Jiangyin Jiangnan Metal Co., Ltd. Open-die forging factory, Jiangyin, China

Nickel superalloy / Open-die forgings / ASTM B637

UNS N07208 forgings

Gamma-prime strengthened Ni-Cr-Co-Mo superalloy, forged to drawing as rings, flanges, bars, discs, sleeves and shafts. Also designated Alloy 282 and HAYNES® 282® alloy.

Summary

UNS N07208 is a wrought, gamma-prime strengthened nickel-base superalloy of nominal composition Ni-20Cr-10Co-8.5Mo-2.1Ti-1.5Al, used for structural components that carry load between 649 °C and 927 °C (1200 to 1700 °F). It is the Unified Numbering System designation for the alloy sold commercially as Alloy 282 and HAYNES® 282®. The alloy reaches Waspaloy-class creep strength while retaining enough weldability and formability to be fabricated into large welded structures, a combination earlier gamma-prime alloys did not offer.

Jiangyin Jiangnan Metal Co., Ltd. is an open-die forging factory in Jiangyin, Jiangsu Province, China. The company produces UNS N07208 forged rings, seamless rolled rings, flanges, round bars, discs, sleeves, bushings, shafts and tube sheets to customer drawings, supplied to ASTM B637 with EN 10204 3.1 or 3.2 material certificates and ultrasonic testing to EN 10228-3, SEP 1921 or ASTM A388. Enquiries: sales@steelforgepieces.com or +86 189 2135 9659.

  • UNS numberN07208
  • Also known asAlloy 282 / HAYNES® 282®
  • Forging standardASTM B637, AMS 5915
  • Strengtheningγ′ Ni3(Al,Ti), 15 to 20 vol%
  • Service window649 to 927 °C
  • Density8.27 g/cm³
  • UTS, aged (RT)1147 MPa / 166.4 ksi
  • 0.2% YS, aged (RT)715 MPa / 103.7 ksi
Temperature map of UNS N07208 (Alloy 282) Creep and service window 649 to 927 degrees Celsius; two-step age hardening at 1010 and 788 degrees Celsius; solution annealing 1121 to 1149 degrees Celsius; open-die forging and hot working 955 to 1177 degrees Celsius; melting range 1300 to 1375 degrees Celsius; gamma-prime solvus at 997 degrees Celsius. γ′ solvus 997 °C Creep and service window · 649 to 927 °C Two-step age hardening · 1010 °C / 2 h + 788 °C / 8 h 788 1010 Solution annealing · 1121 to 1149 °C Open-die forging and hot working · 955 to 1177 °C Melting range · 1300 to 1375 °C 0 200 400 600 800 1000 1200 1400 °C
Processing and service temperatures for UNS N07208 on one scale. Solid orange marks the creep and service window; pale orange marks the open-die forging range. Data: Haynes International alloy data, ASTM B637.
§ 01 / Identification

What is UNS N07208?

UNS N07208 is the Unified Numbering System designation for a wrought nickel-base superalloy strengthened by the ordered gamma-prime phase Ni3(Al,Ti). It was introduced commercially in 2005. The design target was creep strength above that of Alloy 263, without the strain-age cracking that makes Waspaloy and R-41 difficult to weld and fabricate.

The alloy carries a low gamma-prime volume fraction of roughly 15 to 20 percent, against 25 to 35 percent in Waspaloy. The lower fraction slows precipitation kinetics, so material stays ductile after solution annealing and survives post-weld heat treatment without cracking. UNS N07208 contains no niobium. All precipitation strengthening comes from aluminium and titanium.

UNS number
N07208
Common trade names
Alloy 282, HAYNES® 282® alloy, Ni 282
Alloy family
Ni-Cr-Co-Mo, gamma-prime precipitation hardening
Nominal composition
Ni bal. 20 Cr 10 Co 8.5 Mo 2.1 Ti 1.5 Al
Bar and forging spec
ASTM B637, AMS 5915
Sheet, plate and strip
AMS 5951
Pressure code coverage
ASME Code Case 3024 to 870 °C; ASME B31 Case 219
Melting route
EAF + VOD, then ESR remelt
Closest alternatives
Waspaloy, R-41 (Rene 41), Alloy 263, Inconel 718

Specification note. UNS N07208 forgings are covered by ASTM B637, which applies to precipitation-hardening nickel alloy bars, forgings and forging stock. ASTM B564 covers solid-solution nickel alloy forgings and does not list N07208. Where a drawing or purchase order calls out B564 for this grade, we raise it during technical review before release.

