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Stainless Steel 660 A453-660-A

Certified grade

AISI/SAE 660 · UNS S66286 · JIS SUH660

A453-660-A = aSTM A453 Gr 660 Class A

Order this class when a pressure-vessel/flange bolting certificate to A453 Gr 660 Class A minima is required.

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Values for the A453-660-A condition

Other 660 tempers and conditions

660 is listed in 7 conditions; see the grade overview at 660.

Compare all 7 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
980–1010 °C anneal, softest supply condition
Choose for maximum cold formability of sheet/strip and for wire before drawing; must be aged afterwards to develop strength.28064045150 HB—
980 °C/1 h + oil or water quench (AMS 5731/5737 pre-age)
Standard stock condition for bar, sheet and wire that will be machined or formed and then age hardened by the user.31069040160 HB—
A453-660-AThis page
ASTM A453 Gr 660 Class A
Order this class when a pressure-vessel/flange bolting certificate to A453 Gr 660 Class A minima is required.5858951529 HRC1.9 % IACS
solution 980 °C + age 720 °C/16 h (AMS 5731/5737, A453 Gr 660 Cl A)
The normal service condition: γ′ precipitation gives ~1000 MPa tensile with good 540–700 °C strength and stress-relaxation resistance for bolts and turbine hardware.6901,0002032 HRC—
solution treated then cold drawn bar/wire (unaged)
Pick for close-tolerance bright bar and wire feedstock where strength above the solution-annealed level is wanted before final ageing.7009001823 HRC1.9 % IACS
STA
Lower solution temperature keeps a finer grain size for higher room-temperature yield strength in bolting; slightly lower creep/rupture capability than the 980 °C treatment.7601,0351734 HRC—
Cold Worked + Aged
Highest strength form, used for high-temperature springs, retaining rings and fasteners where 1300–1500 MPa with 500–600 °C relaxation resistance is required.1,2501,400644 HRC1.9 % IACS

What is 660 A453-660-A?

660 A453-660-A is 660 in a A453-660-A certified grade — order this class when a pressure-vessel/flange bolting certificate to A453 Gr 660 Class A minima is required. 660 A453-660-A has a yield strength of 585 MPa (84.8 ksi) and a tensile strength of 895 MPa (130 ksi) — stronger than 86% of stainless steel grades. Elongation at break is 15% and the elastic modulus is 201 GPa (29.2 Msi). 660 A453-660-A has a density of 7.94 g/cm³ (0.287 lb/in³), heavier than 78% of stainless steel grades. It melts at 1,370°C (2,498 °F). Solution Annealed is the default condition FabDigit quotes; A453-660-A is available on request or by drawing note.

Advantages

  • High strength — 585 MPa (84.8 ksi), better than 86% of stainless steel grades

Limitations

  • Difficult to machine — 22/100, worse than 95% of stainless steel grades
  • High embodied carbon — 6.8 kg CO₂/kg, worse than 95% of stainless steel grades
  • Limited ductility — 15%, worse than 89% of stainless steel grades
  • Low electrical conductivity — 1.9 % IACS, worse than 84% of stainless steel grades
  • Difficult to weld — 40/100, worse than 83% of stainless steel grades

660 A453-660-A properties

Typical room-temperature values for 660 A453-660-A; 22 are specific to this condition. Other listed values are 660 reference data and may not represent this condition. Bars are the position among stainless steel grades.

Physical3

660 A453-660-A has a density of 7.94 g/cm³ (0.287 lb/in³), heavier than 78% of stainless steel grades. It melts at 1,370°C (2,498 °F).

Density7.94 g/cm³0.29 lb/in³
Melting Point (Solidus)1,370°C2,498 °F
Liquidus Temperature1,400°C2,552 °F

Mechanical13

660 A453-660-A has a yield strength of 585 MPa (84.8 ksi) and a tensile strength of 895 MPa (130 ksi) — stronger than 86% of stainless steel grades. Elongation at break is 15% and the elastic modulus is 201 GPa (29.2 Msi).

