemical plant; Sour gas and oil well piping, offshore piping, and immersion pipes in sea-water-cooled heat exchangers; Steel pickling equipment: heating coils, vessels, baskets and chains in sulfuric acid pickling plants.

Why it exists

Incoloy 825 is a nickel-rich austenitic alloy built for acid and chloride corrosion rather than for strength. Its nickel, molybdenum and copper together resist sulfuric and phosphoric acids, and the titanium stops intergranular attack after heating. Special Metals and VDM both point to chemical processing, pickling equipment, oil and gas piping and nuclear fuel reprocessing. The Special Metals bulletin says the alloy resists chloride stress cracking, but a Jacquet U-bend test shows cracking in boiling magnesium chloride over long times. Its density is 8.14 g/cm3, and it melts between 1370 and 1400 C. No spacecraft, rocket or satellite use was found in the sources read.

Where it's used

Pressure vessels and heat exchangers

VdTÜV approves VDM Alloy 825 for pressure vessels with walls up to 450 C, and ASME Section VIII Division 1 approves it up to 538 C (1,000 F).

Oil, gas and sour service

Special Metals names sour gas, oil wells and sea water as useful environments, and VDM lists oil and gas extraction piping and offshore piping.

Pickling and nuclear

VDM lists sulfuric acid pickling plant parts, and Special Metals lists fuel element dissolvers and radioactive waste handling.

Recipe

Nickel-iron-chromium-molybdenum-copper austenitic alloy, limiting composition (wt %): Ni 38.0 to 46.0, Fe 22.0 min, Cr 19.5 to 23.5, Mo 2.5 to 3.5, Cu 1.5 to 3.0, Ti 0.6 to 1.2, C 0.05 max, Mn 1.0 max, S 0.03 max, Si 0.5 max, Al 0.2 max

Incoloy 825 is an austenitic nickel-iron-chromium alloy with molybdenum, copper and titanium additions. Special Metals gives its limiting composition in weight percent (Table 1). The titanium addition stabilises the alloy against sensitisation to intergranular corrosion, and the alloy is supplied as bar, rod, wire, sheet, strip, plate, tube and pipe (Special Metals; VDM). Special Metals gives a hot-working range in its Hot and Cold Forming section and recommends that final hot working be done in the lower part of that range for best corrosion resistance.

What Alloy 825 (UNS N08825) is made of
IngredientShare of the weightWhat it does
Nickel Ni 38 to 46% Gives resistance to chloride stress corrosion cracking, and with molybdenum and copper gives outstanding resistance to reducing environments (Special Metals)
Iron Fe minimum (matrix) Forms the austenitic matrix with nickel
Chromium Cr 19.5 to 23.5% Confers resistance to oxidising substances such as nitric acid, nitrates and oxidising salt (Special Metals)
Molybdenum Mo 2.5 to 3.5% Aids resistance to pitting and crevice corrosion, and with nickel and copper, to reducing acids (Special Metals)
Copper Cu 1.5 to 3% With nickel and molybdenum, gives resistance to sulfuric and phosphoric acids (Special Metals)
Titanium Ti 0.6 to 1.2% Stabilises the alloy against intergranular corrosion after heating in the sensitising range (Special Metals; VDM)
Minor elements C 0.05 max, Mn 1.0 max, S 0.03 max, Si 0.5 max, Al 0.2 max (wt %) Residual limits

Weight shares are as printed in the sources.

What it can do

Resist acids

Sulfuric and phosphoric acid resistance

Special Metals and VDM both name sulfuric and phosphoric acid among the environments the alloy is particularly useful in.

Carry strength when annealed

338 MPa yield (plate)

measured

Annealed plate has a typical yield strength of 338 MPa and a tensile strength of 662 MPa, stretching 45 percent before breaking (Special Metals).

Gain strength by cold work

889 MPa yield (cold drawn tubing)

measured

Cold drawn tubing has a typical yield strength of 889 MPa and tensile strength of 1000 MPa, with 15 percent elongation.

Weight

8.14 g/cm3

measured

Density is 8.14 g/cm3 in the Ulbrich datasheet.