§ 02 / Chemistry

UNS N07208 chemical composition

Composition limits per ASTM B637 for UNS N07208, in weight percent. Each heat is supplied with a certified ladle analysis on the EN 10204 3.1 or 3.2 certificate.

Table 1. UNS N07208 (Alloy 282) composition limits, wt%
ElementLimits, %Nominal, %
Nickel (Ni)Balance57
Chromium (Cr)18.5 to 20.520
Cobalt (Co)9.0 to 11.010
Molybdenum (Mo)8.0 to 9.08.5
Titanium (Ti)1.90 to 2.302.1
Aluminium (Al)1.38 to 1.651.5
Iron (Fe)1.5 maxn/a
Carbon (C)0.04 to 0.080.06
Manganese (Mn)0.30 maxn/a
Silicon (Si)0.15 maxn/a
Boron (B)0.003 to 0.0100.005
Tungsten (W)0.5 maxn/a
Niobium (Nb)0.2 maxn/a
Tantalum (Ta)0.10 maxn/a
Copper (Cu)0.1 maxn/a
Zirconium (Zr)0.020 maxn/a
Phosphorus (P)0.015 maxn/a
Sulfur (S)0.015 maxn/a
§ 03 / Mechanical properties

UNS N07208 mechanical properties

Typical room-temperature values for solution-annealed and age-hardened material. Acceptance minima for forgings are set by ASTM B637 and by the purchase order. We test to whichever is stricter.

Table 2. Room-temperature tensile properties, solution annealed and aged
PropertyMetricImperial
Ultimate tensile strength1147 MPa166.4 ksi
0.2% offset yield strength715 MPa103.7 ksi
Elongation30%30%
Reduction of area31%31%
Hardness, aged bar29 HRC29 HRC
Hardness, annealed bar86 HRB86 HRB

Strength retained at temperature

Yield strength changes little up to 760 °C, and useful strength is retained to 927 °C. This is the property that governs grade selection.

Table 3. Elevated-temperature tensile properties, aged plate
Temp. °CTemp. °F0.2% YS, MPaUTS, MPaElong. %
20RT715114730
538100064999134
6491200643104831
704130064997829
760140062885622
816150057570928
871160050756631
927170031035950
982180013217471

Values are typical published data for wrought product, quoted for design guidance only. They are not guaranteed minima. Forging properties depend on section size, forging reduction and heat-treat response, and are reported per heat on the material certificate.

§ 04 / Physical properties

UNS N07208 physical properties

Table 4. Physical properties at room temperature, age hardened
PropertyMetricImperial
Density, solution annealed8.27 g/cm³0.299 lb/in³
Density, age hardened8.29 g/cm³0.300 lb/in³
Melting range1300 to 1375 °C2370 to 2510 °F
Gamma-prime solvus997 °C1827 °F
Modulus of elasticity217 GPa31.5 × 106 psi
Shear modulus82 GPa11.9 × 106 psi
Poisson's ratio0.3190.319
Thermal conductivity10.3 W/m·°C72 Btu-in/ft²-hr-°F
Electrical resistivity126.1 µΩ·cm49.7 µΩ·in
Mean CTE, 20 to 1000 °C16.9 µm/m·°C9.3 µin/in·°F
Specific heat, RT436 J/kg·°C0.104 Btu/lb·°F
§ 05 / Heat treatment

Heat treatment of UNS N07208 forgings

UNS N07208 is delivered solution annealed unless the order states otherwise, because that is the condition in which it can still be machined, formed and welded. Strength is developed afterwards by ageing. The standard two-step cycle is as follows.

  1. Solution anneal1121 to 1149 °C (2050 to 2100 °F), soak time set by section thickness, then rapid cool or water quench. Plate and bar are commonly annealed at 1135 °C (2075 °F).
  2. First age, gamma-prime nucleation1010 °C (1850 °F) for 2 hours, air cool. Heat-up to 1010 °C should be as fast as the furnace allows.
  3. Second age, gamma-prime growth788 °C (1450 °F) for 8 hours, air cool. This step sets the final strength.

