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Stainless Steel V-57-ST (Solution annealed)

Heat-treated state

UNS S51770

Soft supply condition for cold forming, deep drawing, machining of complex shapes and welding before aging.

High cost $$$$

Values for the ST condition

Other V-57 tempers and conditions

V-57 is listed in 4 conditions; see the grade overview at V-57.

Compare all 4 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
STThis page
Solution annealed
Soft supply condition for cold forming, deep drawing, machining of complex shapes and welding before aging.27569045170 HB—
STADefault
Solution treated and aged
Standard aerospace bar/forging condition — best balance of strength, ductility and 650 °C creep performance.7251,0702032 HRC—
Solution treated ~900 °C (1650 °F) + aged 720 °C/16 h
Fine-grain low-temperature solution route for maximum room-temperature strength and notch ductility in fasteners and shafts.7951,1401834 HRC—
Cold drawn/cold worked then aged
Choose for high-strength bolts, studs and springs where cold work plus aging pushes strength above the standard STA level.1,0351,2401238 HRC—

What is V-57-ST?

V-57-ST is V-57 heat treated to ST — soft supply condition for cold forming, deep drawing, machining of complex shapes and welding before aging. V-57-ST has a yield strength of 275 MPa (39.9 ksi) and a tensile strength of 690 MPa (100 ksi) — weaker than 77% of stainless steel grades. Elongation at break is 45% and the elastic modulus is 201 GPa (29.2 Msi). V-57-ST has a density of 7.92 g/cm³ (0.286 lb/in³), heavier than 77% of stainless steel grades. It melts at 1,370°C (2,498 °F). STA is the default condition FabDigit quotes; ST is available on request or by drawing note.

Advantages

  • Ductile — tolerates forming and impact — 45%, better than 76% of stainless steel grades

Limitations

  • High embodied carbon — 6.8 kg CO₂/kg, worse than 95% of stainless steel grades
  • Difficult to machine — 25/100, worse than 88% of stainless steel grades
  • Low electrical conductivity — 1.9 % IACS, worse than 84% of stainless steel grades
  • Low strength — 275 MPa (39.9 ksi), worse than 77% of stainless steel grades

V-57-ST properties

Typical room-temperature values for V-57-ST; 14 are specific to this condition. Other listed values are V-57 reference data and may not represent this condition. Bars are the position among stainless steel grades.

Physical3

V-57-ST has a density of 7.92 g/cm³ (0.286 lb/in³), heavier than 77% of stainless steel grades. It melts at 1,370°C (2,498 °F).

Density7.92 g/cm³0.29 lb/in³
Melting Point (Solidus)1,370°C2,498 °F
Liquidus Temperature1,425°C2,597 °F

Mechanical16

V-57-ST has a yield strength of 275 MPa (39.9 ksi) and a tensile strength of 690 MPa (100 ksi) — weaker than 77% of stainless steel grades. Elongation at break is 45% and the elastic modulus is 201 GPa (29.2 Msi).

Elastic (Young's) Modulus201 GPa29.2 Msi
Shear Modulus77 GPa11.2 Msi
Bulk Modulus165 GPa23.9 Msi
Poisson's Ratio0.31
Tensile Strength (Ultimate)690 MPa100 ksi
Yield Strength (0.2% offset)275 MPa39.9 ksi
Elongation at Break45%
Reduction in Area55%
Compressive Strength745 MPa108 ksi
Shear Strength655 MPa95 ksi
Fatigue Strength (Endurance Limit)280 MPa40.6 ksi
Fracture Toughness (K_IC)130 MPa·√m118 ksi·√in
Charpy V-Notch Impact (RT)100 J73.8 ft·lbf
Hardness, Brinell170 HB
Hardness, Rockwell C32 HRC
Hardness, Vickers320 HV

Thermal6

V-57-ST is rated for continuous service to 540°C (1,004 °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 16.5 µm/m·K (9.17 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)16.5 µm/m·K9.2 µin/in·°F
Latent Heat of Fusion285 J/g123 BTU/lb
Max Service Temperature (continuous)540°C1,004 °F
Min Service Temperature-253°C-423 °F

Electrical3

V-57-ST 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

Chemical & Environmental3

Corrosion resistance is good (62/100), worse than 52% of stainless steel grades.

Galvanic Potential (seawater, vs SCE)-0.1 V
Corrosion ResistanceGood62/100
Chemical Resistance SummaryGood oxidation resistance in air to ~700 °C and general aqueous resistance similar to 304/321; limited pitting resistance in chlorides (only ~1.25 % Mo) and vulnerable to hot halide stress corrosion and strongly reducing acids.