Melt

1370 to 1400 C

measured

Special Metals gives the melting range as 1370 to 1400 C (2500 to 2550 F).

How it compares

Compare with Inconel 625 on this site (inconel-625), a nickel-chromium-molybdenum-niobium alloy. Incoloy 825 instead adds copper and titanium. Jacquet ranks Alloy 625 above Alloy 825 for chloride pitting resistance, and the Alloy 825 datasheets name sulfuric and phosphoric acid as its key service. The rows below use this profile's own values only, so read them as examples, not as a ranking against 625.

The same measurements for each material, so you can compare them. Each row names the key condition under the value; the full conditions and methods are in the numbered notes under Technical details. Other materials are shown beside it; each was measured under its own conditions, so open its page before comparing closely. Compare every grade in the family.

Benchmarks
MeasurementAlloy 825 (UNS N08825)IN718 (UNS N07718)IN625 (UNS N06625)FeNi36Ni-MoC-22C-276 (UNS N10276)X (UNS N06002)UNS N07214H230 (UNS N06230)UNS N08800Alloy 600 (UNS N06600, W.Nr. 2.4816)Alloy 601Alloy 617X-750 (UNS N07750)Fe-Ni-CoAlloy 400 (UNS N04400)K-500NiNi3Al, NiAlNiBe2Ni-alloysUNS N07090 (W. Nr. 2.4632)UNS N07001
Thermal behavior and safety
Melting range, Incoloy 825Melting range printed in a manufacturer bulletin1370 to 1400 °C1260 °C1290 to 1350 °C1427 °C1370 to 1418 °C1357 to 1399 °C1323 to 1371 °C1260 to 1355 °C1355 to 1400 °C1301 to 1371 °C1357 to 1385 °C1354 to 1413 °C1360 to 1411 °C1330 to 1380 °C1393 to 1427 °C1450 °C1300 to 1350 °C1315 to 1350 °C1455 °Cno data1195 to 1325 °C1425 °C1370 °C1330 to 1360 °C
Specific heat capacity, 0 to 100 °C440 J/(kg·K)1435 J/kg °C410 J/(kg·K)515 J/(kg·K)373 J/kg.°C410 J/(kg·K)427 J/kg.°C486 J/(kg·K)452 J/kg-°C397 J/kg·°C460 J/kg·°C444 J/kg °C448 J/(kg·K)419 J/(kg·K)0.103 Btu/lb/°F500 J/(kg. K)427 J/kg°C419 J/kg °C456 J/(kg·K)no datano data500 J/(kg·K)446 J/(kg·K)no data
Thermal conductivity at 21 °CValue printed in a manufacturer datasheet11.1 W/(m·K)79 BTU·in/ft²·h·°F9.8 W/m°C72.85 Btu·in/(hr·ft²·°F)11.2 W/m.°C10.1 W/(m·K)10.5 W/m.°C9.2 W/(m·K)12 W/m-°C8.9 W/(m·°C)11.5 W/m°C14.9 W/(m·K)11.2 W/(m·K)13.4 W/(m·K)83 Btu/in./hr/sq ft/°F17.5 W/m °K22 W/m°C17.5 W/m °C70.3 W/(m·K)no data48 W/(m·K)13 W/(m·K)11.47 W/(m·K)19.1 W/(m·°C)
Thermal conductivity at 100 °C12.4 W/(m·K)279 BTU·in/ft²·h·°F9.8 W/m°C72.85 Btu·in/(hr·ft²·°F)11.2 W/m.°C10.1 W/(m·K)10.5 W/m.°C9.2 W/(m·K)12 W/m-°C8.9 W/(m·°C)11.5 W/m°C14.9 W/(m·K)11.2 W/(m·K)13.4 W/(m·K)83 Btu/in./hr/sq ft/°F17.5 W/m °K22 W/m°C17.5 W/m °C70.3 W/(m·K)no data48 W/(m·K)13 W/(m·K)11.47 W/(m·K)19.1 W/(m·°C)
Physical and electrical
Density, Incoloy 825Value printed in a manufacturer datasheet8.14 g/cm³0.297 lb/in38.44 g/cm³8.05 g/cm³9.22 g/cm³8.69 g/cm³8.89 g/cm³8.22 g/cm³8.05 g/cm³8.97 g/cm³7.94 g/cm³0.306 lb/in38.11 Mg/m38.36 g/cm³8.28 g/cm³8.36 g/cm³8.8 g/cm³8.45 g/cm³8.89 g/cm³7.5 g/cm³8.27 g/cm³8.2 g/cm³8.18 g/cm³8.19 g/cm³
Electrical resistivity at 20 °C112 µΩ·cm5725 ohm circ mil/ft129 µΩ-cm84 µΩ·cm1.37 μohm.m1.14 µΩ·m1.23 μohm.m114.8 µohm-cm135.9 µohm-cm125 µohm-m0.989 µΩ·m1.03 µΩ·m1.18 µΩ·m1.22×10^-4 Ω·cm731 ohm circ mil/ft49 μΩcm0.511 µΩ·m0.615 µΩ·m0.096 µΩ·mno data< 28.7 µΩ·cm45 µΩ·cm1.18 µΩ·m1.24 µΩ·m