Alternative cycles

Two other cycles are in service use and either can be run to specification. The alternative two-step cycle is 899 °C for 4 hours air cool, followed by 788 °C for 8 hours air cool, used where higher containment capability is required in engine cases and rolled rings. The single-step cycle of 802 °C for 8 hours air cool is the treatment required by the ASME pressure vessel code under Code Case 3024.

Rough machining is carried out before ageing. Finish machining and finish grinding are carried out after ageing, with the part at full hardness.

§ 06 / Forging practice

Forging UNS N07208

UNS N07208 hot-works well for a superalloy of its strength class, but the working window is narrow and grain size is easily lost. We forge between 955 °C and 1177 °C (1750 to 2150 °F), with the billet soaked long enough to reach temperature uniformly through section.

Initial breakdown is taken at the top of the range, where flow stress is lowest. Finishing passes are taken at the bottom of the range to refine grain size. Finishing too hot produces parts that meet chemistry but fail grain size and ultrasonic requirements. Hot- and cold-worked parts are annealed before ageing, so that properties develop from a known starting microstructure rather than from residual forging strain.

Starting material is melted by EAF plus VOD, then ESR remelted. The ESR step controls sulfur and oxide cleanliness, which governs the achievable ultrasonic acceptance class.

§ 07 / Product forms

UNS N07208 product forms

Jiangyin Jiangnan Metal Co., Ltd. forges UNS N07208 to customer drawings in the following forms. All are made to order; there is no standard stock list for this grade.

  • Forged rings
  • Seamless rolled rings
  • Forged flanges
  • Forged round bars
  • Forged discs and disks
  • Forged sleeves
  • Forged bushings
  • Forged shafts
  • Eccentric shafts
  • Forged tube sheets
  • Forged pipes and tubes
  • Valve bodies and seat rings
  • Forged nozzles
  • Forged blocks
  • Forged wheels
  • Near-net-shape preforms
Table 5. Supply conditions, UNS N07208 forgings
ParameterDetail
Size rangeQuoted per drawing
Delivery conditionAs forged, rough machined, solution annealed, or solution annealed and aged
Machining allowancePer drawing, or per our standard allowance table
Dimensional tolerancePer drawing
Minimum orderOne piece
Quotation turnaround24 hours on working days
§ 08 / Testing and certification

Testing, NDT and certification

Every UNS N07208 forging is supplied with a document package. Contents depend on the order. The following are available.

Table 6. Available testing and documentation
ItemStandard
Ultrasonic testingEN 10228-3, SEP 1921, ASTM A388
Liquid penetrant testingASTM E165, EN ISO 3452
Chemical analysisLadle and product analysis to ASTM B637
Tensile testingASTM E8, ISO 6892-1, room and elevated temperature
Hardness testingASTM E18 (HRC, HRB)
Grain sizeASTM E112
Material certificateEN 10204 3.1, or 3.2 with third-party witness
Third-party inspectionSGS, BV, TUV, Lloyd's, or client-nominated inspector
Dimensional reportPer drawing, issued with the certificate

Where the specification requires a heat-treatment chart, positive material identification, or retained test material, state this on the enquiry so it is priced at quotation stage.

§ 09 / Applications

Where UNS N07208 forgings are used

Aero and industrial gas turbines

Forged rings, cases, seal rings, spacers and nozzle components in the combustor, turbine and exhaust sections, where the part must hold shape and load through the 700 to 900 °C band. The alternative two-step age is worth considering for engine cases and rolled rings that require higher containment capability.

Advanced power generation

Advanced ultra-supercritical (A-USC) steam plant, supercritical CO2 cycles and concentrating solar power. These applications require creep life beyond 100,000 hours at 100 MPa and 760 °C, the regime for which UNS N07208 was characterised under ASME Code Case 3024.

Oil, gas and process equipment

Forged valve bodies, seat rings, stems and blocks; flanges and tube sheets for shell-and-tube heat exchangers; forged shafts and sleeves for chemical and plunger pumps; components for subsea and deepwater production systems, industrial air compressors and nitrogen generators.

Heavy rotating and transmission parts

Seamless rolled rings, spindles, gears and forged rolls for gearboxes, gas compressors and power transmission, where operating temperature rules out steel and rules out Inconel 718.

