AISI 347 stainless steel 347

Fe-based austenitic alloy: Fe balance, Cr 17.00 to 19.00 %, Ni 9.00 to 13.00 % (9.00 to 12.00 % in UPMET and Combmet), C 0.08 % maximum, Mn 2.00 % maximum, S 0.03 % maximum, Nb plus Ta at 10 x C minimum and 1.00 % maximum (ASTM A240 limits)

Also known as UNS S34700, EN 1.4550, EN name X6CrNiNb18-10, AISI 347, JIS SUS347, ASTM A240 · 8 more

AISI 347 (UNS S34700, EN 1.4550) is an austenitic stainless steel with 17 to 19 % chromium and 9 to 13 % nickel, stabilised with niobium (columbium) so that it resists intergranular attack after exposure in the chromium-carbide range of 427 to 816 °C.

12 sources · Updated 2026-10-25 · CC BY 4.0

Evidence level

2 of 5

Lab-measured

Carry heat in air

800 °C

Resist welding damage

427 to 816 °C

Stiffness

193 GPa

Strength when annealed

640 MPa

Recipe, share of the weight

  • Fe not statedIron
  • Cr not statedChromium
  • Ni not statedNickel
  • Nb not statedNiobium (columbium), with tantalum
  • C not statedCarbon
  • Mn not statedManganese
  • Si not statedSilicon
  • P not statedPhosphorus
  • S not statedSulphur

Best for

Welded hot-service parts that cannot be re-annealed afterwards: niobium stabilisation resists intergranular attack, and the grade is rated to 800 °C in air

Weakest at

Strength when hot: tensile strength falls from 93.3 ksi at 68 °F to 69.5 ksi at 800 °F (Rolled Alloys), and no vacuum, radiation or atomic-oxygen data were found

Risk at a glance

  • People Low. Nickel classes apply to dust and fumes
  • If it fails Moderate. Intergranular attack from chromium carbide
  • Corrosion Low. Niobium stabilisation keeps the grade resistant to intergranular corrosion after exposure in the chromium-carbide range.

Quick facts: 347

Key properties of 347
PropertyValueBasis
Density7.96 g/cm³1 sourced value
Yield strength205 to 250 MPa2 sourced values across conditions
Tensile strength515 to 640 MPa2 sourced values across conditions
Young's modulus193 GPa1 sourced value
Thermal conductivity16.3 W/(m·K)1 sourced value
Thermal expansion (CTE)16.6 to 18.9 ppm/K2 sourced values across conditions
Melting point1,398 to 1,446 °C1 sourced value
Specific heat500 J/(kg·K)1 sourced value
Electrical resistivity7.2e-7 Ω·m1 sourced value
Maximum service temperature800 °C1 sourced value

What is the density of AISI 347 stainless steel?

AISI 347 stainless steel has a density of 7.96 g/cm³. The source and test conditions are listed in the properties table on this page.

What is the thermal conductivity of AISI 347 stainless steel?

AISI 347 stainless steel has a thermal conductivity of 16.3 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 AISI 347 stainless steel?

AISI 347 stainless steel has a coefficient of thermal expansion of 16.6 to 18.9 ppm/K. The range covers 2 sourced values across the tempers, forms and test conditions the sources report; room-temperature values are used where a source states a temperature.

What is the melting point of AISI 347 stainless steel?

AISI 347 stainless steel has a melting point of 1,398 to 1,446 °C. The source and test conditions are listed in the properties table on this page.

What is the yield strength of AISI 347 stainless steel?

AISI 347 stainless steel has a yield strength of 205 to 250 MPa. The range covers 2 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 AISI 347 stainless steel?

AISI 347 stainless steel is also written as UNS S34700, EN 1.4550, EN name X6CrNiNb18-10, AISI 347, JIS SUS347, ASTM A240. Each code is printed in the source listed beside it in the designations table.

What is AISI 347 stainless steel used for?

Uses recorded in the sources include Aircraft exhaust stacks and furnace heating elements; Hanger rods, fired heater tubes, thermowells and reactor components; Recuperator tube sheets and fired heater tubes in refineries.