Temperature behavior
Curie temperature< -196 °C6-112 °C< -196 °C279 °Cno datano datano datano datano datano data-115 °C-124 °Cno datano datano data435 °C21 to 49 °C-65 °C360 °Cno datano data450 °Cno datano data
Other measurements
Mean coefficient of thermal expansion, 20 to 100 °C13.9 ppm/K38.91 ppm/°F12.8 ppm/°C1.3 ppm/K10.6 μm/m.°C12.4 ppm/K11.2 μm/m.°C13.9 µm/(m·K)14.6 µm/m-°C11.8 ppm/K14.4 µm/m/°C10.4 ppm/K13.75 µm/m/°C11.6 µm/(m·K)7 10-6 in./in./°F5.86 10-6/°C14.2 µm/m°C13.7 10-6/°C13.3 ppm/Kno data14.5 ppm/K8 ppm/K12.7 µm/(m·K)14.3 µm/m·°C
Modulus of elasticity at 20 °C, hot rolled and annealed plate196 GPa429 ksi x 10^3207.5 GPa140 GPa216 GPa206 GPa205 GPa205 GPa218 GPa209 GPa196.5 GPa214 GPa206.5 GPa211 GPa31 10^3 ksi138 kN/mm226 10^3 ksi179 GPa205 GPa200 GPa195 to 210 GPano data204 GPa211 GPa
Yield strength 0.2 % offset, annealed plate, typical338 MPa7171 ksi60 to 95 ksi40 ksi421 MPa> 310 MPa356 MPa340 MPa577 MPa417 MPa250 MPa170 to 345 MPa292 MPa340 MPa> 105 ksi> 200 N/mm225 to 50 ksi276 to 414 MPa105 to 210 MPano data280 to 480 MPa280 MPa752 MPa586 MPa
Tensile strength, annealed plate, typical662 MPa8201 ksi120 to 150 ksi65 ksi862 MPa690 to 950 MPa792 MPa760 MPa975 MPa837 MPa590 MPa550 to 690 MPa675 MPa710 MPa> 165 ksi450 to 585 N/mm275 to 90 ksi621 to 758 MPa380 to 520 MPa2300 MPa660 to 900 MPa500 MPa1175 MPa1027 MPa
Elongation, annealed plate, typical45 %926 %30 to 60 %35 %53 %> 45 %61 %48.9 %37.3 %47.3 %17 %35 to 55 %46 %62 %> 20 %> 25 %35 to 60 %20 to 35 %40 to 55 %no data> 30 %35 %30 %43 %
Yield strength 0.2 % offset, cold drawn tubing, typical889 MPa10171 ksi60 to 95 ksi40 ksi421 MPa> 310 MPa356 MPa340 MPa577 MPa417 MPa250 MPa170 to 345 MPa292 MPa340 MPa> 105 ksi> 200 N/mm225 to 50 ksi276 to 414 MPa105 to 210 MPano data280 to 480 MPa280 MPa752 MPa586 MPa
Tensile strength, cold drawn tubing, typical1000 MPa11201 ksi120 to 150 ksi65 ksi862 MPa690 to 950 MPa792 MPa760 MPa975 MPa837 MPa590 MPa550 to 690 MPa675 MPa710 MPa> 165 ksi450 to 585 N/mm275 to 90 ksi621 to 758 MPa380 to 520 MPa2300 MPa660 to 900 MPa500 MPa1175 MPa1027 MPa
Minimum yield strength 0.2 % offset, annealed sheet and plate 5 to 100 mm> 240 MPa12171 ksi60 to 95 ksi40 ksi421 MPa> 310 MPa356 MPa340 MPa577 MPa417 MPa250 MPa170 to 345 MPa292 MPa340 MPa> 105 ksi> 200 N/mm225 to 50 ksi276 to 414 MPa105 to 210 MPano data280 to 480 MPa280 MPa752 MPa586 MPa
Minimum tensile strength, annealed sheet and plate 5 to 100 mm> 585 MPa13201 ksi120 to 150 ksi65 ksi862 MPa690 to 950 MPa792 MPa760 MPa975 MPa837 MPa590 MPa550 to 690 MPa675 MPa710 MPa> 165 ksi450 to 585 N/mm275 to 90 ksi621 to 758 MPa380 to 520 MPa2300 MPa660 to 900 MPa500 MPa1175 MPa1027 MPa
Minimum elongation, annealed sheet and plate 5 to 100 mm> 30 %1426 %30 to 60 %35 %53 %> 45 %61 %48.9 %37.3 %47.3 %17 %35 to 55 %46 %62 %> 20 %> 25 %35 to 60 %20 to 35 %40 to 55 %no data> 30 %35 %30 %43 %
Intergranular corrosion rate, boiling 50 % sulfuric acid with ferric sulfateRate printed in a manufacturer datasheet table0.03 mm/a15no datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano datano data