Elastic (Young's) Modulus201 GPa29.2 Msi
Shear Modulus77 GPa11.2 Msi
Bulk Modulus176 GPa25.5 Msi
Poisson's Ratio0.31
Tensile Strength (Ultimate)895 MPa130 ksi
Yield Strength (0.2% offset)585 MPa84.8 ksi
Elongation at Break15%
Reduction in Area18%
Shear Strength580 MPa84.1 ksi
Fatigue Strength (Endurance Limit)440 MPa63.8 ksi
Charpy V-Notch Impact (RT)45 J33.2 ft·lbf
Hardness, Brinell280 HB
Hardness, Rockwell B85 HRB

Thermal5

660 A453-660-A is rated for continuous service to 650°C (1,202 °F). It conducts heat at 14 W/m·K (8.09 BTU/hr·ft·°F), worse than 80% of stainless steel grades. Thermal expansion is 16.6 µm/m·K (9.22 µin/in·°F).

Thermal Conductivity14 W/m·K8.1 BTU/hr·ft·°F
Specific Heat Capacity460 J/kg·K0.11 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)16.6 µm/m·K9.2 µin/in·°F
Max Service Temperature (continuous)650°C1,202 °F
Min Service Temperature-196°C-321 °F

Electrical3

660 A453-660-A conducts electricity at 1.9 % IACS, worse than 84% of stainless steel grades.

Electrical Conductivity1.9 % IACS
Electrical Resistivity9.1×10⁻⁷ Ω·m35.8 µΩ·in
Magnetic Responsenon-magnetic (austenitic, µr ≈ 1.005; may become weakly magnetic after heavy cold work)

Chemical & Environmental3

Corrosion resistance is good (60/100), worse than 58% of stainless steel grades.

Galvanic Potential (seawater, vs SCE)-0.1 V
Corrosion ResistanceGood60/100
Chemical Resistance SummaryOxidation-resistant to ~800 °C in air and resistant to steam and mild industrial atmospheres; general aqueous corrosion similar to 304/316, so it is not intended for strong chlorides, seawater immersion, or hot reducing acids. Susceptible to sulfidation and to hot-salt stress corrosion in high-temperature service.

Sustainability4

Producing a kilogram of 660 A453-660-A takes about 95 MJ of energy and emits 6.8 kg of CO₂ — more than 96% of stainless steel grades. Typical recycled content is 30%.

Embodied Energy (primary production)95 MJ/kg40,843 BTU/lb
Embodied Carbon (primary production)6.8 kg CO₂/kg
Embodied Water200 L/kg24 gal/lb
Typical Recycled Content30%

Manufacturability7

660 A453-660-A's machinability is poor (22/100, worse than 95% of stainless steel grades); weldability fair (40/100); formability poor (25/100).

MachinabilityPoor22/100
Machinability Rating (AISI 1212 = 100 %)18%
WeldabilityFair40/100
Formability (cold)Poor25/100
Brazeability / SolderabilityFair50/100
PolishabilityVery good70/100
Anodizing Responsen/a — not anodizable; use passivation or electropolishing for surface finishing

Values are nominal handbook figures for design screening. Confirm any required mill or lot documentation when quoting.

Working with 660 A453-660-A

Is 660 easy to machine?

Gummy and highly work-hardening — machine in the solution-treated condition where possible with rigid setups, positive-rake carbide, heavy flood coolant, low speed (15–25 m/min) and constant feed to avoid glazing; aged material typically cut at ~15 % of AISI 1212 rates.

Can 660 be welded?

GTAW/EBW with matching A286 or Ni-base filler works, but the alloy is prone to hot cracking and strain-age cracking; weld in the solution-treated state, restrain minimally, and re-solution plus age the weldment for full properties.

Can 660 be formed, bent or molded?

Cold form and draw only in the annealed/solution-treated condition, allowing for high springback and ~2× the load of 304; hot work at 1100–950 °C then solution treat, and never form aged material.

What surface finishes work on 660?

Not anodizable — passivate per AMS 2700/ASTM A967, electropolish or mechanically polish; oxide films from ageing must be pickled or blasted off before plating, and silver or MoS2 coatings are common on fasteners to prevent galling.

660 chemical composition (wt %)

Limits by weight percent from the governing specification, written the way the spec states them — a single maximum for impurities, a range for alloying elements, and the base element as balance. Nominal is the typical mid-range value.