Why it exists

AISI 347 is a stainless steel that keeps its corrosion resistance after welding and heating. It has 17 to 19 % chromium and 9 to 13 % nickel, and niobium (columbium) ties up the carbon so chromium carbide does not form at the grain boundaries. The UPMET datasheet prints a density of 7.96 g/cm3 for grade 347 and a melting range of 1398 to 1446 °C. Smith prints a maximum use temperature in air of 800 °C.

Where it's used

Furnace and exhaust hardware

UPMET lists aircraft exhaust stacks, cabin heaters, furnace heating elements and boiler casings among its industry applications for 347 sheet, coil and bar.

Refinery and reactor parts

Smith lists fired heater tubes, thermowells, hanger rods and reactor components. Rolled Alloys lists recuperator tube sheets, distributor trays and equipment around reactors.

Recipe

Fe-based austenitic alloy: Fe balance, Cr 17.00 to 19.00 %, Ni 9.00 to 13.00 % (9.00 to 12.00 % in UPMET and Combmet), C 0.08 % maximum, Mn 2.00 % maximum, S 0.03 % maximum, Nb plus Ta at 10 x C minimum and 1.00 % maximum (ASTM A240 limits)

AISI 347 is an iron-based austenitic alloy. Composition in weight percent is the ASTM A240 limits printed in the Aalco datasheet, with the niobium row from UPMET; Combmet's nominal table prints silicon 1.00 % maximum and nickel 9 to 12 %, which differ. The process route (melting and casting) was not read from a primary source.

What 347 is made of
IngredientShare of the weightWhat it does
Iron Fe not stated The matrix of the alloy; the other elements are dissolved in it.
Chromium Cr not stated Gives the stainless steel its corrosion and oxidation resistance (Aalco, UPMET, Combmet).
Nickel Ni not stated Keeps the structure austenitic and non-magnetic when annealed (Smith).
Niobium (columbium), with tantalum Nb not stated The stabiliser that ties up carbon so that chromium carbide does not form at grain boundaries (Combmet, Rolled Alloys).
Carbon C not stated Kept low; niobium binds the carbon that remains.
Manganese Mn not stated Printed in the ASTM A240 limits; the sources read give no function for it.
Silicon Si not stated Printed in the composition tables; the datasheets give no function.
Phosphorus P not stated An impurity limit in the ASTM A240 composition.
Sulphur S not stated An impurity limit in the ASTM A240 composition.

Weight shares are as printed in the sources.

What it can do

Carry heat in air

800 °C

measured

Smith prints a maximum use temperature in air of 800 °C. Rolled Alloys says the grade is useful to 1500 °F for oxidation.

Resist welding damage

427 to 816 °C

Combmet says the niobium stabilisation resists intergranular corrosion after exposure in the chromium-carbide range from 800 to 1500 °F.

Stiffness

193 GPa

measured

The modulus of elasticity at 20 °C is 193 GPa, from the Combmet datasheet.

Strength when annealed

640 MPa

measured

Typical annealed tensile strength is 640 MPa and typical 0.2 % yield is 250 MPa (Combmet, based on ATI data). ASTM A240 minimums are 515 MPa and 205 MPa.

How it compares

Type 347 is the niobium-stabilised sibling of Type 321, which is stabilised with titanium. Rolled Alloys says 347 has slightly improved corrosion resistance over 321 in strongly oxidising environments, and that both offer good resistance to polythionic acid stress corrosion cracking. The sibling 321 profile is in this site as stainless-321.