Why choose it, and why not

Good for

  • Acid service: sulfuric and phosphoric acid, with resistance to reducing and oxidising environments.
  • Chloride stress cracking in most tests: the nickel content resists it, except in boiling magnesium chloride over long times.
  • Welded and formed parts: the titanium stabilisation resists intergranular attack after welding.

Watch out for

  • Chloride pitting is only moderate. Use Alloy 625 or AL-6XN where minor pitting cannot be tolerated.
  • Boiling magnesium chloride cracks some samples over long times.
  • Annealed strength is modest, at 338 MPa yield for plate.
  • Dust and fume from cutting or welding carry cancer and sensitiser codes.
  • No spacecraft, rocket or satellite use was found in the sources read.

Incoloy 825 is an acid- and chloride-resistant nickel-iron-chromium alloy, stabilised with titanium so that welded parts resist intergranular attack. Its annealed plate yields at a typical 338 MPa, and it melts at 1370 to 1400 C. Pitting resistance is only moderate, and boiling magnesium chloride cracks some samples over long times. Its dust and fume carry hazard codes. No space application was found.

Technical details

For scientists and researchers. Everything above comes from the record below: every number with its method, its conditions and its source.

Other names and standards

The same grade under other systems, as datasheets and standards print them. Each code was checked against the page it comes from.

Other names and standards
SystemCodes
UNSN08825
EN2.4858
EN nameNiCr21Mo
DIN17750 (plate, sheet and strip), 17752 (rod, bar, wire and forging stock)
AFNORNC21FeDU
BS3076NA16 (rod and bar)
ISONiFe30Cr21Mo3
AMS5542
ASTMB 425 (rod and bar), B 424 (plate, sheet and strip), B 423 (pipe and tube)
Trade nameINCOLOY alloy 825, Nicrofer 4221

Notes

The method, full conditions and any caveat for the numbered rows above.