§ 10 / Alloy selection

UNS N07208 compared with Waspaloy, R-41, 263 and Inconel 718

Below 600 °C, Inconel 718 costs less, is stronger at room temperature, and is normally the correct choice. UNS N07208 justifies its cost between roughly 650 °C and 927 °C, and again where the component must be welded.

Table 7. Selection comparison of gamma-prime strengthened superalloys
PropertyUNS N07208WaspaloyR-41Alloy 263Inconel 718
Strengthening phaseGamma-primeGamma-primeGamma-primeGamma-primeGamma-double-prime
Gamma-prime fraction15 to 20%25 to 35%HighLown/a
Practical upper limit927 °C870 °C925 °C815 °C650 °C
Creep strength, 816 to 927 °CVery highModerateVery highLowerNot applicable
Strain-age cracking resistanceVery goodPoorPoorVery goodGood
WeldabilityGoodDifficultDifficultGoodGood
Room-temperature yield715 MPaHigherHigherLowerHigher
Contains niobiumNoNoNoNoYes
Forging specificationASTM B637AMS 5704, 5708AMS 5712n/aASTM B637, AMS 5662

Two selection rules follow. Where the component sees no sustained load above 600 °C, specify Inconel 718. Where it does, and the component is a welded or complex fabrication, UNS N07208 usually gives lower total cost than Waspaloy or R-41 despite higher raw material cost, because scrap from post-weld cracking dominates the bill on those alloys.

§ 11 / Fabrication

Welding and machining UNS N07208

Weld in the solution-annealed condition, before ageing. GTAW (TIG) and GMAW (MIG) with matching 282 filler are the preferred processes. Submerged arc welding is not recommended for this alloy because of the high heat input and weld restraint.

No preheat is required provided the base metal is above 0 °C. Interpass temperature is kept below 93 °C (200 °F). After welding, the age-hardening cycle is run. A full solution anneal beforehand is neither required nor prohibited, but is advisable on heavy sections and on complex weldments carrying high residual stress.

Machining behaves as for other high-temperature nickel alloys: low speed, heavy positive feed, rigid setup, sharp tools, flood coolant. Roughing cuts are taken before ageing.

Request a quotation

We quote UNS N07208 forgings from drawings, sketches or a size list. Quotations are normally returned within 24 hours on working days.

Jiangyin Jiangnan Metal Co., Ltd., open-die forging factory, No.1 Chengxiqiao Road, Zhouzhuang Town, Jiangyin City, Jiangsu Province, China.

  • Grade and specification (UNS N07208 to ASTM B637, plus any customer spec)
  • Drawing or dimensions, stating whether sizes are finished or rough
  • Quantity and required delivery date
  • Delivery condition: as forged, rough machined, annealed, or annealed and aged
  • NDT class and acceptance standard
  • Certificate type: EN 10204 3.1 or 3.2, and any third-party inspection
§ 12 / Questions

Frequently asked questions about UNS N07208

Is UNS N07208 the same as Alloy 282?

Yes. UNS N07208 is the Unified Numbering System designation for the alloy sold commercially as Alloy 282 and HAYNES® 282® alloy. The composition ranges are identical, so a part ordered to UNS N07208 and a part ordered to Alloy 282 are the same material. Jiangyin Jiangnan Metal Co., Ltd. accepts orders written either way.

Which standard covers UNS N07208 forgings?

UNS N07208 bars, forgings and forging stock are covered by ASTM B637 and AMS 5915. Sheet, plate and strip fall under AMS 5951. For pressure equipment, ASME Code Case 3024 covers the grade to 870 °C in Section I and Section VIII Division 1, and ASME B31 Case 219 covers piping. ASTM B564 does not list UNS N07208, so a drawing calling out B564 for this grade should be corrected.

What is the maximum service temperature of UNS N07208?

UNS N07208 is used for load-bearing structural parts up to about 927 °C (1700 °F). Its creep strength advantage sits in the 649 to 927 °C (1200 to 1700 °F) band. Above 927 °C strength falls away quickly: yield strength drops from 507 MPa at 871 °C to 132 MPa at 982 °C.

What is the heat treatment for UNS N07208 forgings?

The standard cycle is a solution anneal at 1121 to 1149 °C (2050 to 2100 °F) with rapid cooling, followed by two-step ageing: 1010 °C (1850 °F) for 2 hours air cool, then 788 °C (1450 °F) for 8 hours air cool. Two alternatives exist: 899 °C for 4 hours plus 788 °C for 8 hours for higher containment capability, and a single step of 802 °C for 8 hours required by the ASME code. Jiangyin Jiangnan Metal Co., Ltd. runs any of the three on request.