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
Measurement347304 (UNS S30400)301 (UNS S30100)303 (UNS S30300)316 (UNS S31600)316L (UNS S31603)302304L (UNS S30403)309310S (UNS S31008, EN 1.4845)317L321347H904L (UNS N08904, EN 1.4539)Nitronic 60
Thermal behavior and safety
Melting range, grade 3471398 to 1446 °C21673 K1399 to 1421 °C1455 °C1390 °C1390 °C1420 °C1399 to 1421 °C2550 to 2650 °F1410 °C1390 to 1440 °C1398 to 1446 °C2550 to 2635 degF1300 to 1390 °Cno data
Thermal conductivity at 20 °CValue printed in a manufacturer datasheet16.3 W/(m·K)14 W/m.K16.3 W/m.K15 W/m°C14.6 W/m.K14.6 W/m·K16.2 W/(m·K)16.3 W/m·K15.6 W/m·K13 W/(m·K)14 W/(m·K)16.3 W/(m·K)14 W/m.°C12 W/(m·K)9 Btu/ft hr °F
Thermal conductivity, 20 to 500 °CValue printed in a manufacturer datasheet21.4 W/(m·K)314 W/m.K16.3 W/m.K15 W/m°C14.6 W/m.K14.6 W/m·K16.2 W/(m·K)16.3 W/m·K15.6 W/m·K13 W/(m·K)14 W/(m·K)16.3 W/(m·K)14 W/m.°C12 W/(m·K)9 Btu/ft hr °F
Specific heat capacity, 0 to 100 °CValue printed in a manufacturer datasheet500 J/(kg·K)4490 J/kg.K500 J/kg.K500 J/kg°C450 J/kg.K450 J/kg °K500 J/kg K500 J/kg·K502 J/kg·K480 J/(kg·K)500 J/(kg·K)500 J/kg K485 J/(kg.°C)450 J/(kg·K)0.12 Btu/lb °F
Physical and electrical
Density, grade 347Value printed in a manufacturer datasheet7.96 g/cm³17.85 Mg/m38.03 g/cm³7.9 kg/dm38.027 g/cm³8.03 g/cm³7.9 g/cm³7.9 g/cm³8.03 g/cm³7.8 kg/dm38.027 g/cm³7.92 g/cm³7.98 kg/dm37.95 g/cm³7.622 gm/cm³
Electrical resistivity at 20 °CValue printed in a manufacturer datasheet72 µΩ·cm65 10-8 ohm.m72 µΩ·cm72 microhm-cm69 10-8 ohm.m74 μΩ·cm72 µΩ·cm72 microhm-cm78 µΩ·cm0.86 Ω·mm²/m475 Ohm-circ mil/ft72 microhm·cmno data95.2 µΩ·cm98.2 microhm-cm
Electrical resistivity at 900 °CValue printed in a manufacturer datasheet126 µΩ·cm565 10-8 ohm.m72 µΩ·cm72 microhm-cm69 10-8 ohm.m74 μΩ·cm72 µΩ·cm72 microhm-cm78 µΩ·cm0.86 Ω·mm²/m475 Ohm-circ mil/ft72 microhm·cmno data95.2 µΩ·cm98.2 microhm-cm
Hardness, maximum, Brinell (plate)< 201 HB13no data85 HRB< 202 HBN< 217 HBno datano datano datano datano datano datano data< 201 HB< 230 HB> 85 HRB
Hardness, maximum, Rockwell B (sheet and strip)< 92 HRB14no data85 HRB< 202 HBN< 217 HBno datano datano datano datano datano datano data< 201 HB< 230 HB> 85 HRB