Notes for the numbered rows
#MeasurementMethodConditionsCaveat
1Specific heat capacity, 0 to 100 °CValue printed in a manufacturer datasheet in both unitstemperature 0 to 100 °Cunit in source 0.105 Btu/lb °F—
2Thermal conductivity at 100 °CTypical value printed in a manufacturer datasheet tabletemperature 100 °C (212 °F)unit in source 86 Btu·in/(sq. ft·h·°F)basis typical—
3Mean coefficient of thermal expansion, 20 to 100 °CMean value printed in a manufacturer datasheet, metric value in parenthesestemperature mean, 20 to 100 °C (70 to 212 °F)unit in source 7.7 x 10-6 in/in/°F—
4Modulus of elasticity at 20 °C, hot rolled and annealed plateValue printed in a manufacturer bulletin, table of Young's modulus against temperaturetemperature 20 °Cproduct form hot rolled and annealed plateload Young's modulus—
5Electrical resistivity at 20 °CTypical value printed in a manufacturer datasheet tabletemperature 20 °C (68 °F)unit in source µΩcm—
6Curie temperatureValue printed in a manufacturer bulletin as less than the given temperatureunit in source <-320 °Fmeaning the alloy is non-magnetic above this temperature—
7Yield strength 0.2 % offset, annealed plate, typicalTypical room-temperature value printed in a manufacturer bulletinproduct form plate, annealedtemperature room temperaturebasis typicalunit in source 49 ksi—
8Tensile strength, annealed plate, typicalTypical room-temperature value printed in a manufacturer bulletinproduct form plate, annealedtemperature room temperaturebasis typicalunit in source 96 ksi—
9Elongation, annealed plate, typicalTypical room-temperature value printed in a manufacturer bulletinproduct form plate, annealedtemperature room temperaturebasis typical—
10Yield strength 0.2 % offset, cold drawn tubing, typicalTypical room-temperature value printed in a manufacturer bulletinproduct form tubing, cold drawntemperature room temperaturebasis typicalunit in source 129 ksiThe same table gives 1000 MPa tensile strength and 15 percent elongation for this cold-drawn tubing, against 324 MPa yield for annealed bar, so cold work changes strength strongly.
11Tensile strength, cold drawn tubing, typicalTypical room-temperature value printed in a manufacturer bulletinproduct form tubing, cold drawntemperature room temperaturebasis typicalunit in source 145 ksi—
12Minimum yield strength 0.2 % offset, annealed sheet and plate 5 to 100 mmMinimum room-temperature value printed in a manufacturer datasheetproduct form sheet and plate, 5 to 100 mm, annealedtemperature room temperaturestandard VdTÜV data sheet 432 minimum—
13Minimum tensile strength, annealed sheet and plate 5 to 100 mmMinimum room-temperature value printed in a manufacturer datasheetproduct form sheet and plate, 5 to 100 mm, annealedtemperature room temperaturestandard VdTÜV data sheet 432 minimum—
14Minimum elongation, annealed sheet and plate 5 to 100 mmMinimum room-temperature value printed in a manufacturer datasheetproduct form sheet and plate, 5 to 100 mm, annealedtemperature room temperaturestandard VdTÜV data sheet 432 minimum—
15Intergranular corrosion rate, boiling 50 % sulfuric acid with ferric sulfate—environment boiling 50 % sulfuric acid with ferric sulfate, standard ASTM test named in the table headerunit in source 1 mils/yearBenchmark name is not in the canonical list, so it is a snake_case name (see gaps). The table gives 36 (0.91) for Type 316 and 26 (0.66) for Type 316L in the same test.

Corrosion and compatibility

What happens when it meets other materials and environments.