Sustainability4

Producing a kilogram of V-57-ST 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

V-57-ST's machinability is poor (25/100, worse than 88% of stainless steel grades); weldability good (55/100); formability good (60/100).

MachinabilityPoor25/100
Machinability Rating (AISI 1212 = 100 %)20%
WeldabilityGood55/100
Formability (cold)Good60/100
Brazeability / SolderabilityFair40/100
PolishabilityVery good70/100
Anodizing Responsen/a — ferrous alloy; use passivation (ASTM A967) or electropolish instead

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

Working with V-57-ST

Is V-57 easy to machine?

Machine in the solution-treated state where possible; aged material is gummy and work-hardening — use rigid setups, positive-rake carbide or ceramic, low speed (15–25 m/min carbide), heavy feed and flood coolant.

Can V-57 be welded?

GTAW/EBW in the solution-treated condition with matching A-286/V-57 or Ni-base filler, then full solution + age; avoid welding aged material because of strain-age (post-weld) cracking.

Can V-57 be formed, bent or molded?

Cold form, roll-thread or coil springs before aging (solution-treated stock is quite ductile); hot work at 1010–1150 °C and finish above 950 °C to avoid tearing.

What surface finishes work on V-57?

Passivate per ASTM A967 or electropolish; no anodizing — for high-temperature fasteners silver, cadmium-free lubricious coatings or dry-film lubricants are typical.

V-57 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
Mn≤ 0.350.25
Si≤ 0.750.4
P≤ 0.03—
S≤ 0.03—
Cr13 – 1614.8
Ni25.5 – 28.527
Mo1 – 1.51.25
Tiγ′ Ni₃(Ti,Al) former2.7 – 3.23
Vvanadium addition distinguishing V-57 from A-2860.1 – 0.50.3
Al≤ 0.350.25
Bgrain-boundary strengthener0.010.01
Febalance, ~52 %balance—

V-57-ST — frequently asked

What is V-57-ST used for?

V-57-ST is typically used for aerospace fasteners, turbine engine hardware and high-strength bolting. In short: higher-strength A-286 type; 650 °C aerospace fastener alloy; age-hardened iron-base superalloy.

What is the yield strength of V-57-ST?

V-57-ST has a typical yield strength of 275 MPa (39.9 ksi) and a tensile strength of 690 MPa (100 ksi) — weaker than 77% of stainless steel grades. Strength varies by condition: see the 4 listed tempers.

Is V-57-ST easy to machine?

Not especially — machinability is rated poor (25/100, worse than 88% of stainless steel grades). Machine in the solution-treated state where possible; aged material is gummy and work-hardening — use rigid setups, positive-rake carbide or ceramic, low speed (15–25 m/min carbide), heavy feed and flood coolant.

Can V-57-ST be welded?

Yes — weldability is rated good (55/100). GTAW/EBW in the solution-treated condition with matching A-286/V-57 or Ni-base filler, then full solution + age; avoid welding aged material because of strain-age (post-weld) cracking.

What surface finishes work on V-57-ST?

Passivate per ASTM A967 or electropolish; no anodizing — for high-temperature fasteners silver, cadmium-free lubricious coatings or dry-film lubricants are typical.

Can V-57-ST be formed, bent or molded?

Cold form, roll-thread or coil springs before aging (solution-treated stock is quite ductile); hot work at 1010–1150 °C and finish above 950 °C to avoid tearing.

What is the maximum service temperature of V-57-ST?

V-57-ST is rated for continuous use to about 540°C (1,004 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between V-57-STA and V-57-ST?

STA is the default condition — standard aerospace bar/forging condition — best balance of strength, ductility and 650 °C creep performance. ST: soft supply condition for cold forming, deep drawing, machining of complex shapes and welding before aging. Yield strength is 725 MPa in STA versus 275 MPa in ST.

Sources

  1. AMS 5770 — Fe-Ni-Cr precipitation-hardenable alloy bars, forgings and rings — SAE International (2018)
  2. ASTM A638/A638M — Precipitation Hardening Iron Base Superalloy Bars, Forgings and Forging Stock for High-Temperature Service — ASTM (2019)
  3. ASM Specialty Handbook: Heat-Resistant Materials — ASM International (1997)
  4. ASM Handbook Vol.1 — Properties and Selection: Irons, Steels and High-Performance Alloys — ASM International (1990)
  5. MMPDS-18 (A-286 class Fe-Ni superalloy allowables, used as analogue) — Battelle/FAA (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.