Hardness, typical, annealed (HRBW)Typical value printed in a supplier datasheet84 HRBWno data85 HRB< 202 HBN< 217 HBno datano datano datano datano datano datano data< 201 HB< 230 HB> 85 HRB
Other measurements
Modulus of elasticity in tension, 20 °CValue printed in a manufacturer datasheet193 GPa200 GPa193 GPa193 GPa200 GPa193 GPa200 GPa200 GPa200 GPa195 GPa200 GPa193 GPa200 GPa195 GPa180 GPa
Mean coefficient of linear thermal expansion, 20 to 100 °CValue printed in a manufacturer datasheet16.6 ppm/Kno data16.6 10-6/K16 10-6/°C16.5 10-6/K16.5 10-6 cm/cm/°C16.6 µm/(m·°C)16.6 10-6 cm/cm/°C15.6 µm/(m·K)16.5 ppm/K16.5 10^-6 cm/cm/°C16.6 ppm/K9.2 in/in.degF x 10^-615.8 ppm/K15.8 µm/m/°C
Mean coefficient of linear thermal expansion, 20 to 600 °CValue printed in a manufacturer datasheet18.9 ppm/Kno data16.6 10-6/K16 10-6/°C16.5 10-6/K16.5 10-6 cm/cm/°C16.6 µm/(m·°C)16.6 10-6 cm/cm/°C15.6 µm/(m·K)16.5 ppm/K16.5 10^-6 cm/cm/°C16.6 ppm/K9.2 in/in.degF x 10^-615.8 ppm/K15.8 µm/m/°C
Yield strength 0.2 % offset, minimum, ASTM A240 sheet> 205 MPa6> 205 MPa205 MPa> 172 MPa205 MPa170 MPa290 MPa> 170 MPa290 MPa290 MPa> 205 MPa> 205 MPa> 30 ksi> 240 MPa> 345 MPa
Yield strength 0.2 % offset, typical, annealedTypical value printed in a supplier datasheet250 MPa7> 205 MPa205 MPa> 172 MPa205 MPa170 MPa290 MPa> 170 MPa290 MPa290 MPa> 205 MPa> 205 MPa> 30 ksi> 240 MPa> 345 MPa
Tensile strength, minimum, ASTM A240 sheet> 515 MPa8> 515 MPa515 MPa> 517 MPa515 MPa485 MPa655 MPa> 485 MPa621 MPa610 MPa> 515 MPa> 515 MPa> 75 ksi530 to 730 MPa> 655 MPa
Tensile strength, typical, annealedTypical value printed in a supplier datasheet640 MPa9> 515 MPa515 MPa> 517 MPa515 MPa485 MPa655 MPa> 485 MPa621 MPa610 MPa> 515 MPa> 515 MPa> 75 ksi530 to 730 MPa> 655 MPa
Tensile strength at 800 °F, typical69.5 ksi10> 515 MPa515 MPa> 517 MPa515 MPa485 MPa655 MPa> 485 MPa621 MPa610 MPa> 515 MPa> 515 MPa> 75 ksi530 to 730 MPa> 655 MPa
Elongation, minimum, ASTM A240 sheet> 40 %11> 40 %40 %> 35 %40 %40 %55 %> 40 %49 %42 %> 40 %> 35 %> 40 %> 35 %> 35 %
Elongation, typical, annealedTypical value printed in a supplier datasheet45 %12> 40 %40 %> 35 %40 %40 %55 %> 40 %49 %42 %> 40 %> 35 %> 40 %> 35 %> 35 %
Maximum use temperature in airValue printed in a manufacturer datasheet800 °Cno data840 °Cno data1023 Kno data925 °C< 426 °C2000 °F1050 °Cno data850 °C850 °C< 400 °Cno data