Corrosion and compatibility
EnvironmentConcernWhat happens
Sulfuric and phosphoric acids, and oxidising and reducing acids low The nickel, molybdenum and copper together resist reducing acids better than standard stainless steels, and chromium resists oxidising acids.1
Boiling 50 % sulfuric acid with ferric sulfate (ASTM intergranular test) low Alloy 825 shows an intergranular corrosion rate of 0.03 mm/a in the ASTM boiling sulfuric-ferric test, against 0.91 mm/a for Type 316.2
Chloride pitting and crevice corrosion, including sea water moderate Alloy 825 resists chloride pitting only moderately and is judged an improvement, not a dramatic one, over Type 316.3
Chloride stress corrosion cracking, boiling magnesium chloride moderate Chloride stress cracking is resisted in most tests, but Alloy 825 cracks in some samples in boiling magnesium chloride over long times.4
Corrosion details
#EnvironmentDetailsTest conditions
1 Sulfuric and phosphoric acids, and oxidising and reducing acids Special Metals names sulfuric acid and phosphoric acid among the environments where the alloy is particularly useful, and says the nickel with molybdenum and copper gives outstanding resistance to reducing environments. VDM lists good resistance in sulfuric, phosphoric, nitric and organic acids. No quantitative general corrosion rate in these acids was taken from a page with a stated test condition. basis qualitative statements in datasheetsenvironments sulfuric, phosphoric, nitric and organic acids, alkalis, sea water
2 Boiling 50 % sulfuric acid with ferric sulfate (ASTM intergranular test) Jacquet's intergranular table gives 1 (0.03) mils/year (mm/a) for Alloy 825 in boiling 50 % sulfuric acid with ferric sulfate, against 36 (0.91) for Type 316, 26 (0.66) for Type 316L and 19 (0.48) for AL-6XN. In boiling 65 % nitric acid the same table gives 12 (0.30) for Alloy 825 against 34 (0.85) for Type 316. environment boiling 50 % sulfuric acid with ferric sulfate, ASTM standard test named in the table headerunit in source mils/year (mm/a)
3 Chloride pitting and crevice corrosion, including sea water Jacquet says the chromium and molybdenum content gives the alloy a level of chloride pitting resistance that falls short of AL-6XN and Alloy 625, and that the alloy is used in high-chloride environments such as sea water where some pitting can be tolerated. Special Metals lists sea water among the environments where the alloy is particularly useful. The G 48 Practice B crevice-onset temperature in the Jacquet table has no printed unit, so it is not entered. test ASTM G 48 Practice B, 10 % ferric chloride, for the crevice-onset tablebasis vendor comparison and service experience statement
4 Chloride stress corrosion cracking, boiling magnesium chloride In U-bend tests, Jacquet gives Alloy 825 as Mixed in boiling 42 % magnesium chloride (Type 316 Fail), and as Resist in boiling 33 % lithium chloride and boiling 26 % sodium chloride. Jacquet says the alloy will crack in long-time tests in a percentage of samples in the severe boiling magnesium chloride test. VDM describes the high nickel content as giving virtual immunity to stress corrosion cracking. test U-bend samples, boiling 42 % magnesium chloride, boiling 33 % lithium chloride, boiling 26 % sodium chloride

Risks and side effects

Hazards to people, what happens when a cell overheats, and how the material is handled and stored.

For people

The hazard for people depends on the dust and fume, not on the solid alloy. The SDS for the nickel-alloy family classifies the solid as an article and the dust or fume as carcinogenic and a skin sensitiser.

Solid metal
The VDM SDS says the solid alloy as supplied is not classified. Its nickel content carries skin sensitisation (H317), carcinogenicity category 2 (H351) and target organ toxicity (H372).
Cutting, welding, grinding
The SDS says these operations produce dust and fume with the element codes, including H350 may cause cancer and H334 may cause allergy or asthma symptoms. The SDS advises use only outdoors or in a well-ventilated area, and respiratory protection where ventilation is inadequate.

If it fails

These failure routes are in the sources read. The chloride ones are measured in vendor tests, and the heat-related one is a metallurgy warning.

Boiling magnesium chloride
Jacquet says the alloy cracks in long-time tests in a percentage of samples in boiling magnesium chloride, where it is rated Mixed against Fail for Type 316.
Chloride pitting
The alloy is judged only an improvement over Type 316 for chloride pitting. AL-6XN and Alloy 625 are used where minor pitting cannot be tolerated.
Heat exposure
Above about 540 C phase formation can lower ductility and impact strength, so creep-rupture service is not normal for the alloy.