ElementSpec limit (wt %)Nominal
C≤ 0.080.05
Si≤ 10.5
Mn≤ 21.3
P≤ 0.04—
S≤ 0.03—
Cr13.5 – 1614.8
Ni24 – 2725.5
Mo1 – 1.51.25
Tiγ′ (Ni3Ti) former1.9 – 2.352.1
V0.1 – 0.50.3
Al≤ 0.350.2
Bgrain-boundary strengthener0 – 0.010.01
Febalance, ~53 %balance—

660 A453-660-A — frequently asked

What is 660 A453-660-A used for?

660 A453-660-A is typically used for aircraft engine fasteners and turbine bolting, gas-turbine discs and ring parts, exhaust valves, high-temperature springs, turbocharger components and jet engine casings and housings. In short: high-temp aerospace stainless.

What is the yield strength of 660 A453-660-A?

660 A453-660-A has a typical yield strength of 585 MPa (84.8 ksi) and a tensile strength of 895 MPa (130 ksi) — stronger than 86% of stainless steel grades. Strength varies by condition: see the 7 listed tempers.

Is 660 A453-660-A easy to machine?

Not especially — machinability is rated poor (22/100, worse than 95% of stainless steel grades). Gummy and highly work-hardening — machine in the solution-treated condition where possible with rigid setups, positive-rake carbide, heavy flood coolant, low speed (15–25 m/min) and constant feed to avoid glazing; aged material typically cut at ~15 % of AISI 1212 rates.

Can 660 A453-660-A be welded?

With care — weldability is rated fair (40/100). GTAW/EBW with matching A286 or Ni-base filler works, but the alloy is prone to hot cracking and strain-age cracking; weld in the solution-treated state, restrain minimally, and re-solution plus age the weldment for full properties.

What surface finishes work on 660 A453-660-A?

Not anodizable — passivate per AMS 2700/ASTM A967, electropolish or mechanically polish; oxide films from ageing must be pickled or blasted off before plating, and silver or MoS2 coatings are common on fasteners to prevent galling.

Can 660 A453-660-A be formed, bent or molded?

Cold form and draw only in the annealed/solution-treated condition, allowing for high springback and ~2× the load of 304; hot work at 1100–950 °C then solution treat, and never form aged material.

What is the maximum service temperature of 660 A453-660-A?

660 A453-660-A is rated for continuous use to about 650°C (1,202 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between 660 Solution Annealed and 660 STA-900?

Solution Annealed is the default condition — standard stock condition for bar, sheet and wire that will be machined or formed and then age hardened by the user. STA-900: lower solution temperature keeps a finer grain size for higher room-temperature yield strength in bolting; slightly lower creep/rupture capability than the 980 °C treatment. Yield strength is 310 MPa in Solution Annealed versus 760 MPa in STA-900.

Can FabDigit make parts in 660 A453-660-A?

Yes — 660 A453-660-A is available for CNC machining and sheet metal; every part is priced by an engineer rather than instantly. Upload a STEP file to get a price and a DFM check.

Sources

  1. ASTM A453/A453M Grade 660 — Bolting with Expansion Coefficients Comparable to Austenitic Stainless Steels — ASTM International (2021)
  2. AMS 5731 / 5732 / 5734 / 5737 — Alloy Bars, Forgings and Rings, 15Cr-25.5Ni-1.2Mo-2.1Ti-0.3V-0.005B — SAE International (2018)
  3. JIS G 4311 SUH660 / GB/T 1221 (0Cr15Ni25Ti2MoAlVB, GH2132) — JISC / SAC (2016)
  4. ASM Specialty Handbook: Heat-Resistant Materials — ASM International (1997)
  5. MMPDS-17, Metallic Materials Properties Development and Standardization — Battelle/FAA (2022)
  6. A286 / Alloy 660 technical data sheet — Specialty steel producers (e.g. Carpenter, Aubert & Duval, VDM) (2023)

Property data is compiled from published supplier and standards handbooks and normalised for comparison. Nothing on this page is a certification — request mill certs, CoC or material test reports with your order.