What is the density of UNS N07208?

8.27 g/cm³ (0.299 lb/in³) in the solution-annealed condition, and 8.29 g/cm³ (0.300 lb/in³) after age hardening. Use 8.27 g/cm³ for forging weight estimates.

Does UNS N07208 contain niobium?

No. Niobium is limited to 0.2 percent maximum as a residual. All precipitation strengthening comes from the gamma-prime phase Ni3(Al,Ti), formed from 1.38 to 1.65 percent aluminium and 1.90 to 2.30 percent titanium. This is the main metallurgical difference from Inconel 718, which relies on niobium-bearing gamma double prime.

Is UNS N07208 weldable?

Yes. UNS N07208 is more weldable than other alloys of comparable strength. Its resistance to strain-age cracking approaches Alloy 263 and is far better than Waspaloy or R-41, because the gamma-prime volume fraction is only 15 to 20 percent and precipitation is slow. Weld in the solution-annealed condition using GTAW or GMAW with matching filler, keep interpass temperature below 93 °C, then age. Submerged arc welding is not recommended.

UNS N07208 or Waspaloy: which should be specified?

Specify UNS N07208 where the part is welded or complex, or where it runs above about 815 °C. Its 1 percent creep strength exceeds Waspaloy across the whole 649 to 927 °C range, and its rupture strength is comparable at the low end and better at the high end, while being substantially easier to weld and form. Waspaloy has higher room-temperature yield strength, so for a machined-from-solid part that runs cool, Waspaloy may be the better choice.

What forms of UNS N07208 can you forge?

Jiangyin Jiangnan Metal Co., Ltd. produces UNS N07208 as forged rings, seamless rolled rings, flanges, round bars, discs, sleeves, bushings, shafts, eccentric shafts, tube sheets, forged pipes and tubes, valve bodies and seat rings, nozzles, blocks, wheels and near-net-shape preforms. All are made to drawing; there is no stock list for this grade.

What certification comes with the forgings?

EN 10204 3.1 certificates as standard, or EN 10204 3.2 with a third-party witness such as SGS, BV, TUV or Lloyd's. Ultrasonic testing is performed to EN 10228-3, SEP 1921 or ASTM A388 as specified. Chemical analysis, tensile results, hardness, grain size and a dimensional report are issued with the certificate.

How do I get a quotation?

Send a drawing or size list to sales@steelforgepieces.com, or call +86 189 2135 9659. Include quantity, delivery condition, NDT acceptance class and certificate type. Quotations are normally returned within 24 hours on working days. The factory is at No.1 Chengxiqiao Road, Zhouzhuang Town, Jiangyin City, Jiangsu Province, China.

§ 13 / Sources

Standards and sources

  1. ASTM B637, Standard Specification for Precipitation-Hardening and Cold Worked Nickel Alloy Bars, Forgings, and Forging Stock for Moderate or High Temperature Service. ASTM International.
  2. SAE AMS 5915, nickel alloy billet, rod, bar and forgings, UNS N07208.
  3. SAE AMS 5951, nickel alloy sheet, plate and strip, UNS N07208.
  4. ASME Boiler and Pressure Vessel Code, Code Case 3024; ASME B31 Case 219.
  5. Haynes International, HAYNES® 282® alloy principal features and property data. Source of the tensile, creep, physical property and heat-treatment data above.
  6. EN 10204, metallic products, types of inspection documents. EN 10228-3, SEP 1921 and ASTM A388, ultrasonic testing of forgings.

Trademark notice. HAYNES® and 282® are registered trademarks of Haynes International, Inc. Jiangyin Jiangnan Metal Co., Ltd. is not affiliated with, endorsed by, sponsored by, or a licensee of Haynes International, Inc. These trademarks appear on this page only to identify the material grade to which UNS N07208 corresponds, so that engineers searching by trade name can locate the correct UNS designation. Waspaloy and Inconel are trademarks of their respective owners.

Published by Jiangyin Jiangnan Metal Co., Ltd., open-die forging factory, Jiangyin, Jiangsu, China Technical content reviewed by the Jiangnan Metal engineering department First published 2019-04-12. Last reviewed and updated 2026-08-30.