Why choose it, and why not

Good for

  • Welded hot-service parts that cannot be annealed afterwards, rated to 800 °C in air (Smith).
  • Refinery service where polythionic acid cracking is a concern (Rolled Alloys).
  • Heating elements, exhaust stacks and furnace parts (UPMET application list).

Watch out for

  • Strength falls when hot: 93.3 ksi at 68 °F against 69.5 ksi at 800 °F (Rolled Alloys).
  • Nickel content of 9 to 13 % puts the hazard class on the 10 % CLP line, so check the heat certificate (Uddeholm sheet).
  • Cold work is the only way to harden it, so the temper sets the strength (Smith).
  • No vacuum, radiation or atomic-oxygen data were found for this profile.

AISI 347 is a welded, niobium-stabilised austenitic stainless steel with a printed maximum use temperature of 800 °C in air, 193 GPa modulus and typical annealed strength of 640 MPa. Its hot strength drops steeply above room temperature, its nickel content sets the hazard class of its dust and fumes, and this profile lacks space-environment numbers.

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
UNSS34700
EN1.4550
EN nameX6CrNiNb18-10
AISI347
JISSUS347
ASTMA240 (plate, sheet and strip), A269 (tube), A312 (pipe), TP347 (tube and pipe grade)
AMS5512 (sheet, coil and bar), 5646
ASMESA-240
Trade nameAlloy 347, Type 347

Notes

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

Notes for the numbered rows
#MeasurementMethodConditionsCaveat
1Density, grade 347—grade 347temperature not stated in the tableunit in source 0.288 lb/in3—
2Melting range, grade 347Melting range printed in a manufacturer datasheetgrade 347unit in source 2550-2635 °Fpressure not stated—
3Thermal conductivity, 20 to 500 °C—temperature range 20 to 500 °Cunit in source 147.7 Btu-in/hr-ft2-°FThe UPMET thermal table is not labelled by grade; the datasheet title is for 347 sheet, coil and bar.
4Specific heat capacity, 0 to 100 °C—temperature range 0 to 100 °Cunit in source 0.12 Btu/lb·°FThe UPMET specific heat table is not labelled by grade; the datasheet title is for 347 sheet, coil and bar.
5Electrical resistivity at 900 °C—temperature 900 °Cunit in source microhm·cmThe UPMET resistivity table is not labelled by grade; the datasheet title is for 347 sheet, coil and bar.
6Yield strength 0.2 % offset, minimum, ASTM A240 sheetMinimum value printed in a supplier datasheet quoting ASTM A240spec ASTM A240form sheetmeasure 0.2 % proof stress, minimum—
7Yield strength 0.2 % offset, typical, annealed—temper annealedbasis typical values based on ATI source, ASTM A240unit in source 37 ksi—
8Tensile strength, minimum, ASTM A240 sheetMinimum value printed in a supplier datasheet quoting ASTM A240spec ASTM A240form sheet—
9Tensile strength, typical, annealed—temper annealedbasis typical values based on ATI source, ASTM A240unit in source 93 ksi—
10Tensile strength at 800 °F, typicalTypical value printed in a manufacturer datasheettemperature 800 °F as printed (about 427 °C)basis typical tensile and impact propertiesform not stated—
11Elongation, minimum, ASTM A240 sheetMinimum value printed in a supplier datasheet quoting ASTM A240spec ASTM A240form sheetgauge length A50 mm—
12Elongation, typical, annealed—temper annealedgauge length 2 in (50.8 mm)basis typical values based on ATI source, ASTM A240—
13Hardness, maximum, Brinell (plate)Maximum value printed in a manufacturer datasheetproduct form platescale Brinell—
14Hardness, maximum, Rockwell B (sheet and strip)Maximum value printed in a manufacturer datasheetproduct form sheet and stripscale Rockwell B—

Corrosion and compatibility

What happens when it meets other materials and environments.

Corrosion and compatibility
EnvironmentConcernWhat happens
Chromium-carbide sensitisation range, 427 to 816 °C (welding and stress relief) low Niobium stabilisation keeps the grade resistant to intergranular corrosion after exposure in the chromium-carbide range.1
Polythionic acid in oil refineries low Type 347 resists polythionic acid stress corrosion cracking, a refinery hazard.2
Strongly oxidising service and high-temperature air low Type 347 has slightly better corrosion resistance than Type 321 in strongly oxidising environments, and is useful to 1500 °F.3
Chloride and general wet service low Smith describes the grade as having excellent pitting resistance and good resistance to most chemicals.4
Corrosion details
#EnvironmentDetailsTest conditions
1 Chromium-carbide sensitisation range, 427 to 816 °C (welding and stress relief) Combmet says the 347 alloys are stabilised by columbium and resist intergranular corrosion after exposure at 800 to 1500 °F (427 to 816 °C). Rolled Alloys says the grade has good resistance to intergranular corrosion in the as-welded condition. basis datasheet statements; no corrosion rate printedstabiliser columbium (niobium)
2 Polythionic acid in oil refineries Rolled Alloys says both 347 and 321 offer good resistance to polythionic acid stress corrosion cracking encountered in oil refineries. Smith says the alloy has good resistance to polythionic acid stress corrosion cracking and is useful around reactor plants. basis datasheet statements; no test duration or concentration printed
3 Strongly oxidising service and high-temperature air Rolled Alloys says 347 has slightly improved corrosion resistance over type 321 in strongly oxidising environments, and that its high-temperature oxidation resistance is similar to 304 stainless steel. Smith prints a maximum use temperature in air of 800 °C. basis datasheet statements; no oxidation rate printed
4 Chloride and general wet service The Smith datasheet states excellent pitting resistance and good resistance to most chemicals, without a critical pitting temperature or a chloride limit. basis general statement; no test data printed

Risks and side effects

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

For people

Dust and fumes from working the steel carry the hazards, because the sources classify nickel, not the massive metal.