Handling and storage

Anneal after forming
Anneal at 930 to 980 C and quench, so the titanium keeps the alloy resistant to intergranular corrosion after heating.
Keep iron out
Use clean, dedicated tools and keep carbon steel contact off the surface, because ferrous particles pressed into the surface cause corrosion.

Test details
The original wording and numbers from the sources, for readers who want them.

Failure risks

Failure risks
FailureTrigger and consequence
Chloride stress cracking in boiling magnesium chloridemoderate severityLong exposure to boiling 42 % magnesium chloride, as in the severe U-bend testJacquet says the alloy cracks in long-time tests in a percentage of samples. The alloy is rated Mixed in that test, against Fail for Type 316.
Intergranular attack after heating in the sensitising rangemoderate severityHeavy sections cooled slowly from hot working, or semi-finished products used between 600 and 650 C and then reused in that range after repair welding, without a stabilising annealSpecial Metals says heavy sections may become sensitised during cooling from hot-working temperature and be subject to intergranular corrosion in certain media. VDM recommends stabilising anneal on semi-finished products used between 600 and 650 C before reuse in that range.
Chloride pitting and crevice attackmoderate severityChloride service, including sea water, where minor pitting cannot be toleratedJacquet judges the alloy only an improvement over Type 316 for pitting and says it is not suitable where even minor pitting cannot be tolerated; AL-6XN and Alloy 625 are used there instead.
Phase formation and loss of ductility after long exposure above 540 Cmoderate severityExposure to temperatures above about 1000 F (540 C), where creep-rupture is a design factorSpecial Metals says microstructural changes (phase formation) can significantly lower ductility and impact strength, so the alloy is not normally used where creep-rupture properties are design factors.

Side effects on surrounding parts

Side effects on surrounding parts
AffectsEffect
Mass of hardwareDensity is 8.14 g/cm3, so part mass is high for a given volume. The datasheet gives this value without a mass comparison against other alloys.

Handling and storage

  • Anneal after fabrication at 1700 to 1800 F (930 to 980 C) and air cool or water quench rapidly, so that the stabilising titanium keeps its corrosion resistance. VDM gives a soft annealing range of 920 to 980 C, preferably 940 plus or minus 10 C, with rapid water quench.
  • The two sources differ on work hardening. VDM says the rate is higher than for austenitic stainless steels, while Special Metals says it is somewhat less but still relatively high, and both say forming equipment must be well powered. Cold work should be done on annealed material, with soft annealing after more than 15 percent deformation (VDM).
  • Use a separate workplace and clean tools, and keep carbon-steel tools away from nickel alloy work, so that ferrous particles do not contaminate the surface and cause corrosion. Welding interpass temperature should not exceed 150 C (VDM).
  • Use only outdoors or in a well-ventilated area, avoid generating dust and sparks, and wear respiratory protection where ventilation is inadequate. The SDS gives these as precautions for cutting, welding and grinding of the alloy.

Supply and geography

How common the raw materials are and where they come from.

Nickel

World resources are more than 350 million tons of nickel (USGS 2026)

Top producers (2025)
Indonesia 66.7%, Philippines 6.9%, Russia 5.1%, Canada 3.6%, New Caledonia 3.6%
Recycling
In 2025, nickel recovered from scrap accounted for approximately 60 percent of apparent consumption, and most secondary nickel was stainless-steel scrap (USGS).
Substitutes
Low-nickel, duplex, or ultrahigh-chromium stainless steels have been substituted for austenitic grades in construction. Titanium alloys can substitute for nickel or nickel-base alloys in corrosive environments (USGS).

Molybdenum

Identified resources are about 5.4 million tons in the United States and about 20 million tons in the rest of the world (USGS 2026)

Top producers (2025)
China 37.3%, Chile 16.2%, United States 15.4%, Peru 15%, Mexico 6.5%
Recycling
Molybdenum is recycled as a component of catalysts, ferrous scrap and superalloy scrap, and the amount recycled may be as much as 30 percent of apparent supply (USGS).