Nickel in the alloy
Uddeholm's safety information sheet for steel articles classes nickel with H317, H351 and H372 (DANGER). It says massive steel needs no label, but dust and fumes from grinding, polishing, welding or cutting carry the risk.
Nickel limit rule
The same sheet puts steels above 10 % nickel in STOT RE1 and steels above 1 % nickel in Carcinogen Category 2. The 347 range of 9 to 13 % nickel straddles the 10 % line, so the class depends on the actual heat.

If it fails

These are failure routes printed in the sources. None is a measured space result.

Intergranular attack
Combmet says the niobium addition resists intergranular corrosion after exposure at 427 to 816 °C, the range where chromium carbide forms in unstabilised grades.
Polythionic acid
Rolled Alloys and Smith say 347 has good resistance to polythionic acid stress corrosion cracking, which arises in oil-refinery equipment.
Hot strength
Rolled Alloys gives a typical tensile strength of 93.3 ksi at 68 °F and 69.5 ksi at 800 °F.

Handling and storage

Welds that cannot be annealed
Rolled Alloys says the grade keeps good resistance to intergranular corrosion in the as-welded condition, which is why it is chosen for welded parts.
Temper
Smith says the alloy is essentially non-magnetic when annealed and can only be hardened by cold working.

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

Failure risks

Failure risks
FailureTrigger and consequence
Intergranular attack from chromium carbidemoderate severityExposure in the chromium-carbide range of 427 to 816 °C, for example after welding, where the carbon is not tied up by niobiumChromium carbide forms at grain boundaries and the metal loses intergranular corrosion resistance. Combmet states that the niobium addition is what prevents this.
Polythionic acid stress corrosion crackingmoderate severityPolythionic acid formed in oil-refinery equipmentRolled Alloys and Smith say 347 has good resistance to this cracking. The sources print no crack or failure data for the grade.
Loss of strength when hotlow severityService at 800 °F and aboveTypical tensile strength falls from 93.3 ksi at 68 °F to 69.5 ksi at 800 °F, and typical 0.2 % yield falls from 36.5 ksi to 29.7 ksi over the same range (Rolled Alloys).

Handling and storage

  • The grade is chosen where welded parts cannot be annealed afterwards, since Rolled Alloys says it keeps good resistance to intergranular corrosion in the as-welded condition.
  • Smith says Type 347 is essentially non-magnetic in the annealed condition and can only be hardened by cold working, so strength depends on the temper.
  • Specify the temper and product form: the minimum values of ASTM A240 apply to sheet, and the typical annealed values in the Combmet sheet were measured on the ATI basis.

Supply and geography

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

Nickel (world mine production, nickel content, 2025 estimate)

Top producers (2025)
Indonesia 66.7%, Philippines 6.9%, Russia 5.1%, New Caledonia 3.6%, Canada 3.6%
Recycling
USGS: nickel recovered from scrap accounted for about 60 % of U.S. apparent consumption in 2025; most secondary nickel went into new stainless steel and alloys.
Substitutes
USGS: 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.

Chromium (world mine production, chromium content, 2025 estimate)

Top producers (2025)
South Africa 45.1%, Turkey 17.6%, Kazakhstan 13.7%, India 5.9%
Recycling
USGS: recycled chromium in stainless-steel scrap receipts accounted for 21 % of U.S. apparent consumption in 2025.
Substitutes
USGS: chromium has no substitute in stainless steel, the leading end use.

Niobium (columbium) (world mine production, niobium content, 2025 estimate)

Top producers (2025)
Brazil 92.9%, Canada 5.4%, Congo (Kinshasa) 0.9%
Recycling
USGS: scrap recovery of niobium was negligible; niobium was recycled mainly as part of niobium-bearing steels and superalloys.
Substitutes
USGS: ceramic matrix composites, molybdenum, tantalum and tungsten can replace niobium in high-temperature superalloy uses, with a performance loss or higher cost.